Model Aeroplanes and Their Engines: A Practical Book for Beginners

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Title: Model Aeroplanes and Their Engines: A Practical Book for Beginners
Author: Cavanagh, George
Language: English
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————————————— Start of Book —————————————

[Illustration: Waid Carl’s model in flight.

Courtesy Edward P. Warner, Concord Model Club]

MODEL AEROPLANES
AND THEIR ENGINES

_A Practical Book for Beginners_

BY
GEORGE A. CAVANAGH
MODEL EDITOR “AERIAL AGE”

DRAWINGS BY
HARRY G. SCHULTZ
PRESIDENT THE AERO-SCIENCE CLUB OF AMERICA

WITH AN INTRODUCTION BY
HENRY WOODHOUSE
Managing Editor “Flying”
Governor of the Aero Club of America

NEW YORK
MOFFAT, YARD & COMPANY
1917

Reprinted August, 1917

TO
M. T. H.

INTRODUCTION

History tells us—what some of us luckier ones heard the Wright Brothers
themselves tell—that the Wrights’ active work in aëronautics was a
result of the interest aroused by a toy helicopter presented to them by
the Reverend Bishop Milton Wright, their father.

Tremendous developments have taken place in aëronautics and aircraft
are fast developing in size, speed, and range of action. They have
revolutionized warfare, and seem to be destined to become a most
important factor in the reconstruction that will follow the war.

The greater the development the truer the fact that model aëroplanes
may be instrumental in bringing to aëronautics men who may make
valuable contributions to aëronautics. As a matter of fact, there are
already in active life, contributing their share to the development of
aëronautics, young men who only a few years ago competed for prizes
which the writer offered for model competition.

The young men who are now flying models will live in the new age—and
they have much to give and much to receive from it.

Through the tremendous strides forward of aëronautics there are
wonderful possibilities for the employment of ingenuity, genius
and skill, and business opportunities, as great as have ever been
created by progress in important lines of human endeavor. Problems
of engineering as huge as were solved by master builders; juridical
and legal questions to be decided as stupendously difficult as any
Gladstone would wish them; possibilities for the development of
international relations greater than were ever conceived; problems
of transportation to be solved by the application of aircraft,
as wonderful as any economist could wish; opportunities to gain
distinction splendid enough to satisfy the most ambitious person.

HENRY WOODHOUSE.

New York, June 5th, 1916.

LIST OF CONTENTS

PAGE
INTRODUCTION ix

HISTORY OF MODEL AVIATION 1

CONSTRUCTION 8
Propellers—Wings—Frame—Assembling—Launching—
Chassis—Pontoons—Launching an R. O. G. or Model
Hydroaëroplane.

WORLD RECORD MODELS 52
Lauder Distance and Duration Model—Hittle Tractor
Hydro—La Tour Flying Boat—Cook No. 42 Model—Rudy Funk
Duration Model—Alson H. Wheeler Twin Pusher Biplane.

A MODEL WARPLANE 83

A SIMPLE COMPRESSED AIR ENGINE 85–93

COMPRESSED AIR DRIVEN MODELS 94–102
The Dart Compressed Air Driven Model—The McMahon
Compressed Air Driven Monoplane—The McMahon
Compressed Air Driven Biplane.

COMPRESSED AIR ENGINES 103–109
Wise Compressed Air Engine—Schober-Funk Three Cylinder
Engine—The Schober Four Cylinder Opposed Engine.

GASOLINE ENGINES 110–117
Jopson—Midget Aëro Gasoline Engine.

STEAM POWER PLANTS 118–122
H. H. Groves Steam Power Plants—G. Harris’s Steam
Engine—Professor Langley’s Steam Engine—French
Experiments with Steam Power Plants.

CARBONIC GAS ENGINE 123–124

THE FORMATION OF MODEL CLUBS 125–138

WORLD’S MODEL FLYING RECORDS 139–141

DICTIONARY OF AËRONAUTICAL TERMS 142–152

LIST OF ILLUSTRATIONS

PAGE
Model Aëroplane in Flight _Frontispiece_

First Model Aëroplane Exhibition Opp. 4

Propellers (Diagram 1) 9

How to cut propellers (Diagram 2) 11

Designs for propellers (Diagram 3) 14

Designs for propellers (Diagram 4) 17

Wing construction (Diagram 5) 20

Members of the Aëro Science Club Opp. 22

Members of the Milwaukee and Illinois Model Aëro
Clubs Opp. 22

Frame construction (Diagram 6) 25

Model Assembly (Diagram 7) 30

C. W. Meyer and Wm. Hodgins exhibiting early type
models Opp. 32

Henry Criscouli with five foot model Opp. 32

Schultz hydroaëroplane Opp. 32

Rubber winder (Diagram 8) 35

Chassis construction (Diagram 9) 38

Pontoon construction (Diagram 10) 43

Obst flying boat Opp. 44

McLaughlin twin tractor hydroaëroplane Opp. 44

Louis Bamberger hydro about to leave water Opp. 44

E. B. Eiring and Kennith Sedgwick Milwaukee Club How
to launch R. O. G. model Opp. 48

Waid Carl, Concord Model Club Launching R. O. G.
model Opp. 48

Wallace A Lauder model (Diagram 11) 54

Lauder distance and duration model Opp. 56

Lauder R. O. G. model Opp. 56

Lindsay Hittle world record hydroaëroplane (Diagram 12)
61

La Tour Flying Boat (Diagram 13) 66

Ellis Cook R. O. G. model (Diagram 14) 73

Funk duration model (Diagram 15) 78

Rudy Funk speed model Opp. 80

McMahon and Schober compressed air driven models Opp. 80

Alson H. Wheeler twin pusher biplane Opp. 82

C. V. Obst tractor Opp. 82

Model Warplane 84

Simple compressed air engine (Diagram 16) 87

Schober compressed air driven monoplane Opp. 90

Schober compressed air driven biplane Opp. 90

Dart compressed air driven model 95

John McMahon and compressed air driven monoplane Opp. 98

Frank Schober preparing model for flight Opp. 98

John McMahon pusher biplane (Diagram 17) 102

Wise compressed air engine Opp. 104

Schober-Funk three-cylinder rotary engine Opp. 105

Schober four cylinder engine (Diagram 18) 107

Jopson gasoline engine Opp. 110

Sectional view of Jopson engine (Diagram 19) 112

Power curve of Jopson engine (Diagram 20) 115

Midget gasoline engine Opp. 116

English steam power plant Opp. 120

V. E. Johnson steam driven hydroaëroplane Opp. 120

English compressed air driven biplane Opp. 122

Tractor hydroaëroplane fitted with steam power plant Opp. 122

English compressed air engine fitted with simple
speedometer Opp. 122

The Rompel six-cylinder carbonic gas engine Opp. 124

MODEL AËROPLANES

HISTORY OF MODEL AVIATION

Model aëroplaning, as a sport, was first introduced in America during
the year of 1907. It was then that the first model aëroplane club in
America was formed by Miss E. L. Todd, with the assistance of Mr.
Edward Durant, now Director of the Aëro Science Club of America.
Prior to this the model aëroplane was considered an instrument of
experimentation or, when built to resemble a full sized machine,
was used for exhibition purposes. Noted scientists, men such as
Maxim, Langley, Eiffel and others, depended largely on models to
bring about the desired results during their experiments. Before the
Wright Brothers brought forth and launched the first heavier than air
machine their experiments, to a great extent, were confined to model
aëroplanes. There is little doubt but that a large majority of aviators
engaged in flying machines in different parts of the world were at one
time in their career interested in the construction and flying of model
aircraft, and from which no doubt they obtained their initial knowledge
of the aëroplane, in so far as the same principles and laws apply to
any aëroplane, regardless of its size.

The first model aëroplane club went under the name of the New York
Model Aëro Club and during its existence a great many of its contests
were carried on in armories. The reason for this was because of the
fact that the greater number of the models prevalent at that time
were built along the lines of full sized machines, and their manner
of construction was such as to interfere with the flying efficiency
of the model. Streamline construction was something unknown to model
constructors in those days and, in consequence, crudely constructed
and heavy models were very often evidenced, and, as a result, flights
of over one hundred feet were very seldom made. At about the same time
model enthusiasts in both England and France were actively engaged
in constructing and flying models, but the type of model used was of
a different design from those flown by the American modelists and
as a result of this innovation many of the early records were held
abroad. The type of model flown by the English modelists resembled in
appearance the letter “A”, hence the term “A” type.

It was not long after the introduction of this type of model in America
that model aëroplaning as a sport began to assume an aspect of great
interest. Models were constructed along simpler lines and with a
greater tendency toward doing away with all unnecessary parts, thus
increasing the flying qualities of the models. Flights of greater
distance and duration were the objects sought and, in their efforts to
achieve them new records were made at most every contest, until flights
of from 500 to 1000 feet were common occurrences. By the use of the A
type model and the single stick model which made its appearance shortly
after the A type model, American modelists succeeded in breaking most
of the world records for this type of model which is now termed by
English modelists “flying sticks.”

[Illustration: First model aëroplane exhibition held at Boston, 1910]

One by one model aëroplane clubs were formed in different parts of the
country until to-day there are in existence about twenty-five clubs
and all with memberships of from two to eight times that of the first
model aëro club. The work which was started by the New York Model Aëro
Club is now being carried on by the Aëro Science Club of America and
its affiliated clubs. The interest in model flying grew to such an
extent that during the year of 1915 the Aëro Club of America decided
to hold the First National Model Aëroplane Competition for the purpose
of offering to the young men of America an opportunity of becoming
acquainted with this new sport and its advantages. The results of
this competition were beyond expectation. Models were made capable
of flying distances and with durations that, to the early flyers,
seemed impossible. In the hand launched contests models were flown for
distances ranging from 2000 to 2500 feet, the winning flight being
3537 feet, and it might also be said that the contestant who flew this
model, with a model of the same design established a duration record
of 195 seconds. As this goes to press, information is received that
the World’s Record for distance for hand launched models has been
broken by Thomas Hall, of Chicago, Ill., an Illinois Model Aëro Club
member, with a flight of 5337 feet. Another interesting result of the
competition was the establishing of a world hydroaëroplane record by
a member of the Illinois Model Aëro Club with a model of the tractor
type, a four-bladed propeller being used in connection with the model.
The flying boat which is a late advent to the field of model flying
also proved a record breaker in this competition, having remained in
the air after rising from the surface of the water, for a duration of
43 seconds. This model was flown by a member of the Pacific Northwest
Model Aëro Club of Seattle, Washington. The establishing of these
records clearly indicates the advantage of scientific designing and
construction and careful handling.

So satisfactory have been the results of the First National Model
Aëroplane Competition that the Aëro Club of America has made
arrangements for holding the Second National Model Aëroplane
Competition during the year 1916. But in the announcement of the Second
National Competition the Aëro Club of America has made provision for
the holding of contests for mechanically driven models, in view of
the interest which is being shown by model flyers in the construction
of models more closely resembling large machines to be driven by
compressed air, steam and gasoline power plants. This is the outcome
of a desire on the part of model constructors to substitute for what
is now commonly known as the “flying stick,” models more closely
resembling large machines, which models can be more satisfactorily
flown by the use of compressed air, steam or gasoline power plants. As
in the early days, the best flights made by models using compressed air
and steam have been made by English flyers, the duration of the flights
ranging anywhere from 25 to 50 seconds.

Whether or not the American flyers will repeat history and achieve
greater results with this type of model motive power is something that
can only be determined in the future. But in any event the scientific
mechanically driven model will, without doubt, assume an important
position in the field of model aviation.

CONSTRUCTION

PROPELLERS

Propellers may be cut from various kinds of wood, but the most
suitable, from every standpoint, is white pine. The advantage of using
this wood lies in the fact that the propellers may be cut more rapidly
and when cut are lighter than those made from most other kinds of wood.
When coated with the proper kind of varnish they are sufficiently
strong for ordinary flying. Wood selected for propellers should be free
from knots, holes and other imperfections and it is very desirable that
it should be of perfectly straight grain.

A piece of such clear white pine 8″ long, 1″ wide and ³⁄₄″ thick should
be selected and on one side marked TOP. A tracing of the propeller
similar in design to Figure 1, should be laid on this piece of wood and
an imprint of the propeller design drawn on the TOP side.

[Illustration: Diagram 1]

To find the center of the block two lines should be drawn from the
opposite corners, their point of meeting being approximately in the
center—near enough for all practical purposes to insure greater
accuracy. Similar lines should be drawn from the corners on the BOTTOM
side of the block of wood. A hole ³⁄₃₂ of an inch in diameter should
be bored through the center thus obtained, through which the propeller
shaft will be inserted when the propeller is finished. The two sections
of the propeller blades drawn in diagrammatical form on the TOP of the
block, should be marked respectively BLADE 1 and BLADE 2, as shown in
diagram 1. The block is then ready for the commencement of the actual
cutting. In cutting out the propeller, BLADE 1 should be held in the
left hand and the knife in the other, with the blade of the knife on
the straight edge of BLADE 1. The cutting should be carried out very
carefully with attention constantly paid to Fig. 2, and should be
stopped when the line shown in Fig. 2 has been reached. The semi-blade
should then be sandpapered until a small curve is obtained by which the
propeller will be enabled to grip the air.

[Illustration: Diagram 2]

To cut BLADE 2, BLADE 1 should be held in the left hand and BLADE 2 cut
until the line shown in Fig. 3 is reached, after which the sandpapering
process is carried out in the same manner as in the case of BLADE 1.
During all of the foregoing operations it must be clearly borne in
mind that the TOP of the blank propeller must always face upward,
and the cutting should always be done on the STRAIGHT lines. Should
the straight edge be cut on one edge of the blank propeller and the
curved edge on the other, it would result in the blades of the finished
propeller having a tendency to push in opposite directions and in
consequence no propulsion of the model would be possible.

Attention should next be turned to the back of the propeller blank on
which the manner of cutting is exactly like that suggested for the top
side, with the exception that instead of cutting along the STRAIGHT
lines, the cutting is done along the CURVED lines. In this part of
the work great care is to be exercised for by the time the necessary
cutting has been done on the back of the propeller the entire structure
is very fragile and one excessive stroke of the knife may result in
destroying the entire propeller blade. By constantly holding the wood
to the light it is possible to determine with a reasonable degree of
accuracy the evenness of thickness. To complete the BOTTOM side of the
propeller the blade should be sandpapered as was the top.

