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Cody No.2

Страна: Великобритания

Год: 1910

Cody - The British Army Aeroplane I - 1908 - Великобритания<– –>Cody - No.3 - 1911 - Великобритания


M.Goodall, A.Tagg British Aircraft before the Great War (Schiffer)


CODY biplane No.IIA, B, C, D and E (British Michelin Trophy Type)

  No.IIA. For 1910 Cody planned a smaller machine with single pusher propeller, but much in the style of the last version of his first machine. He required more power and planned to fit a ten-cylinder 100hp Phoenix rotary engine, which did not materialize. The design was changed to accept two 60hp Green engines, but only one was fitted initially. On its first appearance the radiators were above the engine and no horizontal tail surface was fitted. In this form it flew two circuits of Laffan's Plain on 23 June 1910, at about 50ft but crashed on landing, injuring Cody.
  In the course of the rebuild