The method of cutting the second propeller is exactly that used in
cutting the first propeller, only that the diagram shown in Fig. 4
should be used. This will result in two propellers being made that will
revolve in opposite directions in order to produce even and balanced
propulsion. If both propellers revolved in the same direction the
effect would be to overturn the model.

[Illustration: Diagram 3]

In diagram 1 the propellers are shown with the straight edge as the
entering or cutting edge of the blade. Some of the model builders
prefer the curved edge as the cutting edge (diagram 2). It is
significant that Mr. Frank Schober, a well known model constructor,
tested both designs on his compressed air driven model, and while
both propellers were the same in weight, diameter and pitch, the one
having the straight edge as the cutting edge was found one-third more
efficient.

When the propellers have been given a light coat of shellac they should
be laid aside until the assembling of the complete model.

By following the foregoing instructions a simple and effective set of
propellers will be produced. But in order to vary the experimental
practice of the constructor various other diagrams, Nos. 3 and 4,
illustrating suitable designs, are provided and can be made by applying
the above general theory and using the diagrams herewith.

WINGS

One of the most important considerations in the construction of a model
is the making of the wings. To obtain the greatest efficiency the
wings must be carefully designed, with due attention to whether the
model is being constructed for speed, duration or climbing ability.
Attention should be given to streamline construction; that is, the
parts of the wing should be so assembled that the completed wing would
offer the least possible resistance to the air, if the best results are
to be obtained.

For the main wing three strips of spruce, each 30″ in length, two of
them being ³⁄₁₆″ × ¹⁄₄″ and the third ³⁄₁₆″ × ¹⁄₁₆″ are required. To
make them thoroughly streamline all edges should be carefully rounded
off and all surfaces should be smooth. A strip of bamboo at least 20″
long, ¹⁄₂″ wide, ¹⁄₈″ thick, should be cut into pieces, each piece to
be 5 in. long. To secure the necessary curve, ¹⁄₂″ depth, the pieces
of bamboo should be held in steam and slowly bent in a manner closely
resembling the skids of an ordinary bobsled. When the curvature has
been obtained, care should be exercised in cutting each piece into four
longitudinal strips, from which twelve should be selected to be used as
ribs, each to be ¹⁄₈″ wide. The bending of the bamboo preliminary to
making the ribs is done in order to secure uniformity of curvature.

[Illustration: Diagram 4]

When this has been done the ribs are ready for fastening to the
sticks—entering and trailing edges—and each must be attached an equal
distance apart. In order that the ribs may be evenly spaced it is
necessary to put a mark every 3″ on the larger stick or entering edge
of the wing, and also on the flat stick or trailing edge. The main beam
which is of the same dimensions as the entering edge is afterwards
fastened across the center of the wing, and does not necessarily need
to be thus marked, as it is fastened to the ribs after the ribs have
been attached to the entering and trailing edges of the wing frame.
By holding the ribs one at a time so that the curved edge rests upon
the entering edge where the mark indicates, as shown in diagram 5,
they should be fastened thereon by means of thread and glue. The rear
end of the rib must be fastened to the trailing edge where the mark
indicates, also by thread and glue.

After all ribs have been thus securely fastened to both edges of the
frame the third stick, or main beam, should be attached to the frame
on the underside, the fastening being made at the highest point of
the curve of each rib. This main beam prevents the wing covering from
drawing in the end ribs and adds very materially to the strength of
the entire wing structure. To cover the wings fiber paper may be used
and is a suitable material, but the best results, from a standpoint of
flying efficiency and long service, are obtained by the use of China
silk.

The frame of the forward wing or elevator is made in the same manner
as is the main wing, but it is only 12″ in span by 4″ in chord, and is
constructed without the use of a main beam. This wing has only five
ribs which are made in the same manner as those for the rear wing, and
each is placed a distance of 3″ apart.

[Illustration: Diagram 5]

A piece of silk measuring 2″ longer and 2″ wider than each of the wing
frames should be used in covering the wings, and this can be held in
position by the use of pins prior to the actual sewing. The extra inch
of silk on all sides of the frame is placed around the under side of
the frame—in order that it can be made thoroughly taut when the silk
has been sewn close to the edges of the frame. After the silk has been
sewn close to the edges the pins may be removed and the surplus silk
that hangs from the under side of the frame may be cut off. To make
this silk airproof it should be coated with a thin coat of shellac or
varnish and the wings should be thoroughly dry before being used. This
coating, in addition to airproofing, will assist in making the covering
perfectly taut, and also in making the wing ready for service when the
entire model is ready to be assembled.

FRAME

As all other parts of the model are attached to the frame in addition
to its having to stand the strain of the tightly wound rubber strands
which serve as the motive power for the model, it must be made strong.
It is therefore necessary to exercise care and judgment in making
certain that the different units that make up the frame are rightly
proportioned and are of the proper material. Just as in the large sized
aëroplanes there are many types of bodies, so there are many different
types of frames in use in model construction, but the standard, and for
all practical purposes the best frame, resembles the letter A in shape,
hence the name A type. The lightness of the frame depends entirely on
the materials used and the manner in which it is constructed.

Some model flyers use but a single stick for the frame, but generally
the A type frame is preferred for the reason that it is more durable,
the wings can be more securely attached to it, and that it is possible
of developing very much better results.

[Illustration: Members of the Aëro Science Club]

[Illustration: Members of the Milwaukee and Illinois Model Aëro Clubs]

To construct such an A type frame 2 main sticks to serve as frame side
members are necessary and are made from spruce. Each member should be
36″ in length, ³⁄₈″ in depth by ¹⁄₄″ in width. By rounding the edges
and smoothing the various surfaces with sandpaper streamline effect
will be secured and will add to the efficiency of the machine as well
as to its appearance. When the side members are placed in A formation
the extremity of the sticks at which they meet should be so tapered
in the inner sides that when they meet and are permanently fastened
the result will be a continuance of the general streamline effect. The
permanent fastening of the frame side members at the point of the A
may be accomplished by using either strong fish glue or better, a good
waterproof glue and then have the jointure reinforced by securing a
piece of ³⁄₃₂″ steel wire 3″ in length and placing the center of it
at the point of the A, afterwards bending the wire along either outer
edge of the frame side members, putting as much pressure on the wire as
the strength of the structure will permit; after this the reinforced
jointure should have thread wound around it to insure even greater
strength. About ¹⁄₂″ of the wire on each side of the point should be
left clear and afterwards turned into a loop as shown in diagram 6, for
the purpose of attaching the hooks that hold the rubber strands. To
hold the side members apart at the rear end and for a propeller brace,
a piece of bamboo 10″ long, ¹⁄₈″ thick by ¹⁄₂″ in width is required
and this should be fastened to the extreme rear ends of the frame side
members, allowing the propeller brace to protrude on either side 1¹⁄₂″
as illustrated. To put the propeller brace in position a slot ¹⁄₂″ deep
by ¹⁄₈″ wide should be cut into the rear ends of the frame side members
for the reception of the propeller brace. After the brace has been
placed in position the outer edge should come flush with the rear ends
of the side members. To hold the brace in place thread and glue should
be used in the same manner as described for the point of the frame
side members. Between the point of the frame and the propeller brace
two bamboo pieces, one 9″ long and another 2¹⁄₃″ long, should be used
as braces for the general strengthening of the structure. The longest
piece should be secured across the top of the frame about 9″ from the
rear and the shorter piece about 9″ from the point.

[Illustration: Diagram 6]

When these two braces are in position the next matter that calls for
the attention of the constructor is the matter of getting into position
at the two outer extremities of the propeller brace bearings for the
propellers. For this purpose two pieces of ³⁄₃₂nd inch brass tubing,
each ³⁄₄th of an inch long, should be used, and should be fastened to
the underside of the propeller brace, at each extremity of that brace,
by the use of thread and glue. Sometimes greater efficiency is secured
by putting these pieces of bronze tubing about ¹⁄₄″ from the end. Some
model constructors make a very neat jointure here by soldering the
piece of tubing to a strip of thin brass, which is bent over the end
of the propeller brace and bound and glued thereon. In fastening the
bronze tubing to the propeller brace it should be so adjusted that it
will run parallel to the side members of the frame and will therefore
offer the least possible resistance to the shaft of the propeller when
the rubber strands have been attached.

When the frame has been completed a coat of shellac should be applied
to the entire structure to render it damp-proof.

ASSEMBLING

The proper assembling of the parts of the model is as essential to good
results as is the designing and making. Parts, although properly made,
if improperly placed in relation to each other will very often lead to
trouble. Therefore very great care must be exercised in the assembling
process.

When all the parts have been prepared and are ready to be assembled
the first thing that should be done is to mount the propellers in
position. This must be done very carefully on account of the fact
that the propeller shafts are easily bent and if bent the result is
considerable trouble, for such a bend in the propeller shaft will
cause the propeller to revolve irregularly with a consequent loss of
thrust. Before inserting the propeller shafts in the tubing 4 washers
each ¹⁄₄″ in diameter should be cut from hard metal, and a hole large
enough for the propeller shaft to pass through should be bored in the
center of each washer. The metal washers should be passed over the
straight ends of the shafts which extend from the rear of the tubing,
after they have been inserted in the tubing, and in this manner the
cutting into the hubs of the propellers which would follow is avoided.
The propellers are now to be mounted and this is accomplished by
allowing the ends of the shafts, which extend out from the rear of
the tubing, to pass through the hole in the hub of each propeller. In
mounting the propellers it is absolutely necessary to have the straight
edge of the propellers to face the point or front end of the model. The
propeller shown in Fig. 4 of diagram 1, should be mounted on the left
side of the frame to revolve to the left, while the propeller shown in
Fig. 1 should be mounted on the right side of the frame to revolve to
the right. When the propellers have thus been mounted the one-half inch
of shafting which extends out from the hubs of the propellers should be
bent over to grip the propeller hub and thereby prevent the shaft from
slipping during the unwinding of the rubber strands. For the reception
of the rubber strands to provide motive power a hook must be formed in
each shaft and this can be done by holding securely that portion of the
shaft which extends toward the point of the model, while the end is
being formed into a hook as illustrated in diagram 7.

[Illustration: Diagram 7]

Eighty-four feet of ¹⁄₈th″ flat rubber is necessary to propel the
model. This should be strung on each side from the hooks (see diagram)
at the front part of the model to the propeller shafts at the rear
of the model. In this way 14 strands of rubber will be evenly strung
on each side of the frame. To facilitate the winding of the rubbers
two double hooks made of ³⁄₃₂″ steel wire to resemble the letter S,
as shown in diagram 7, should be made. One end of this S hook should
be caught on the frame hook, while the other end is attached to the
strands of rubber, and to prevent the possible cutting of the strands a
piece of rubber tubing is used to cover over all wire hooks that come
in contact with the rubber strands providing propelling power.

The wings are mounted on the top side of the frame members by means
of rubber bands and in placing them upon the frame it should be noted
that the entering edge of each wing must face the point or front of
the model. The wings must be so adjusted on the frame that they result
in perfect side balance which means that there is an even amount of
surface on either side of the model. To secure a longitudinal balance
it will be found that the entering edge of the main wing should be
placed approximately 8″ from the propeller brace or rear of the model,
and the entering edge of the small wing or elevator approximately 6″
from the point. But it is only by test flying that a true balance
of the entire model can be obtained. To give the necessary power of
elevation (or lifting ability) to make the model rise, a small block of
wood about 1″ long by ¹⁄₄″ square must be placed between the entering
edge of the small wing and the frame of the model.

After the wings have been thus adjusted and a short test flight made to
perfect the flying and elevating ability of the model, and this test
flight has been satisfactory, the model is ready for launching under
its full motive power.

LAUNCHING

In the preliminary trials of a model close attention must be paid to
the few structural adjustments that will be found to be necessary
and which if not properly and quickly remedied will result in the
prevention of good flights or even in possible wrecking of the model.
Careful designing and construction are necessary but it is equally as
important that the model should be properly handled when it is complete
and ready for flying.

[Illustration: Charles W. Meyers and William Hodgins exhibiting models
of early design.]

[Illustration: Henry Criscouli and his five foot model. This model may
be disassembled and packed conveniently in small package.]

[Illustration: Harry G. Schultz hydroaëroplane.]

The approximate idea of the balance of a model can be secured by
launching it gently into the air. If the model dives down point first
it indicates that the main wing should be moved a little toward the
front. If it rises abruptly the main wing should be moved slightly
toward the rear. In this way by moving the wing forward or rearward
until the model glides away gracefully and lands flat upon the ground,
proper adjustment of the balance can be effected. If when launching
from the hand the model should curve to the left the main wing should
be moved slightly to the left of the frame members. And if the curve
is to the right the main wing should be moved in that direction. This
process can be continued until the model flies in the course desired.

The winding of the rubber strands to get the necessary propelling power
is an important detail. The model should be firmly held by some one
at the rear with the thumb on either side member, pressing down on
the jointure and with the four fingers of each hand gripping the under
side of the frame members, and in this way holding the model steady
and until the rubber strands have been sufficiently wound. With the
hands in this position the propellers, of course, cannot and should
not revolve. The hooks attached to the rubber strands at the point or
front of the model should be detached from the side members and affixed
to the hooks of the winder. A winder may be made from an ordinary egg
beater as is shown in diagram 8. When the hooks attached to the rubber
strands at the point of the model have been affixed to the winder the
rubbers should be stretched four times their ordinary length (good
rubber being capable of being stretched seven times its length) and
the winding commenced, the person winding slowly moving in towards the
model as the strands are wound. If the ratio of the winder is 5 to 1,
that is if the rubber is twisted five times to every revolution of the
main wheel of the winder, 100 turns of the winder will be sufficient
for the first trial. This propelling power can be increased as the
trials proceed. When the winding has been accomplished the rubber hooks
should be detached from the winder hooks and attached to the hooks at
the front of the side members as shown in the diagram.

[Illustration: Diagram 8]

In preparation for launching, the model should be held above the head,
one hand holding it at the center of the frame, the other in the center
of the propeller brace in such a way as to prevent the propellers
from revolving. When the model is cast into the air if it is properly
adjusted it will fly straight ahead.

A precaution which is sometimes worthy of attention before the
launching of the model under its full power is to test out the
propellers to find out whether or not they are properly mounted and
whether they revolve evenly and easily. To do this the rubber strands
may be given a few turns, enough to revolve the propellers for a brief
period, while the machine is held stationary. If the shafts have been
properly inserted in the hubs of the propellers and have not been
bent during the winding of the rubbers, the propellers will revolve
evenly and readily. If the propellers revolve unsteadily it indicates
that there is a bend in the propeller shafts or the propellers have
not been properly balanced. If the trouble is a bend in the shaft, it
must be removed before the model is launched on actual flight. If the
propeller does not revolve freely the application of some lubrication
(such as vaseline) to the shaft will eliminate this trouble. With these
adjustments made satisfactorily, the model can be launched with the
anticipation of good flying.

CHASSIS

The preceding instructions and discussions have dealt with different
parts of a simple model to be used as a hand-launched type of model.
The experience which will come as the result of flying this type of
model for a period will undoubtedly tend toward a desire on the part of
the constructor to make his model more nearly represent a large sized
aëroplane and will make him want to have his model rise from the ground
under its own power. Such a model is known as an R. O. G. type, that
is, rises off the ground.

[Illustration: Diagram 9]

To meet this desire all that it is necessary to do is to make a
chassis, or carriage, which can be secured to the frame of the model,
and with extra power added, will result in a practical R. O. G. model.
In constructing such a chassis or carriage it is necessary to bear
in mind that it must be made sufficiently strong to withstand the
shock and stress which it will be called upon to stand when the model
descends to the ground.

For the main struts of the chassis two pieces of bamboo each 9″ in
length are needed and these should be bent over 1″ on one end as shown
in the diagram, that they may be fastened to the under side of the
frame members, one on either side, at a point on that member 12″ from
the front. Two similar pieces of bamboo, each piece about 7″ in length,
are required to act as braces between the frame members and the main
chassis struts. Each end of each of the braces should be bent over in
the same direction and in the same manner as that described for the
main strut so that the fastening to the main frame member and the main
chassis strut may be accomplished. Steam may be used in bending the
ends of the pieces of bamboo. To make the landing chassis sufficiently
stable to withstand landing shocks a piece of bamboo 9″ should be
fastened from either side of the main chassis struts at the point where
the chassis brace on either side meets with main strut. The ends of
this cross brace should be bent in similar fashion to the other braces
to enable its being fastened easily and securely.

Two small wheels constitute the running gear for the front part of
the chassis, for which two pieces of ¹⁄₁₆″ steel wire each 2¹⁄₄″ long
are required. These small wires are fastened to the bottom ends of
the main struts, and to accomplish this the wire should be bent in
the center at right angles; one leg of the angle is attached to the
bottom end of the main strut as shown in the diagram. Disks for wheels
may be cut from a bottle cork which should be ³⁄₄″ in diameter by
approximately ¹⁄₄″ in thickness. The edges should be rounded off to
prevent chipping. Before mounting the wheels on the axles which have
been provided by the wires attached to the bottom of the main struts,
a piece of bronze tubing ³⁄₃₂″ inside diameter and ³⁄₁₆″ long should
be inserted in the center of each disk. To secure the least possible
resistance on the revolutions of the wheels, there should be placed on
the wire axles pieces of bronze tubing similar in diameter and ¹⁄₈″ in
length on either side of the wheel (see illustration). When the wheel
is thus placed in position with the pieces of bronze tubing on either
side about ¹⁄₄″ of the axle wire will extend from the outward end of
the outside piece of tubing. This should be bent over the tubing to
prevent its falling off and at the same time hold the wheel securely in
position.

For the rear skid a piece of bamboo 6″ long is used, one end of which
is curved as in a hockey stick so that it will glide smoothly over
the ground. The other end of the rear skid should be bent over about
¹⁄₂″ so that it can be securely fastened to the propeller braces,
as illustrated in the diagram. Two 7″ pieces of bamboo are required
to act as braces for the rear skid. Both ends of each brace strut
are bent over ¹⁄₂″ in the same direction, one end of each strut is
securely fastened to a side member 3″ from the rear and the other end
of each strut is fastened to the rear skid, at their point of meeting
as shown in diagram 9, the method of attaching being the same as in
the case of the forward portion of the chassis. All joining should be
accomplished by first gluing the braces and then binding with thread.
When completed, the rear skid should glide along the ground in bobsled
fashion, thus preventing the propellers from hitting the ground.

[Illustration: Diagram 10]

In making such a chassis or carriage the endeavor should be made to
use, as near as possible, the same weight of material on either side of
the model so as little interference as possible will be made with the
general balance of the model in flight.

PONTOONS

Having satisfactorily developed the hand launched model and the
model rising off the ground under its own propulsion the constructor
will next turn his mind to the question of having his model rise
under its own power from the surface of the water in the fashion of
passenger-carrying hydros and flying boats. This will be accomplished
by the use of pontoons attached to a specially designed chassis.

[Illustration: C. V. Obst World record flying boat]

[Illustration: Twin tractor Hydroaëroplane designed and constructed by
George F. McLaughlin]

[Illustration: Louis Bamberger’s hydro about to leave surface of water]

Three pontoons are necessary and these should be made as light as
possible. Each pontoon should be made 6″ long, 1″ deep toward the
forward part, by ³⁄₄″ at the rear and 2″ wide. The side members of
each pontoon are made from pieces of thin white pine wood ¹⁄₃₂nd of an
inch thick, slightly curved up at the front and sloped down toward the
rear. Small niches should be made on the top and bottom sides of the
pontoons into which the cross braces are inserted and glued. Further
reference to diagram 10 will show that at the extreme forward end of
the sides a cut is made large enough to receive a flat piece of spruce
¹⁄₁₆″ wide. Another cut of the same dimensions is made at the extreme
rear end. Still further cuts are made on the top and bottom sides of
the pontoons, the forward cuts measuring 1¹⁄₂″ from the front and the
rear cuts 1¹⁄₂″ from the rear, to join the sides of the pontoons as
illustrated in diagram 10. Six pieces of ¹⁄₁₆″ flat spruce are required
for the rear pontoon, the ends of which are held in position by glue.
For the forward pontoon only 4 braces are required in so far as the
ends of the two main brace spars of the forward part of chassis are
inserted in the cuts on the top sides of the pontoon. These brace spars
measure 10 inches in length and are made from bamboo ¹⁄₈th inch in
diameter, which necessitates enlargement of the cuts on the top sides
of the forward pontoons so that the extreme ends of the spars can be
inserted in the cuts in the place of the braces. To complete the rear
pontoon and prepare it for covering, three strips of ¹⁄₈″ bamboo are
required for struts. Two of these strips should measure 9″ in length
and should be attached to the front of the pontoon on the inner side
as shown in diagram 10. Thread and glue should be used in attaching
the ends of the strips to the pontoon. To enable fastening to the
frame the upper ends of the bamboo strips should be bent over about
¹⁄₂″. The third strip should measure 8″ in length and is attached to
the upper and lower braces toward the front of the pontoon as shown
in the diagram. It is necessary that this strip be secured in the
approximate center of the pontoon to insure a good balance. For the
purpose of securing the upper end of the third strut to the center of
the propeller brace a piece of wire 1¹⁄₂″ long should be secured to the
upper end of the strut and looped as shown in diagram 10. The three
pontoons should now be covered with fiber paper and it is necessary to
exercise care to avoid punctures. For the purpose of coating the fiber
paper to render it waterproof, a satisfactory solution can be made by
mixing banana oil with celluloid until it has attained the desired
thickness, after which it should be applied to the covering of the
pontoons with a soft brush.

For the main strut of the forward portion of the chassis two pieces of
¹⁄₈″ bamboo, each 11″ in length, are required and these should be bent
over 1″ on one end as shown in the diagram, that they may be fastened
to the under side of the frame members, one on either side at a point
on that member 11″ from the front. Two similar pieces of bamboo, each
piece 8″ in length, are required to act as braces between the frame
members and the main chassis struts. Each end of the braces should
be bent over in the same direction and in the same manner as that
described for the main struts so that the fastening to the main frame
member and the main chassis struts may be accomplished. Steam or an
alcohol lamp may be used in bending the ends of the pieces of bamboo.
To make the chassis sufficiently stable a piece of bamboo 7¹⁄₂″ should
be fastened from either side of the main chassis struts at the point
where the chassis brace on either side meets with the main strut. The
ends of this cross brace should be bent in similar fashion to the other
braces to enable its being fastened easily and permanently.

For the accommodation of the pontoons two strips of flat steel wire,
each 4″ in length, should be attached to the ends of the main struts,
about one inch from the bottom, the farthest ends should be bent to
grip the second spar which joins the pontoons. Note diagram 10.

To further strengthen the chassis a strip of flat steel wire
sufficiently long enough should be bent so that ¹⁄₂″ of the central
portion can be securely fastened to the center of the cross brace as
shown in diagram 10. The two outer ends should be bent down and are
fastened to the wires which are attached to the bottom ends of the
struts. This method of attaching the forward pontoons enables the
constructor to adjust them to any desired angle and also detach them
when not in use.

A model hydroaëroplane is one of the most interesting types of models
and if properly taken care of will afford the constructor many pleasant
moments.

[Illustration: Erwin B. Eiring about to release R. O. G. Model. (Note
manner of holding propellers.) Kennith Sedgwick, tractor record holder
Milwaukee Model Club. Courtesy Gilbert Counsell.]

[Illustration: Waid Carl releasing R. O. G. Model. Courtesy Edward P.
Warner.]

LAUNCHING AN R. O. G. OR MODEL
HYDROAËROPLANE

Although the method of determining the balance of an R. O. G. or a
model hydroaëroplane is exactly the same as that of a hand launched
model, the manner of launching is somewhat different. Instead of
holding the model one hand in the center of the frame and the other at
the rear as in the case of the hand launched model, in launching an R.
O. G. or hydro, the model should be rested upon the ground or water,
as the case may be, with both hands holding tightly to the propellers.
Then when about to let the model go release both propellers instantly.
If the model has sufficient power and it has been properly adjusted
it will glide over the surface of the ground or water for a short
distance, then rise into the air. Should the model fail to rise into
the air additional strands of rubber should be added, after which it
should be rewound and a second attempt made.

Should the model fail to respond after the addition of extra rubber,
the indications are that something requires further adjustment. Perhaps
the pontoons need further elevation if the model is a hydro, or if
it be an R. O. G. model the forward wing may require an increase of
elevation. In any event the model should be carefully examined and
adjustments made where necessary, after which the model should be
tested for balance and elevation. If satisfied with the behavior of the
model after test flights have been made, another attempt should be made
to launch the model from the ground or water.

On no account try to fly the model in the house, or see, supposing the
model is of the R. O. G. type, if it will rise from the dining room
floor. This advice may seem unnecessary, but it is not so, for there
has been quite a number of instances in which the above has been done,
nearly always with disastrous results, not always to the model, more
often to something of much greater value. The smashing of windows has
often resulted from such attempts, but generally speaking pictures
are the worst sufferers. It is equally unwise to attempt to fly the
model in a garden in which there are numerous obstructions, such as
trees and so forth. A wrecked model is very often the result of such
experimenting. The safest way to determine the flying ability of any
model is to take it out in an open field where its flight is less apt
to be interrupted.

WORLD RECORD MODELS

THE LAUDER DISTANCE AND
DURATION MODEL

After many months of experimentation Mr. Wallace A. Lauder succeeded in
producing a model that proved to be one of his most successful models.
But a few years ago flights of 1000 feet with a duration of 60 seconds
were considered remarkable. But so rapid has been the development of
the rubber strand driven model that to-day it is hardly considered
worth while to measure a flight of 1000 feet, especially in contests
where models fly over 2500 feet or 3537 feet which was the distance
flown by Mr. Lauder’s model during one of the contests of the National
Model Aëroplane competition of 1915. Mr. Lauder’s model on several
occasions made flights of over 3500 feet with a duration in each event
of over 195 seconds. It is therefore to be remembered that this model
is both a distance and duration model, both qualities being seldom
found in one model.

Reference to the accompanying drawing will give a clear idea of the
constructional details.

The frame or fuselage consists of two side members 40″ in length, of
straight grained spruce. At the center each member is of approximately
circular cross section, and is ¹⁄₄″ in diameter. The members taper to
about ³⁄₁₆″ at the ends, the circular cross section being maintained
throughout. The frame is braced by a strip of bamboo of streamline
form, extending from one side member to the other, 18″ from the apex of
the frame. The ends of this frame are bent to run parallel to the side
members of the frame where they are secured by binding with silk thread
and gluing. Piano wire hooks are also secured to the side members of
the frame adjacent the ends of the cross brace, and from these hooks
extend wires of steel (No. 2 music wire) which run diagonally to the
rear brace or propeller spar where they are secured.

[Illustration: Diagram 11]

The frame is braced further by an upwardly arched strip of bamboo, as
shown in diagram 11, this strip being 2¹⁄₂″ in height. At the top of
this brace are two bronze strips of No. 32 gauge brass, one above the
other, one on top of the brace and the other below.

Adjacent the ends of these strips of metal are perforations through
which pass bracing wires, one of which wires runs to the front of
the frame where a hook is mounted for its reception, and the other
two wires extend to the rear of the frame where they are secured
to the propeller brace. The propeller brace consists of a strip of
streamlined spruce 11³⁄₄″ in length, the propellers being at an angle,
thus clearance is allowed ¹⁄₄″ wide at the center, tapering to ³⁄₁₆″
at the ends. The ends of the propeller brace extend out one inch from
the side members of the frame, to allow room for the rubber strands to
be used as motive power. In order to avoid slotting the ends of the
side members of the frame so that the propeller brace can be secured
therein, thin strips of bamboo are secured above and below the end of
each side member, by binding with silk thread and gluing, the space
between these bamboo strips being utilized for the brace which is
securely bound and glued therein. The propeller bearings consist of
strips of very thin bronze (No. 32 gauge), about ³⁄₁₆″ in width, bent
over ⁵⁄₈″ strips of German silver tubing, the tubing being soldered to
the bronze strips and the propeller brace, which fits between the upper
and lower portions of the bronze strips, is securely bound and glued
thereto.

The propellers are cut from solid blocks of pine, and are 12″ in
diameter. The blade, at its widest portion, measures 1³⁄₈″. The blades
are cut very thin, and in order to save weight, they are not shellacked
or painted.

The propeller shafts are of piano wire (No. 20 size) to fit the tubing
used in the bearings, pass through the propellers and are bent over
on the outer side to prevent turning. A few small bronze washers are
interposed between the propellers and the outer ends of the tubing to
minimize friction when the propellers are revolving. Twelve strands of
rubber are used for each propeller, the rubber being ¹⁄₈″ flat.

[Illustration: Wallace A. Lauder distance and duration model]

[Illustration: Wallace A. Lauder R. O. G. Model]

The wings are both double surfaced, and are of the swept back type. The
span of the main wing is 28¹⁄₂″, with a chord of 6¹⁄₂″. The elevator
has a span of 15″ with a chord of 4³⁄₄″. The main wing has eleven
double ribs, these ribs being built up on mean beams of spruce ¹⁄₁₆″ ×
³⁄₁₆″, the front beam being placed 1¹⁄₄″ from the entering edge, and
the second beam being 2″ back from the front beam. The entering and
trailing edges are formed from a single strip of thin split bamboo, all
the joints being made by binding with thin silk and gluing.

The elevator is constructed in like manner, except that it only has
seven ribs, and the measurements are as above set forth. Both planes
are covered with goldbeater’s skin, sometimes known as “Zephyr” skin,
which is first glued in place and then steamed, which tightens the same
on the plane, and given a coat of preparation used for this purpose.

THE HITTLE WORLD RECORD
MODEL

(SINGLE TRACTOR MONOPLANE, 116 seconds
DURATION RISING FROM WATER)

The Hittle World record model hydroaëroplane, designed and constructed
by Mr. Lindsay Hittle of the Illinois Model Aëro Club, is perhaps
one of the most interesting types of models yet produced. The
establishing of this record illustrates the value of careful designing
and construction and offers to the beginner an example which might
be followed if good results are sought. In having broken the world’s
model hydroaëroplane record with a tractor type model Mr. Hittle
accomplished a feat of twofold importance. First, in having advanced
the possibilities of the tractor model, and, second, in illustrating
the value of scientific construction. The previous record for this
type of model has been but 29 seconds, just one-fourth of the duration
made by Mr. Hittle’s model.

Mr. Hittle’s model shows many new and original features not hitherto
combined on any one model. Note diagram 12. The model is of extremely
light weight, weighing complete but 1.75 ounces. The floats and their
attachments have been so designed as to offer the least possible wind
resistance. In fact every possible method was utilized in order to cut
down weight and resistance on every part of the model. As a result of
this doing away with resistance an excellent gliding ratio of 8³⁄₄ to 1
has been obtained.

For the motor base of the model a single stick of white pine ⁵⁄₆″
deep and 45″ in length is used. On the front end the bearing for the
propeller is bound with silk thread and a waterproof glue of the
constructor’s own composition being used to hold it secure. For the
bearing a small light weight forging somewhat in the shape of the
letter “L” is used, this being made streamline. At the rear end of
the engine base is attached a piano wire hook for the rubber. The
stabilizer consisting of a segment of a circle measuring 12″ × 8″ is
attached to the under side of the engine base. The rudder measuring
3¹⁄₂″ × 3¹⁄₂″ is attached to the stabilizer at the rear of the engine
base.

The wing is built up of two beams of white pine with ribs and tips of
bamboo and has an area of 215 square inches.

The wing which has a total span of 43″ and a chord of 5¹⁄₈″ is built up
of two beams of white pine with ribs and tips of bamboo and has a total
area of 215 square inches. The wing is given a small dihedral and the
wing tips are slightly upturned at the rear.

The trailing edge is longer than the entering edge the ribs being
placed somewhat oblique in order to secure an even spacing. The wing is
attached to the frame by two small bamboo clips which hold it rigidly
and permit easy adjustment and is set at an angle of about 4 degrees
with the line of thrust.

[Illustration: Diagram 12]

Both the floats which take practically the whole weight of the machine
are situated directly under the wing just far enough behind the center
of gravity to prevent the model from tipping backward. These floats
are attached to the engine base by means of streamlined bamboo struts.
Bamboo is also used in the construction of the float frames. A single
float of triangular sections is situated just behind the propeller. The
entire weight of the floats and their attachments is but .23 ounces.

The propeller which consists of four blades is built up of two
propellers joined together at the hubs and securely glued, the
completed propeller having a diameter of 10″ with a theoretical pitch
of 14″. The blades are fairly narrow, tapering almost to a point at the
tips. The propeller is driven by five strands of ³⁄₁₆th″ strip rubber
at about 760 r.p.m. when the model is in flight. At the time when
the model made its record flight of 116 seconds the rubber was given
1500 turns which is not the maximum number of turns. At other times
the model has flown satisfactorily with less turns of the rubber.
While in the air the model flies very slow and stable notwithstanding
its light weight and large surface. On three occasions the model has
made durations of approximately 90 seconds which rather dispenses the
possibility of its being termed a freak.

THE LA TOUR FLYING BOAT

One of the most notable results of the National Model Aëroplane
Competition of 1915 was the establishing of a new world’s record for
flying boats. Considering that the model flying boat is a difficult
type of model to construct and fly, the establishing of this new world
record of 43 seconds is remarkable. Credit for this performance is
due Mr. Robert La Tour of the Pacific Northwest Model Aëro Club, who
designed, constructed and flew the model flying boat which is herewith
described and illustrated. Diagram 13.

The frame is made of laminated spruce 40″ in length, made of two strips
glued together. They are ³⁄₈″ × ¹⁄₈″ at the center tapering to ³⁄₁₆″ ×
¹⁄₈″ at the ends. The cross braces are of split bamboo and are fastened
to the frame side members by bringing them to a wedge at the ends and
then inserting them into slots in the sides of the frame side members
and are finally drilled and bound to the latter. The rear brace is
of streamlined spruce ¹⁄₄″ × ¹⁄₈″; this butts against the frame side
members and is bound to them. The propeller accommodations are made of
brass.

The propellers are 10″ in diameter with a 19″ pitch. These are carved
from a block of Alaska cedar 1¹⁄₄″ wide by ³⁄₄″ thick. Of course the
propellers may also be made from white pine. To turn the propellers 15
strands of ¹⁄₈″ flat rubber are used.

Bamboo about ¹⁄₁₆″ square is used to obtain the outline of the wings.
The main wing has a span of 33″ with a chord of 5¹⁄₂″. Split bamboo
is used for the making of the 9 ribs. The wing spar or brace is of
spruce ³⁄₁₆″ × ¹⁄₈″ and is fastened below the ribs as illustrated in
diagram 13. The elevator is constructed in like manner but has a span
of only 17″ × 4³⁄₄″ and has only 5 ribs. A block ³⁄₄″ high is used for
elevation. Both wings have a camber of ¹⁄₂″ and are covered on the
upper side with silk doped with a special varnish and a few coats of
white shellac.

[Illustration: Diagram 13]

The boat is 20″ long, 3″ in width and shaped as shown. The slip is
¹⁄₂″ deep and is located 7″ from the bow. The rear end is brought down
steeply to avoid the drag of the water on this point when the boat is
leaving the surface of the water. Spruce ³⁄₆₄ths of an inch thick is
used for the making of the sides, but the cross bracing is of slightly
heavier material, there being six braces used throughout. The rear
brace is much heavier in order to withstand the pull of the covering
and to receive the ends of the wire connections. The outriggers or
balancing pontoons are constructed of the same material as that of the
boat and are held together by a spruce beam 18″ long, ¹⁄₂″ wide by
³⁄₁₆″ thick, streamlined. This beam is fastened to the boat by means
of three brads to permit changing if necessary. The lower edges of the
outriggers should clear the water about ¹⁄₈″ before the steps on the
boat leave the water. The boat and outriggers are covered with silk,
shrunk with a special solution and then coated several times with white
shellac. It is a good plan to shellac the interior walls of the boat
and pontoons before covering to prevent them from losing their form by
becoming soft from the influence of water in the case of a puncture.

The boat is connected to the frame at its front by two steel wires,
their ends being inserted into the cross members of the boat, and then
brought up along the sides, crossed and then bound to the frame. A
similar pair of connecting wires are used to connect the rear end of
the boat to the rear end of the frame. A U-shaped wire is bound to the
outrigger beam and frame. A single diagonal strip of bamboo is also
fastened to the outrigger beam with a brad, its upper end being bound
to the cross bracing of the frame, making a very solid connection.

Under ideal weather conditions this model will fly on 12 strands of
rubber with the possibility of a better duration than has been made.
But, however, with 15 strands the model will rise at every attempt.
More rubber, however, causes the bow of the boat to nose under and to
accommodate this increase of power the boat should be lengthened.

THE COOK NO. 42 WORLD
RECORD MODEL

(TWIN PROPELLER HYDROAËROPLANE, 100.6
SECONDS RISING FROM WATER)

During the National Model Aëroplane Competition of 1915 held under
the auspices of the Aëro Club of America, a number of new world
records were established, one of which was for twin propeller
hydroaëroplanes. The credit for this record is due Mr. Ellis C. Cook
of the Illinois Model Aëro Club, who succeeded in getting his model
hydroaëroplane—which by the way is a rather difficult type of model to
operate—to rise from the water and remain in the air for a duration
of 100.6 seconds. This model is of the common A frame design with the
floats or pontoons arranged in the familiar fashion, two forward and
one aft. The model is fairly light, weighing, when complete, 3.33
ounces, ¹⁄₂ ounce of which is made up in rubber strands for motive
power. Diagram 14.

The frame is made of two sticks of white pine for side members, each
member measuring 38¹⁄₄″ in length, ⁵⁄₁₆″ in depth, by ¹⁄₈″ in width.
These are cut to taper toward the ends where they are only ¹⁄₈″ in
width by ³⁄₁₆″ in depth in the front and rear respectively. Three “X”
strips of streamlined bamboo measuring ³⁄₁₆″ in width by ³⁄₆₄ths of an
inch in depth, are used for bracing the frame between the front and
rear and are arranged as shown in diagram 14. The propeller bearings
are of small streamlined forgings of light weight, and are bound to the
rear end of each side member first by gluing, then binding around with
thread. The front hook is made of No. 16 piano wire and is bound to the
frame as shown in diagram 14. The chassis which holds the floats or
pontoons is made of ³⁄₃₂″ bamboo bent to shape and bound to the frame
members. By the use of rubber strands the floats are attached to the
chassis; the forward ones being attached so that angle may be adjusted.

The main wing has a span of 36″ and a chord of 5″ and is constructed of
two white pine beams each 39″ long, with bamboo wing tips. The ribs,
seven in number, are also made of bamboo and are spaced along the edges
of the wing at a distance of 4¹⁄₂″ apart. The “elevator” or front wing
has a span of 14″ and a chord of 3¹⁄₄″, the framework of which is made
entirely of bamboo. The entering edge of this wing is given a slightly
greater dihedral so that the angle of incidence at the tips is greater
than at the center. By this method the added incidence in the front
wing is obtained. By the use of rubber bands both wings are attached to
the frame.

[Illustration: Diagram 14]

The two forward floats are spaced eight inches apart and are of the
stepped type, the step being 3¹⁄₂″ from the front and has a depth of
¹⁄₈″. These two floats are separated by two bamboo strips as shown
in the diagram, which are tied to the rounded portion of the under
carriage by small rubber bands. By the sliding of these strips back
and forth the necessary angle of the floats may be obtained to suit
conditions. The floats are built up with two thin pieces of white pine
for sides, separated by small pieces of wood about one-half the size
of a match in cross section. Chiffon veiling which is used for the
covering of the wings, is also used for the covering of the floats,
after which it is covered with a special preparation to render both the
wings and the floats air and water-tight.

The two ten-inch propellers with which the model is fitted have a
theoretical pitch of twelve and one-half inches. The propellers are
carved from blanks one-half inch thick, the blades of the completed
propellers having a maximum width of one inch at a radius of three
inches. The propeller shafts are made from No. 16 piano wire and have
small washers for bearings. Each propeller is driven by three strands
of ¹⁄₄″ strip elastic. The rubber is given 1700 to 1750 turns and
revolves the propellers at 1150–1200 r.p.m., when the model is in
flight.

The model usually runs over the surface of the water for a distance of
from two to three feet before it rises, after which it climbs at a very
steep angle to the necessary altitude. The model seems, when in flight,
to be slightly overpowered but this is misleading. The rubbers usually
unwind in from 85 to 90 seconds. On four out of six flights this model
has made a duration of between 98 and 100 seconds which is rather
unusual for a model of this type.

THE RUDY FUNK DURATION MODEL

Of the many different types of duration models that have made their
appearance during the year of 1915 perhaps the model described
herewith, constructed and flown by Mr. Rudolph Funk, of the Aëro
Science Club, was one of the most successful. Unlike most models the
propellers of this model are bent and not cut. This model made its
appearance during the latter part of 1915, on several occasions having
flown for over 100 seconds duration. Diagram 15.

While retaining the important characteristics of his standard model,
slight changes have been made. Instead of the usual wire for the
construction of the frame of the wings, bamboo is used in its place for
lightness and strength. The wing frames are single surfaced, China
silk being used for covering. The “dope” which is used to render the
silk airtight is made by dissolving celluloid in banana oil. This in
turn is applied to the silk with a soft brush.

The camber of the main wing is ³⁄₄″ at the center, with a slight
reduction towards the negative tips; it also has a dihedral angle of 2
degrees. The main beam, which is secured to the under side of the frame
for rigidness, is of spruce 1″ by ⁵⁄₆₄″, tapering to ³⁄₄″ × ⁵⁄₆₄″.
The ribs for the main wing and small wing or “elevator” are cut from
solid pieces of bamboo ³⁄₁₆″ thick by ¹⁄₄″ wide. These pieces of bamboo
are first bent to the proper camber and are then cut into strips each
¹⁄₁₆″ wide. The ribs are next tapered to a V at the bottom, toward the
trailing edge, as shown in diagram 15, and also toward the entering
edge. To accommodate the entering and trailing edges of the frame, each
rib is slit slightly at both ends. Both edges of the frame are then
inserted in the slots at the ends of the ribs and bound around with
silk thread.

[Illustration: Diagram 15]

The frame is composed of two sticks of silver spruce 38″ in length,
⁵⁄₁₆″ × ³⁄₁₆″, tapering to ¹⁄₄″ × ⁵⁄₃₂″, held apart by a streamline
bamboo cross brace in the center. An additional brace of bamboo is
securely fastened across the frame toward the front. The propeller
brace consists of a streamline-cut piece of bamboo 12¹⁄₂″ in length
by ³⁄₈″ in width at the center, tapering to ¹⁄₄″ toward the ends. The
propeller brace is inserted in slots cut in the rear ends of the frame
members, then bound and glued.

The propellers are bent from birch veneer, the bending being done
over an alcohol flame as illustrated in diagram 15. But first of all
the blades are cut to shape, sandpapered and finished before they are
bent. As shown in the drawing a slot is filed in the hub of each blade
to enable the propeller shaft to pass through when both have been
glued together. The blades are then glued and bound together, first by
placing a piece of wire in the slots to insure their being centered and
also to prevent their being filled with glue. After this has been done
each propeller is given three coats of the same dope as is used on the
wings.

The propeller bearings are turned out of ¹⁄₃₂″ bronze tubing, the
length of each bearing being ¹⁄₂″. Steel washers are slipped over the
propeller shaft, between the bearing and propeller to insure smooth
running. The propeller shafts are made from steel hatpins which are
heated at both ends, one end of which is bent into a loop to receive
the rubber strands, the other end being bent around the hub of the
propeller to prevent the shaft from slipping during the unwinding of
the rubbers. Two strips of brass, each ¹⁄₄″ × 2″, are bent around the
one-half inch bearing and soldered. The brass strips are then glued and
bound onto the ends of the propeller brace as shown in diagram 15.

[Illustration: Rudy Funk speed model]

[Illustration: Schober compressed air driven monoplane. McMahon
compressed air driven tractor (right)]

THE ALSON H. WHEELER WORLD RECORD MODEL

(TWIN PUSHER BIPLANE 143 SEC. DURATION
RISING FROM THE GROUND)

Since the beginning of model flying very little attention has been
paid to the model biplane. Practically all records are held by
model aëroplanes of the monoplane type. With this fact in view, the
record established by Mr. Wheeler with his Twin Pusher Biplane is
extraordinary, in so far as it surpasses many of the monoplane records.
This model is a very slow flyer, and has excellent gliding ability. At
the time when this model flew and broke the world’s record, the greater
portion of the flight consisted of a beautiful glide of 86 seconds’
duration, after the power gave out, making it possible for the model to
remain in the air for a duration of 143 seconds.

The frame consists of two I-beams, each 48″ in length, running
parallel, and spaced by cross pieces, each piece 11¹⁄₂″ long. The
bearing blocks used made it possible for the propellers to clear by
one-half inch. Two 12″ expanding pitch racing propellers are used and
these are mounted on ball bearing shafts. The main upper plane has a
span of 34″ with a chord of 5″, the lower plane being 26″ by 5″. The
elevator consists of two planes, each measuring 14″ by 5″. Cork wheels
are used, each being one inch in diameter. For motive power one-eighth
inch flat rubber is used, this being coated with glycerine to prevent
sticking.

[Illustration: Alson H. Wheeler twin pusher Biplane]

[Illustration: C. V. Obst tractor model]

A MODEL WARPLANE

The model shown in the accompanying photograph was constructed by
Master R. O’Neill, of Montreal, Canada. The machine was designed
after one of the leading warplanes now in active service abroad and
in carrying out the entire features he did not fail to include the
identification marks which are of utmost importance in the war zone.

The dimensions of the model are as follows: Length of fuselage, 23″;
span of top wing, 33″; span of lower wing, 29″, both having a chord of
7″. Motive power is derived from two ¹⁄₈ inch square elastic strands
which operate a multiple gear to which is attached a 10″ propeller.

In coloring the model a dull aluminum was selected. Complete the model
weighs 12 ounces. Perhaps the most interesting feature of the model
is the ability to change it to a monoplane by the removal of the
upper wing after which the lower wing is raised to the sockets in the
fuselage which were especially arranged for that particular purpose.

[Illustration: Model warplane]

A SIMPLE COMPRESSED AIR ENGINE

During the past few years model flyers in America have shown a tendency
toward the adoption of compressed air engines for use in connection
with model aëroplanes. Hitherto, England has been the home of the
compressed air engine, where a great deal of experimenting has been
carried on, to a considerable degree of success. Flights of over 40
seconds have been made with models in which compressed air power plants
were used. But, however, the desire on the part of a large majority of
model flyers in America to build scientific models, that is, models
more closely resembling large machines, has made it necessary to find a
more suitable means of propulsion; rubber strands being unsatisfactory
for such purposes. Many different types of compressed air engines have
made their appearance during the past few years, among which the two
cylinder opposed type is very favorably looked upon, because it is
perhaps one of the easiest to construct.

To make a simple two cylinder opposed compressed air power plant, as
illustrated in Figure 1 of diagram 16, it is not necessary that the
builder be in possession of a machine shop. A file, drill, small gas
blow torch and a small vise comprise the principal tools for the making
of the engine.

The first things needed in the making of this engine are cylinders.
For the making of the cylinders two fishing rod ferrules, known as
female ferrules, are required. And for the heads of the cylinders, two
male ferrules are required. Such ferrules can be secured at most any
sporting goods store. The female ferrules should be filed down to a
length of 2″, cut down on one side a distance of ³⁄₄ of the diameter,
then cut in from the end as shown in Figure 7. When this has been done
the two male ferrules should be cut off a distance of ¹⁄₈″ from the top
as shown in Figure 7-a, to serve as heads for the cylinders.

[Illustration: Diagram 16]

A hole ¹⁄₈″ in diameter should be drilled in the center of each head
so as to enable the connecting of the intake pipes. By the use of soft
wire solder the heads should be soldered into the ends of the cylinders
as shown in Figure 1-d.

The pistons should now be made; for this purpose two additional male
ferrules are required. These should be made to operate freely within
the cylinders by twisting them in a rag which has been saturated with
oil and upon which has been shaken fine powdered emery. When they have
been made to operate freely they should be cut down one-half inch
from the closed end as shown in Figure 5-a. For the connecting rods,
2 pieces of brass tubing, each ¹⁄₈″ in diameter by 1¹⁄₄″ long, are
required, and, as illustrated in Figure 6, should be flattened out at
either end and through each end a hole ³⁄₃₂″ in diameter should be
drilled. For the connecting of the piston rods to the pistons, studs
are required, and these should be cut from a piece of brass rod ¹⁄₄″ in
diameter by ¹⁄₂″ in length. As two studs are necessary, one for each
piston, this piece should be cut in half, after which each piece should
be filed in at one end deep enough to receive the end of the connecting
rod. Before soldering the studs to the heads of the pistons, however,
the connecting rods should be joined to the studs by the use of a steel
pin which is passed through the stud and connecting rod, after which
the ends of the pin are flattened, to keep it in position as shown in
Figure 5-a.

For the outside valve mechanism and also to serve in the capacity as a
bearing for the crankshaft, a piece of brass tubing ¹⁄₄″ in diameter by
1¹⁄₂″ long is required. Into this should be drilled three holes, each
¹⁄₈″ in diameter, and each ¹⁄₂″ apart as shown in Figure 4. Next, for
the valve shaft and also propeller accommodation, secure a piece of
³⁄₁₆″ drill rod 2″ long. On the left hand side of the valve shaft, as
shown in Figure 3, a cut ¹⁄₃₂″ deep by ¹⁄₂″ in length is made 1″ from
the end. Another cut of the same dimensions is made on the right side
only; this cut is made at a distance of ³⁄₈″ from the stud end.

As shown in Figure 1-f, the crank throw consists of a flat piece of
steel, ³⁄₃₂″ thick, ³⁄₈″ in length by ¹⁄₄″ in width. At each end of the
crank throw a hole ³⁄₁₆″ in diameter should be drilled, the holes to
be one-half inch apart. Into one hole a piece of steel drill rod ³⁄₃₂″
in diameter by ¹⁄₄″ long is soldered, to which the connecting rods are
mounted, as shown in Figure 1-f. Into the other hole the stud end of
the crank throw is soldered.

[Illustration: Schober pusher type compressed air driven monoplane]

[Illustration: Schober compressed air driven biplane]

Before making the tank it is most desirable to assemble the parts of
the engine, and this may be done by first fitting the pistons into the
cylinders as shown in Figure 1-b, after which the cylinders should be
lapped one over the other and soldered as shown in Figure 1-a. When
this has been done a hole one-fourth of an inch in diameter should be
drilled half way between the ends of the cylinders, and into this hole
should be soldered one end of the valve casing shown in Figure 4. For
the inlet pipes as shown in Figure 1-c secure two pieces of ¹⁄₈″ brass
tubing and after heating until soft, bend both to a shape similar
to that shown in Figure 1-c. When this has been done solder one end to
the end of the cylinder and the other in the second hole of the valve
shaft casing. The valve shaft should now be inserted in the valve shaft
casing and the connecting rods sprung onto the crank throw as shown
in Figure 1-d. To loosen up the parts of the engine which have just
been assembled it should be filled with oil and by tightly holding the
crankshaft in the jaws of a drill the engine can be worked for a few
minutes.

The tank is made from a sheet of brass or copper foil 15″ long by
¹⁄₁₀₀₀″ thick. This is made in the form of a cylinder, the edges of
which are soldered together as shown in Figure 2. Sometimes this seam
is riveted every one-half inch to increase its strength, but in most
cases solder is all that is required to hold the edges together. For
the caps, or ends, the tops of two small oil cans are used, each can
measuring 2¹⁄₂″ in diameter. To complete the caps two discs of metal
should be soldered over the ends of the cans where formerly the spouts
were inserted, the bottoms of the cans having been removed. The bottom
edges of the cans should be soldered to the ends of the tank as shown
in Figure 2. Into one end of the completed tank a hole large enough
to receive an ordinary bicycle air valve should be drilled. Figure 2.
Another hole is drilled into the other end of the tank, into which is
soldered a small gas cock to act as a valve. Figure 2. This should be
filed down where necessary, to eliminate unnecessary weight. To connect
the tank with the engine, a piece of ¹⁄₈″ brass tubing 3″ long is
required, the ends of which are soldered into the holes in the valve
shaft casing nearest the cylinders, as shown in Figure 1-ee. As shown
in Figure 1-ee, a hole ¹⁄₈″ in diameter is drilled in one side of this
piece, but not through, in the end nearest the tank. Another piece of
brass tubing ¹⁄₈″ in diameter is required to connect the tank with
the engine, one end of which is soldered to the cock in the tank, the
other in the hole in the pipe which leads from the engine to the tank,
illustrated in Figure 1-ee, thus completing the engine.

In conclusion it is suggested that the builder exercise careful
judgment in both the making and assembling of the different parts
of the engine in order to avoid unnecessary trouble and secure
satisfactory results. After having constructed an engine as has just
been described, the constructor may find it to his desire to construct
a different type of engine for experimental purposes. The constructor
therefore may find the descriptions of satisfactory compressed air
engines in the following paragraphs of suggestive value.

COMPRESSED AIR DRIVEN MODELS

The development of the compressed air engine has given an added impetus
to model making, necessitating more scientific experimenting and
developing the art of model flying along lines of greater value to
those who may eventually take up the work of building our future air
fleets.

THE DART COMPRESSED AIR DRIVEN MODEL

In the accompanying illustration is shown a model aëroplane of
monoplane type driven by a three-cylinder rotary engine which was
constructed by Edward Willard Dart of South Norwalk, Connecticut.

The engine was constructed after several months of patient labor.
Careful judgment was exercised in the drafting of the plane and
likewise in the assembling of the engine for it is absolutely
essential that all parts be properly fitted as to enable the engine to
run smoothly. In designing the wings every detail was taken into
consideration to insure good flying.

[Illustration: Model by Edward Willard Dart]

The main wing has a spread of 58″ and 7″ in chord. The elevator
measures 23″ in spread and 6″ in chord. In the construction of both
wings bamboo ribs are used, the frames being covered over with China
silk and coated with celluloid solution. The main wing is made in two
sections to facilitate quick adjustment to the fuselage.

THE MCMAHON COMPRESSED AIR DRIVEN MONOPLANE

One of the latest developments in the field of model flying is the
McMahon compressed air driven monoplane. This model was built to be
used as either a tractor or pusher, but in view of its ability to
balance more easily as a pusher most of the experiments have been
carried out on this machine as a pusher. The machine in itself is
simple and inexpensive to construct, the chief portion of the expense
being involved in the making of the engine. By using the machine as a
pusher a great deal of protection is afforded both the propeller and
engine, and this protection helps to avoid damaging the propeller or
engine, which would mean an additional expenditure for repairs, thus
minimizing the cost of flying the model.

The frame has been made to accommodate both the tank and engine, and
this is done by using two 30″ strips of spruce, each ¹⁄₄″ wide by ³⁄₈″
deep, laid side by side, a distance of three inches apart, up to within
10″ of the front, as shown in the accompanying photograph. No braces
are used on the frame, as the tank, when securely fastened between the
frame, acts in that capacity.

The wings are made in two sections, each section measuring 24″ in span
by 8″ in chord, consisting of two main spars, ³⁄₁₆″ in diameter, one
for the entering edge and one for the trailing edge. To these edges, at
a distance of three inches apart, are attached bamboo ribs, 18 in all,
each measuring 8″ in length by ¹⁄₈″ in width by ¹⁄₁₆″ thick. The wings
are round at the tips, and have a camber of approximately one-half
inch, but they are not set at an angle of incidence. Light China silk
is used for covering and after being glued over the top of the wing
frame is given two coats of dope to shrink and fill the pores of the
fabric. A good “dope” for the purpose can be made from celluloid
dissolved in banana oil. The wing sections are attached to the frame
and braced by light wire. The forward wing or “elevator” is made in the
same manner as the main wing, but should measure only 18″ × 3″. Instead
of being made in two sections as the main wing, the forward wing is
made in one piece.

The chassis is made by forming two V struts from strong steel wire
sufficiently large enough so that when they are attached to the frame
of the model the forward part will be 9″ above the ground. One V strut
is securely fastened to either side of the frame, at a distance of 8″
from the front. A 7″ axle is fastened to the ends of these struts. On
the axle are mounted two light wheels, each about 2″ in diameter. The
chassis is braced by light piano wire.

The rear skid is made in the same manner as the forward skid, only
that the ends of the struts are brought together and a wheel 1 inch in
diameter is mounted at the bottom ends by means of a short axle. The
struts are not more than 7¹⁄₂″ long, thus allowing a slight angle to
the machine when it is resting upon the ground.

[Illustration: John McMahon and his compressed air driven monoplane]

[Illustration: Frank Schober preparing his model for flight. Gauge to
determine pressure of air may be seen in photograph]

The machine complete does not weigh over 7 ounces. The power plant
used in connection with this model is of the two cylinder opposed
engine type, with tank such as has just been described in the foregoing
chapter.

The tank is mounted in the frame by drilling a ¹⁄₁₆″ hole through
either end of the tank, through which a drill rod of this diameter can
be inserted. About ³⁄₄ths of the drill rod should extend out on each
side of the tank, to permit the fastening of the tank to the frame
side members. This method of mounting the tank serves two purposes to
a satisfactory degree. First, it permits secure fastening; second, as
the rods are passed through the side and cap of the tank they help
materially in preventing the caps from being blown off in the event of
excessive pressure.

THE MCMAHON COMPRESSED AIR DRIVEN BIPLANE

In the McMahon model we find a very satisfactory type of compressed
air driven model. On several occasions this model has made flights of
over 200 feet with a duration of between 10 and 15 seconds, and the
indications are that by the use of a more powerful engine the model can
be made to fly a greater distance, with a corresponding increase of
duration. The engine used in connection with the model is of the two
cylinder opposed type, such as described in the foregoing paragraphs.
The tank, however, is somewhat different in design from that just
described, it having been made of 28 gauge sheet bronze, riveted every
one-half inch. The two long bolts that hold the steel caps on either
end of the tank also serve as attachments for the spars that hold the
tank to the engine bed, as shown in diagram 17. The tank has been
satisfactorily charged to a pressure of 200 lbs. per square inch, but
only a pressure of 150 lbs. is necessary to operate the engine. The
tank measures 10″ in length by 3″ in diameter and weighs 7 ounces.

The wings of this machine are single surfaced and covered with fiber
paper. The top wing measures 42″ in span by 6″ in chord. The lower
wing is 24″ by 6″. The wings have a total surface of 396 square inches
and are built up of two ³⁄₁₆″ dowel sticks, flattened to streamline
shape. Only two sets of uprights separate the wings, thus adding to the
streamline appearance of the machine.

Both tail and rudder are double surfaced and are built entirely of
bamboo for lightness, the tail being made in the form of a half circle
measuring 12″ by 8″. Steel wire is used on the construction of the
landing chassis, the chassis being so designed as to render it capable
of withstanding the most violent shock that it may possibly receive
in landing. The propeller used in connection with the model is 14″ in
diameter and has an approximate pitch of 18″.

[Illustration: Diagram 17]

COMPRESSED AIR ENGINES

THE WISE COMPRESSED AIR ENGINE

Although of peculiar construction, the Wise rotary compressed air
engine offers a very interesting design from a viewpoint of ingenuity.
This engine embodies a number of novel features not hitherto employed
in the construction of compressed air engines, and in view of the fact
that the majority of compressed air engines are made on the principle
of the opposed type, this engine suggests many possibilities for the
rotary type engine.

The engine consists of five cylinders and weighs four ounces, including
the propeller and mounting frame. On a pressure of 15 lbs. the engine
will revolve at a speed of 1000 r.p.m. The connecting rods are fastened
to the crankshaft by means of segments and are held by two rings,
making it possible to remove any one piston without disturbing the
others. This is done by simply removing a nut and one ring. The crank
case is made from seamless brass tubing, into which the cylinders are
brazed. The valve cage and cylinder heads are also turned separately
and brazed. One ring only is used in connection with the pistons. The
cylinders have a bore of ¹¹⁄₃₂″, with a piston stroke of ⁷⁄₁₆″. In
view of the fact that pull rods show a greater tendency to overcome
centrifugal force, they are used instead of push rods to operate the
valves. The crankshaft has but one post, which is uncovered in turn by
each inlet pipe as the engine revolves. The “overhang” method is used
to mount this engine to the model. With the exception of the valve
springs, the entire engine, including the mounting frame and tank, is
made of brass.

[Illustration: Wise five cylinder rotary compressed air engine]

THE SCHOBER-FUNK COMPRESSED AIR ENGINE

Two of the most enthusiastic advocates of the compressed air engine
for use in model aëroplanes are Messrs. Frank Schober and Rudolph
Funk, both members of the Aëro Science Club. For a number of months
both these gentlemen have experimented with compressed air engines of
various designs, until they finally produced what is perhaps one of
the most satisfactory rotary engines now in use, from a standpoint of
simplicity and results.

[Illustration: Schober-Funk three cylinder rotary engine]

As can be seen from the accompanying illustration, this little
engine is remarkably simple in appearance. The engine complete, with
equipment, weighs at the most but 14 ounces. The cylinders, three in
all, are stamped from brass shells for strength and lightness. The
pistons are made from ebony fiber. The cylinders have a bore of ⁵⁄₈″,
with a piston stroke of ¹⁄₂″. The crank case is built up from a small
piece of brass tubing and is drilled out for lightness. The crankshaft
is hollow, and is supported at the rear by a special bearing which
acts as a rotary valve, admitting the intake through the crankshaft
and permitting the exhaust to escape through a specially constructed
bearing.

The tank is constructed of 30 gauge sheet bronze, wire wound, and
fitted at the ends with spun brass caps. The actual weight of the
engine alone is 2¹⁄₂ ounces, the tank and fittings weighing 11¹⁄₂
ounces, making the total weight of the complete power plant 14 ounces.

THE SCHOBER FOUR CYLINDER OPPOSED ENGINE

Another interesting type of compressed air engine that has been
developed in America is the Schober four cylinder opposed engine.
While this engine is different in appearance from most compressed air
engines, it has been made to work satisfactorily and is consistent with
the same high class construction that is displayed in most all of Mr.
Schober’s engines. The accompanying diagram 18 illustrates the method
of operation of the four cylinder engine.

[Illustration: Diagram 18]

The crank case is constructed from four pieces of 24 gauge spring
brass, substantially connected in the form of a rectangle, the top and
bottom being left open. The front and rear walls have flanges which
engage the inside of the side walls and are secured thereto by four
small screws on each side, thereby making it an easy matter to take the
crank case apart.

The four cylinders are made from drawn brass shells and have a bore of
¹⁄₂″ and stroke of ¹⁄₂″. The pistons are made of solid red fiber. The
two-throw crankshaft is built up of steel with brass webs. The bearings
are of steel. The valves, being overhead, are driven by a gear mounted
at the end of the crankshaft, the gear driving the valve shaft by means
of a gear on that shaft, with which the crankshaft gear meshes. The
valve arrangement, as shown in diagram 18, consists of four recesses
cut into the valve shaft, two of which allow the air to pass from the
inlet pipes, which lead into the valve chamber at the center of same,
to two of the cylinders at once, while the other two recesses allow the
exhaust to pass from openings in the sides of the valve chamber.

The cylinders are secured to the side plates of the crank case so
that when those side plates are removed, the cylinders are removed with
them. The pipes are detachable at their centers; small pipes running to
the heads of the cylinders extending into the larger pipes which run
to the valve chamber. This arrangement is shown in the end view of the
engine. A 17″ propeller is used in connection with this engine.

GASOLINE ENGINES

THE JOPSON 1 H. P. GASOLINE ENGINE
FOR MODEL AËROPLANES

During the past few years several attempts have been made, both in this
country and abroad, to produce a reliable gasoline engine for model
aëroplane work, but mostly without any degree of success. The reason
for this inability, no doubt, is due to the scarcity of small working
parts sufficiently light and at the same time reliable. The engine
described herewith, designed by Mr. W. G. Jopson, a member of the
Manchester Aëro Club, England, is one of the few that have been made to
work satisfactorily.

[Illustration]

[Illustration: The interesting horizontal-opposed Jopson gasoline
engine for model aëroplanes. The top photograph shows the half-speed
shaft and the arrangement of the valve mechanism. This engine is
air cooled, develops 1 h.p. at 1,500 r.p.m., and weighs 7¹⁄₂ lbs.,
including gasoline tank and propeller. The bottom view shows the engine
with propeller _in situ_. Courtesy _Flight_.]

As the accompanying diagrams 19 and 20 and photograph show, the engine
is of the four-cycle, horizontal opposed type, having two cast-iron
cylinders of 1¹⁄₄″ bore and 1³⁄₈″ stroke. Each cylinder is cast in
one piece, and as the engine is air cooled, they are cast with
radiating fins. One h.p. is developed at 1500 r.p.m. The total weight
of the engine, gasoline tank and propeller is 7¹⁄₂ lbs. In preparing
the design of this engine, the designs of similar full-sized aëro
engines were followed as far as possible. The pistons are similar to
those used on large aëro engines and are fitted with two rings; the
crankshaft is turned out of two inch special bar steel, and is carried
in two phosphor-bronze bearings. There is no special feature about the
connecting rods, these being of the standard type, but very strong and
light. To enable the two cylinders to be exactly opposite one another,
the connecting-rods are offset in the pistons and are connected to
the latter by gudgeonpins. The aluminum crank case is extremely
simple, being cylindrical and vertically divided. The inlet valves are
automatic, the exhaust valves being mechanically operated; the camshaft
is driven from the main shaft by two-to-one gearing.

[Illustration: Diagram 19

Sectional elevation of the 1 h.p. Jopson gasoline engine for
models. The disposition of the gasoline tank and wick carburettor
is particularly noteworthy. It will be seen that metal journals are
provided for the crankshaft, which is turned out of 2-inch bar steel.
Courtesy _Flight_.]

To assist the exhaust, and also the cooling, small holes are drilled
round the cylinder in such a position that when the piston is at the
inner end of its stroke, these holes are uncovered, thus permitting
the hot exhaust to escape, and so relieve the amount passing through
the exhaust valves. The commutator is also driven off the camshaft, as
shown in the drawing. No distributor is fitted to the commutator, as
small ones are somewhat troublesome and very light coils are obtainable
at a reasonable price.

The gasoline tank is made of copper in streamline form, and is usually
fitted to the back of the crankcase, thus reducing the head resistance,
but if desired it can be fitted in any other position. The action of
the carburetor can be easily seen from the drawings; it is of the
surface type and much simpler, lighter and quite as efficient as the
spray type. Specially light and simple spark plugs are used, that give
very little trouble. The propeller used in connection with this engine
is somewhat out of the ordinary, having been specially designed for
this engine, and patented. The propeller is made entirely of aluminum
and has a variable pitch, this being easily obtainable, as the blades
are graduated so that any desired pitch, within certain limits, may be
given at once. The results of a series of tests on a 30 inch propeller
are shown on the accompanying chart, and from it the thrust as certain
speeds with a certain pitch can be obtained. Taking the engine running
at 1540 r.p.m. with a pitch of 15″, the thrust comes out at 9¹⁄₂ lbs.,
or more than the weight of the engine and accessories.

[Illustration: Diagram 20

Diagram of results obtained from tests of the 1 h.p. Jopson model
gasoline engine, showing the thrust in pounds at varying speeds with
propellers of different pitch. Courtesy _Flight_.]

THE MIDGET AËRO GASOLINE ENGINE

Although numerous model constructors in America are experimenting with
model gasoline engines, the Midget Gasoline Engine, the product of
the Aëro Engine Company, Boston, Massachusetts, is perhaps the most
satisfactory up to the present time. An engine of this type was used by
Mr. P. C. McCutchen of Philadelphia, Pennsylvania, in his 8 foot Voisin
Type Biplane Model, for which he claims a number of satisfactory
flights.

The engine is made from the best iron, steel, aluminum and bronze and
the complete weight including a special carburetor, spark plug and
spark coil is 2¹⁄₂ lbs. From the top of the cylinder head to the bottom
of the crank case the engine measures 7″. It is possible to obtain from
this engine various speeds from 400 to 2700 r.p.m., at which speed it
develops ¹⁄₂ h.p. The propeller used in connection with this engine
measures 18″ in diameter and has a 13″ pitch.

[Illustration: The Midget ¹⁄₂ H. P. gasoline engine]

It might be of interest to know that one of the parties responsible
for the development of this engine is Mr. H. W. Aitken, a former model
maker and who is now connected with one of the largest aëro engine
manufacturing companies in America.

STEAM POWER PLANTS

Aside from the compressed air engine there is the steam driven
engine which has been used abroad to considerable degree of success.
Owing to the difficulty in constructing and operating a steam driven
engine, very few model flyers in America have devoted any attention
to the development of this engine as a means of propulsion for model
aëroplanes. But irrespective of the limitations of the steam engine
a great deal of experimentation has been carried on in England, and
without doubt it will soon be experimented with in America.

H. H. GROVES STEAM POWER PLANTS

Perhaps one of the most successful steam power plants to have been
designed since the development of the Langley steam driven model, is
the Groves type of steam power plant, designed by Mr. H. H. Groves, of
England. On one occasion several flights were made with a model driven
by a small steam engine of the Groves type weighing 3 lbs. The model
proved itself capable of rising from the ground under its own power and
when launched it flew a distance of 450 feet. This is not a long flight
when compared with the flight made by Prof. Langley’s steam driven
model on November 28, 1896, of three-quarters of a mile in 1 minute and
45 seconds, but the size of the models and also that Mr. Groves’ model
only made a duration of 30 seconds, must be considered. The model was
loaded 12 ounces to the square foot and had a soaring velocity of some
20 m.p.h. The total weight of the power plant was 1¹⁄₂ lbs. Propeller
thrust 10 to 12 ounces. The total weight of the model was 48 ounces.
The type of steam plant used in connection with this model was of the
flash boiler, pressure fed type, with benzoline for fuel.

Mr. Groves has done considerable experimenting with the steam driven
type power plant. Many of the designs used in the construction of
steam plants for models are taken from his designs. A Groves steam
power plant is employed in one of Mr. V. E. Johnson’s (Model Editor
of _Flight_) model hydroaëroplanes, the first power-driven, or
“mechanically driven” model hydroaëroplane (so far as can be learned)
to rise from the surface of the water under its own power. This model
has a total weight of 3 lbs. 4 ounces.

G. HARRIS’S STEAM ENGINE

Another advocate of the steam driven type model is Mr. G. Harris, also
of England. Several good flights were made by Mr. Harris with his
pusher type monoplane equipped with a steam driven engine. As a result
of his experiments he concluded that mushroom valves with a lift of
¹⁄₆₄ part of an inch were best, used in connection with the pump, and
at least 12 feet of steel tubing should be used for boiler coils. The
first power plant constructed by Mr. Harris contained a boiler coil 8
feet long, but after he had replaced this coil with one 12 feet long,
irrespective of the fact that the extra length of tube weighed a couple
of ounces, the thrust was increased by nearly a half pound.

[Illustration: An English steam power plant for model aëroplanes.
Courtesy _Flight_.]

[Illustration: Model hydroaëroplane owned by V. E. Johnson, Model
Editor of _Flight_, England, equipped with an H. H. Groves steam power
plant. This model is the first power driven—as far as can be learned—to
rise from the surface of the water under its own power. Courtesy
_Flight_.]

The principal parts used in Mr. Harris’s steam power plant was an
engine of the H. H. Groves type, twin cylinder, ⁷⁄₈″ bore with a piston
stroke of ¹⁄₂″. The boiler was made from 12″ of ³⁄₁₆″ × 20″ G. steel
tubing, weighing 10.5 ounces. The blow lamp consisted of a steel tube,
⁵⁄₃₂″ × 22″ G. wound round a carbide carrier for a nozzle. The tank was
made of brass ⁵⁄₁₀₀₀″ thick. The pump, ⁷⁄₃₂″ bore, stroke variable to
¹⁄₂″, fitted with two non-return valves (mushroom type) and was geared
down from the engine 4.5 to 1.

PROFESSOR LANGLEY’S STEAM ENGINE

The Langley steam driven model, of which so much has been said, and
which on one occasion flew a distance of one-half mile in 90 seconds,
had a total weight of 30 lbs., the engine and generating plant
constituting one-quarter of this weight. The weight of the complete
plant worked out to 7 lbs. per h.p. The engine developed from 1 to 1¹⁄₂
h.p. A flash type boiler was used, with a steam pressure of from 150
to 200 lbs., the coils having been made of copper. A modified naphtha
blow-torch, such as is used by plumbers, was used to eject a blast or
flame about 2000 Fahrenheit through the center of this coil. A pump was
used for circulation purposes. With the best mechanical assistance that
could be obtained at that date, it took Professor Langley one year to
construct the model.

FRENCH EXPERIMENTS WITH STEAM POWER PLANTS

About ten months after Langley’s results, some experiments were carried
out by the French at Carquenez, near Toulon. The model used for the
experiments weighed in total 70 lbs., the engine developing more than
1 h.p. As in the Langley case, twin propellers were used, but instead
of being mounted side by side, they were mounted one in front and the
other behind. The result of these experiments compared very poorly with
Langley’s. A flight of only 462 feet was made, with a duration of a few
seconds. The maximum velocity is stated to have been 40 m.p.h. The span
of this model was a little more than 6 meters, or about 19 feet, with a
surface of more than 8 square meters, or about 80 square feet.

[Illustration: An English hydroaëroplane of tractor design equipped
with steam power plant. Courtesy _Flight_.]

[Illustration: On the left an English 10 oz. Compressed air driven
biplane. On the right, the engine shown fitted with a simple speedometer
for experimental purposes. Courtesy _Flight_.]

CARBONIC GAS ENGINE

The six-cylinder carbonic gas engine described herewith is the product
of Mr. Henry Rompel, Kansas City, Missouri.

This is perhaps one of the most interesting of its kind to have been
developed during 1916, and its appearance in the model aëroplane field
adds weight to the claim that mechanical engines will soon replace the
rubber strand as motive power for model aëroplanes.

Mr. Rompel’s engine is of rotary, carbonic gas type, having six
cylinders, a bore of ⁵⁄₈″ and a stroke of ³⁄₄″.

The intake is derived through a rotary valve which also acts as a crank
shaft bearing, thereby saving weight.

The exhaust is accomplished by mechanically operated valves situated in
the heads of the cylinders being opened by the aid of rocker arms and
push rods, which gain their timing from a cam placed on the crankshaft.

To save weight in construction the crankshaft, connecting rods, pistons
and cylinders were made of telescopic tubing with a side wall of one
thirty-second of an inch or less in thickness.

The engine has a swing of 5¹⁄₂″ over all, weighs a little less than 8
ounces complete, and is operated on 1,500 pounds pressure (carbonic
gas) and at a speed of 3,500 to 3,700 r.p.m. will develop about 1 horse
power. While spinning a 17″ propeller with a pitch of 20 inches it will
deliver a thrust of 21 ounces, and has a duration of 40 seconds. Two
hundred and fifty-six pieces were embodied in its construction.

[Illustration: The Rompel six-cylinder carbonic gas engine]

THE FORMATION OF MODEL CLUBS

To form a model aëroplane club at least six interested persons are
necessary. As soon as a place in which to hold meetings has been
decided upon the club should proceed to elect a director whose duty
should be to manage the affairs of the club. One of the first things
to be considered is the name under which the club will operate; the
custom is usually to adopt the name of the town or city in which the
club is located, viz.: Concord Model Aëro Club, Concord, Massachusetts,
although it is the privilege of the majority of the members to choose
a name such as they might feel will best benefit the purpose for which
the club was organized. As in the case of the Aëro Science Club of
America, this club was formed for the purpose of stimulating interest
in model aëronautics and to help those who might become interested
therein, not only in New York City but throughout the entire United
States.

When the matter of name and place has been settled the club should
decide upon the course it is to follow, first by electing OFFICERS and
second by preparing a CONSTITUTION AND BY-LAWS. In the case of clubs
whose membership does not comprise more than six members, it does not
seem desirable to have more than one officer, namely, a DIRECTOR, who
might perform the duties of a president, treasurer and secretary until
the club has reached a larger membership. In this way the members are
enabled to concentrate upon the construction and flying of models
and to engage in such other activities as to carry out the purpose
for which the club was organized. However, the foregoing is merely a
suggestion on the part of the writer, who by the way is a member of
the Aëro Science Club of America and formerly acted in the capacity of
secretary to that club.

Clubs whose membership totals more than twelve, however, should proceed
to elect a President, Treasurer and Secretary, all of whom must receive
a vote of at least two-thirds of the membership. With clubs of this
size a director is not needed as the affairs of the club are usually
entrusted with the governing officers, the President, Treasurer and
Secretary. In as much as the constitution and by-laws are an important
factor in the affairs of any model club, the governing officers,
before mentioned, should hold a private meeting at the earliest
moment whereat to frame a constitution and set of by-laws embodying
the purposes and policy of the club. When the proposed constitution
and by-laws are completed they should be presented to the members for
approval after which a copy should be given to every member.

The following is a specimen of constitution and by-laws that might be
used by any person or persons desiring to form a Model Aëro Club:

CONSTITUTION AND BY-LAWS OF A MODEL
AËROPLANE CLUB

ARTICLE 1. NAME. The name of this club will be known as The ..........
Model Aëro Club.

PURPOSE. The object of this club shall be to study and increase the
interest in the science of aëronautics in every way possible and to
realize this object, shall construct and fly model aëroplanes, gliders
and man carrying machines.

FURTHER, Contests shall be held for model aëroplanes and prizes awarded
to the winners thereof. And as a further step in the advancement of
this art, meetings, lectures, discussions, debates and exhibitions will
be held.

ARTICLE 2. MEMBERSHIP. Any person may become a member of this club
provided his application receives the unanimous approval of the
majority of members, or is passed upon by the membership committee.
A member may resign his membership by written communication to the
secretary who shall present it to the membership committee to be passed
upon.

ARTICLE 3. OFFICERS. The officers of this organization shall be a
President, Vice-president, Secretary and Treasurer and a board of
governors to consist of said officers. The president and vice-president
shall constitute the executive committee of the board of governors,
with full powers to act for them in the affairs of the club. The
election of officers shall take place at the first meeting held during
the month of .......... of each year and shall hold office for one
year. In the event of a vacancy in the office of the President the
Vice-president or next highest officer present shall preside. Any
other vacancy shall be filled by an officer temporarily appointed by
the President. The President shall preside at all meetings of the
club and of the board of governors, and shall perform such other
duties as usually pertain to that office. The President shall have
full authority to appoint committees or boards as may be necessary to
further the interests of the club.

The Secretary shall keep a record of all meetings of the club, board of
governors and committees and shall use the seal of the club as may be
directed by the executive committee. Further, he shall issue notices
to officers and members of all special meetings and perform such other
duties as may be assigned him by the constitution, by the club or by
the board of governors.

The Treasurer shall have charge of the funds of the club, receive
all moneys, fees, dues, etc.; pay all bills approved by the board of
governors, and preserve all proper vouchers for such disbursements.

RULES FOR CONTESTS

We now come to the matter of contests. As there are many different
types of models so must there be rules to correspond to avoid
misunderstandings, and until the club has reached the stage where
it may decide upon a particular set of rules under which its members
should participate perhaps the following set of rules, applicable to
contests for hand launched models, can be adopted. In so far as there
are different rules for different contests, namely, hand launched, R.
O. G. and R. O. W. and mechanical driven, the following rules are used
only in connection with contests for hand launched models; rules for
other contests follow:

RULES

A contest to be official must have at least five contestants.

Each contestant must abide by the rules of the contest and decision of
the judges.

Each contestant must register his name, age, and address before the
event.

Each contestant must enter and fly models made by himself only.

Trials to start from a given point indicated by the starter of the
trials, and distance to be measured in a straight line from the
starting point to where the model first touches the ground, regardless
of the curves or circles it may have made. Each contestant must have
his models marked with his name and number of his models (1, 2, 3,
etc.), and each model will be entitled to three official trials.
Contestant has the privilege of changing the planes and propellers as
he may see fit, everything to be of his own construction, but only
three frames can be used in any contest. If in the opinion of the board
of judges there are too many entries to give each one nine flights in
the length of time fixed, the judges have the power to change that part
of rule No. 6 to the following:

“Six flights or less, as circumstances may require, will be allowed to
each contestant, which can be made with one model or any one of three
entered; all of his own construction; due notice must be given to each
contestant of the change.”

No trial is considered as official unless the model flies over 100 feet
from the starting point. (The qualifying distance can be changed by
agreement between the club and the starter provided the entrants are
notified.) Should the rubber become detached from the model, or the
propeller drop off during the trial, the trial is counted as official,
provided the model has covered the qualifying distance. No matter what
may happen to the model after it has covered the qualifying distance
the flight is official. Contests should cover a period of three hours,
unless otherwise agreed.

No contestant shall use the model of another contestant, although the
former may have made it himself.

The officials should be: a starter, measurer, judge and scorer; also
three or four guards to keep starting point and course clear. The first
three officials shall, as board of judges, decide all questions and
disputes. A space 25 feet square (with stakes and ropes) should be
measured off for officials and contestants, together with an assistant
for each contestant. All others must be kept out by the guards and a
space kept clear (at least 25 feet) in front of the starting point, so
a contestant will not be impeded in making his trial.

Each official should wear a badge, ribbon or arm band designating his
office, and must be upheld in his duties.

HANDICAPS

At the discretion of the club there may be imposed a handicap for club
events as follows: A contestant in order to win must exceed his last
record with which he won a prize.

COMBINATION AND DURATION EVENTS

First, second and third records to count. Lowest number of points to
win. For example:

A may have 1st in distance and 2nd in duration, 3 total points.

B may have 3rd in distance and 1st in duration, 4 total points.

C may have 2nd in distance and 3rd in duration, 5 total points.

Accordingly A wins.

R. O. G. CONTESTS

(Rising from the Ground)

Models to be set on the ground and allowed to start off without any
effort on the part of the contestant. Models should rise from the
ground before reaching a predetermined mark, no flight to be considered
unless it does so. Contestant may start at any length back from the
mark, but the distance is to be measured only from the mark.

MECHANICALLY DRIVEN MODEL CONTESTS

For duration, or distance, contests for mechanically driven models
might be held under the same ruling that applies to R. O. G. models.
But owing to the many types of engines used in mechanically driven
models, definite rules for the holding of such a contest must be left
to the discretion of the club or contestants.

EVENTS OPEN TO ALL

These events are open to all, with no handicaps to be imposed on either
club members or others.

INTER-CLUB MODEL AËROPLANE TOURNAMENTS

(Prizes to be determined by contesting clubs)

The tournament to consist of five events as follows:

Duration: Models launched from hand.

Distance: Models launched from hand.

Duration: Models launched from ground. R. O. G.

Distance: Models launched from ground. R. O. G.

Duration: Models launched from water. R. O. W.

Dates for inter-club contest should be arranged for at least three
weeks prior to date of first contest, to allow ample time for the
construction of special models and elimination trials.

In event of inclement weather the contest to take place the week
following (each contest following to be set one week ahead), or at any
time that may be determined by a committee appointed by the contesting
clubs.

Each competing club must be represented by a team of three contestants
and one non-competitor, who will act as judge in conjunction with the
judges from the other clubs, and a manager selected by the judges who
will supervise over the entire tournament and issue calls for meetings.
(Substitutes should also be selected for any possible vacancy.)

Meetings of the judges of the competing clubs should be held at some
designated place, at which time dates and general details shall be
arranged, and between events there should be a meeting called, for
general discussion regarding the recent event, receive protests and
suggestions and to announce officially the result of the contest.

The manager shall have control of the various events, assisted by the
judges and they shall decide all disputes that may arise, and act as
scorers and timers, as well.

Each flyer will be allowed but one model and shall be entitled to three
official flights, but he shall be permitted to make any repairs or
replace any broken parts. No contestant shall be privileged to fly a
model not of his own construction. Each event shall close when all the
contestants have made three official flights, or when three hours’ time
has elapsed.

WORLD’S MODEL FLYING RECORDS

(TWIN PROPELLER PUSHER TYPE MODELS)

MONOPLANE

Year 1917. Ward Pease (America), rise off ground, distance
3364 feet.

Year 1916. Thomas Hall (America), hand launched, distance
5537 feet.

Year 1917. Donovan Lathrop (America), hand launched,
duration 5 minutes.

Year 1917. Emil Laird (America), 18 inch type model,
distance 750 feet.

Year 1915. Wallace A. Lauder (America), hand launched,
distance 3537 feet.

Year 1915. Wallace A. Lauder (America), hand launched,
duration 195 seconds.

Year 1914. Fred Watkins (America), rise off ground,
distance 1761 feet.

Year 1914. J. E. Louch (England), rise off ground, duration
169 seconds.

Year 1915. E. C. Cook (America), rise off water, duration
100 seconds.

(TWIN PROPELLER TRACTOR TYPE)

MONOPLANE

Year 1913. Harry Herzog (America), rise off water, duration
28 seconds.

(TWIN PROPELLER PUSHER TYPE)

BIPLANE

Year 1915. A. H. Wheeler (America), rise off ground,
duration 143 seconds.

(SINGLE PROPELLER PUSHER TYPE)

MONOPLANE

Year 1914. J. E. Louch (England), hand launched, duration
95 seconds.

Year 1914. W. E. Evans (England), rise from ground,
distance 870 feet.

Year 1914. J. E. Louch (England), rise from ground,
duration 68 seconds.

Year 1914. L. H. Slatter (England), rise from water,
duration 35 seconds.

(SINGLE PROPELLER TRACTOR TYPE)

MONOPLANE

Year 1915. D. Lathrop (America), hand launched, distance
1039 feet.

Year 1915. D. Lathrop (America), hand launched, duration
240 seconds.

Year 1914. C. D. Dutton (England), rise from ground,
distance 570 feet.

Year 1914. J. E. Louch (England), rise from ground,
duration 94 seconds.

Year 1915. L. Hittle (America), rise from water, duration
116 seconds.

(SINGLE PROPELLER TRACTOR TYPE)

BIPLANE

Year 1915. Laird Hall (American), rise from ground,
duration 76 seconds.

(FLYING BOAT TYPE)

MONOPLANE

Year 1915. Robert La Tour (America), rise from water,
duration 43 seconds.

(FLYING BOAT TYPE)

BIPLANE

Year 1914. C. V. Obst (America), rise from water, duration
27 seconds.

(MECHANICAL DRIVEN MODEL)

Year 1914. D. Stanger (England), rise from ground, duration
51 seconds.

(All British records are quoted from _Flight_)

DICTIONARY OF AËRONAUTICAL TERMS

AËRODROME—A tract of land selected for flying purposes.

AËRODYNAMICS—The science of Aviation, literally the study of the
influence of air in motion.

AËROFOIL—A flat or flexed plane which lends support to an
aëroplane.

AËRONAUT—One engaged in navigating the air.

AËRONAUTICS—The science of navigating the air.

AËROPLANE—A heavier than air machine supported by one or more
fixed wings or planes.

AËROSTATICS—The science of aërostation, or of buoyancy caused by
displacement, ballooning.

AËROSTATION—The science of lighter than air or gas-borne machines.

AILERON—The outer edge or tip of a wing, usually adjustable, used
to balance or stabilize.

AIRSHIP—Commonly used to denote both heavier and lighter than air
machines; correctly a dirigible balloon.

ANGLE OF INCIDENCE—The angle of the wing with the line of travel.

AREA—In the case of wings, the extent of surface measured on
both the upper and lower sides. An area of one square foot
comprises the actual surface of two square feet.

ASPECT RATIO—The proportion of the chord to the span of a wing.
For example if the wing has a span of 30 inches and a chord
of 6 inches the
span
aspect ratio will be 5 or —————
chord.

AUTOMATIC STABILITY—Stability secured by fins, the angle of the
wings and similar devices.

AVIATOR—One engaged in Aviation.

AVIATION—The science of heavier than air machines.

ANGLE OF BLADE—The angle of the blade of a propeller to the axis
of the shaft.

BALANCER—A plane or other part intended for lateral equilibrium.

BEARING BLOCK—Used in connection with the mounting of propellers
on model aëroplanes. Made from wood and metal.

BRACE—Strip of bamboo or other material used to join together the
frame side members. Also used in joining other parts of a
model.

BIPLANE—An aëroplane or model aëroplane with two wings superposed.

BODY—The main framework supporting the wing or wings and the
machinery.

BANKING—The lateral tilting of an aëroplane when taking a turn.

CAMBER—The rise of the curved contour of an arched surface above
the Chord Line.

CENTER OF GRAVITY—The point at which the aëroplane balances.

CENTER OF PRESSURE—The imaginary line beneath the wing at which
the pressure balances.

CHASSIS (CARRIAGE)—The part on which the main body of an
aëroplane or model aëroplane is supported on land or water.

CHORD—The distance between the entering and trailing edges of a
wing.

DECK—The main surface of a biplane or multiplane.

DIRECTIONAL CONTROL—The ability to determine the direction of the
flight of an aëroplane.

DIRIGIBLE—A balloon driven by power.

DOPE—A coating for wings.

DOWN WIND—With the wind.

DRIFT—The resistance of the wing to the forward movement.

DIHEDRAL ANGLE—The inclination of the wings to each other usually
bent up from the center in the form of a flat V.

ELEVATOR—The plane or wing intended to control the vertical
flight of the machine.

ENGINE—A contrivance for generating driving power.

ENGINE BASE—Main stick used for frame of single stick model.

ENGINEER—One who controls the power, driving the machinery.

ENTERING EDGE _or_ LEADING EDGE—Front edge or edge of the surface
upon which the air impinges.

EQUILIBRATOR—A plane or other contrivance which makes for
stability.

FIN—A fixed vertical plane.

FLEXED—A wing is said to be flexed when it curves upward forming
an arc of a circle.

FLYING STICK—Name applied to ordinary A type and single stick
models.

FLYING MACHINE—Literally a form of lighter than air craft; a
gas-borne airship.

FLYING BOAT—A hull or large float used in connection with an
aëroplane to enable its rising from and alighting upon the
surface of the water.

FRAME—A single or double stick structure to which all parts of
a model are attached. Three or more sticks are sometimes
employed in the construction of a frame. However, the usual
number is two, joined together in the form of letter “A.”

FRAME HOOKS—The looped ends of a piece of wire attached to the
point of the frame to accommodate the S hooks attached to the
rubber strands.

FRAME SIDE MEMBERS—Two main sticks of an A type frame.

FUSELAGE—The body or framework of an aëroplane.

GLIDER—An aëroplane without motive power.

GUY—A brace, usually a wire or cord used for tuning up the
aëroplane.

GROSS WEIGHT—The weight of the aircraft, comprising fuel,
lubricating oils and the pilot.

GYROSCOPE—A rotating mechanism for maintaining equilibrium.

GAP—The vertical distance between the superposed wings.

HANGAR—A shed for housing an aëroplane.

HARBOR—A shelter for aircraft.

HEAVIER THAN AIR—A machine weighing more than the air it
displaces.

HELICOPTER—A flying machine in which propellers are utilized to
give a lifting effect by their own direct action on the air.
In aviation the term implies that the screw exerts a direct
lift.

HELMSMAN—One in charge of the steering device.

HYDROAËROPLANE—An aëroplane with pontoons to enable its rising
from the surface of the water. Known as hydro in model
circles.

KEEL—A vertical plane or planes arranged longitudinally either
above or below the body for the purpose of giving stability.

LATERAL STABILITY—Stability which prevents side motion.

LOADING—The gross weight divided by the supporting area measured
in square feet.

LONGITUDINAL STABILITY—Stability which prevents fore and aft
motion or pitching.

LONGERONS—Main members of the fuselage. Sometimes called
longitudinals.

MAST—A perpendicular stick holding the stays or struts which keep
the wings rigid.

MODEL AËROPLANE—A scale reproduction of a man-carrying machine.

MECHANICAL POWER—A model driven by means other than rubber
strands such as compressed air, steam, gasoline, spring,
electricity and so forth is termed a mechanical driven model.
The power used is termed mechanical power.

MOTIVE POWER—In connection with model aëroplanes a number of
rubber strands evenly strung from the propeller shaft to the
frame hooks which while unwinding furnish the necessary power
to propel the model.

MAIN BEAM—In connection with model aëroplanes a long stick which
is secured to the under side of the wing frame at the highest
point in the curve of the ribs adding materially to the
rigidity of the wing.

MONOPLANE—An aëroplane or heavier than air machine supported by a
single main wing which may be formed of two wings extending
from a central body.

MULTIPLANE—An aëroplane with more than four wings superposed.

NACELLE—The car of a dirigible balloon, literally a cradle. Also
applied to short body used in connection with aëroplanes for
the accommodation of the pilot and engine.

NET WEIGHT—Complete weight of the machine without pilot, fuel or
oil.

ORNITHOPTER—A flapping wing machine which has arched wings like
those of a bird.

ORTHOGONAL—A flight maintained by flapping wings.

OUTRIGGERS—Members which extend forward or rearward from the main
planes for the purpose of supporting the elevator or tail
planes of an aëroplane.

PLANE—A surface or wing, either plain or flexed, employed to
support or control an aëroplane.

PILOT—One directing an aëroplane in flight.

PITCH—Theoretical distance covered by a propeller in making one
revolution.

PROPELLER—The screw used for driving an aëroplane.

PROPELLER BEARINGS—Pieces of bronze tubing or strips of metal
formed to the shape of the letter “L” used to mount
propellers. Also made from blocks of wood.

PROPELLER BLANK—A block of wood cut to the design of a propeller.

PROPELLER SPAR(S)—The heavy stick or sticks upon which the
bearing or bearings of a single or twin propeller model are
mounted.

PROPELLER SHAFT—A piece of wire which is run through the hub of
the propeller and tubing in mounting the propeller.

PYLON—Correctly, a structure housing a falling weight used for
starting an aëroplane, commonly a turning point in aëroplane
flights.

PUSHER—An aëroplane with the propeller or propellers situated in
back of the main supporting surfaces.

QUADRUPLANE—An aëroplane with four wings superposed.

RUDDER—A plane or group of planes used to steer an aëroplane.

RUNNER—Strip beneath an aëroplane used for a skid.

RUNNING GEAR _or_ LANDING GEAR—That portion of the chassis
consisting of the axle, wheels and shock absorber.

RIB—Curved brace fastened to the entering and trailing edges of a
wing.

SCALE MODEL—A miniature aëroplane exactly reproducing the
proportions of an original.

SPAR—A mast strut or brace.

SIDE SLIP—The tendency of an aëroplane to slide or slip sideways
when too steep banking is attempted.

STABILITY—The power to maintain an even keel in flight.

STARTING PLATFORM—A runway to enable an aëroplane to leave the
ground.

SURFACE FRICTION—Resistance offered by planes or wings.

SLIP—The difference between the distance actually traveled by a
propeller and that measured by the pitch.

SOARING FLIGHT—A gliding movement without apparent effort.

SUSTAINING SURFACE—Extent of the wings or planes which lend
support to an aëroplane.

SPAN (SPREAD)—The dimension of a surface across the air stream.

STREAMLINE—Exposing as little surface as possible to offer
resistance to air.

SKIDS—In connection with model aëroplanes, steel wires or strips
of bamboo allowed to extend below the frame to protect the
model in landing and to permit its rising off the ground or
ice.

S OR MOTOR HOOKS—A piece of wire bent in a double hook to
resemble the letter “S.” One end to be attached to the frame
hook, the other serving as accommodation for the rubber
strands.

TAIL—The plane or planes, both horizontal and vertical, carried
behind the main planes.

TANDEM—An arrangement of two planes one behind the other.

THRUST—The power exerted by the propeller of an aëroplane.

TENSION—The power exerted by twisted strands of rubber in
unwinding.

TRACTOR—An aëroplane with the propeller situated before the main
supporting surfaces.

TRIPLANE—An aëroplane with three wings superposed.

TRAILING EDGE—The rear edge of a surface.

TORQUE—The twisting force of a propeller tending to overturn or
swerve an aëroplane sideways.

UP WIND—Against the wind.

WAKE—The churned or disturbed air in the track of a moving
aëroplane.

WASH—The movement of the air radiating from the sides of an
aëroplane in flight.

WINGS—Planes or supporting surfaces, commonly a pair of wings
extending out from a central body.

WINDER—An apparatus used for winding two sets of rubber strands
at the same time in opposite directions or one at a time.
Very often made from an egg beater or hand drill.

WARPING—The springing of a wing out of its normal shape, thereby
creating a temporary difference in the extremities of the
wing which enables the wind to heel the machine back again
into balance.

ABREVIATIONS

H. P. Horse Power.
R. P. M. Revolutions per minute.
H. L. Hand launched.
R. O. G. Rise off ground model.
R. O. W. Rise off water model.
M. P. H. Miles per hour.

THE END

————————————— End of Book —————————————

Transcriber’s Note (continued)

Errors in punctuation have been corrected. Inconsistencies in spelling,
grammar, capitalisation, and hyphenation are as they appear in the
original publication except where noted below:

Page 16 – “bob-sled″” changed to “bobsled″” (an ordinary bobsled)

Page 53 – “approximately cross section” changed to “approximately
circular cross section”

Page 55 – “run” changed to “runs” (one of which wires runs to)

Page 83 – “ten″” changed to “10″” (10″ propeller)

Page 105 – “five cylinder” changed to “three cylinder” (Schober-Funk
three cylinder rotary engine) [This change was made to
the illustration caption on this page and also to the
entry in the List of Illustrations that points to it.]

Page 106 – “diagram 17” changed to “diagram 18” (The accompanying
diagram 18 illustrates)

Page 108 – “crank-shaft” changed to “crankshaft” (The two-throw
crankshaft)

Page 111 – “cam-shaft” changed to “camshaft” (provided for the
camshaft)

Page 112 – “crank-shaft” changed to “crankshaft” (the crankshaft
is driven)

Page 113 – “stream-line” changed to “streamline” (streamline form)

Page 116 – “Bi-plane” changed to “Biplane” (Type Biplane Model)

The prefix of AËRO/Aëro/aëro as in ‘aëroplane’, etc., is used
throughout the body text of the original publication with a few
exceptions. These latter have been changed for consistency in this
transcription. The unaccented prefix AERO/Aero/aero is now only used
in title page text.

Incorrect entries in the Table of Contents have had their text and/or
page references changed so that they agree with the text and location
of the parts of the original publication to which they refer.

Entries in the DICTIONARY OF AËRONAUTICAL TERMS which are not in
the correct alphabetical order have been left as they appear in the
original publication. Some minor typographical errors and spelling
mistakes have been corrected without further note.

*** End of this LibraryBlog Digital Book "Model Aeroplanes and Their Engines: A Practical Book for Beginners" ***

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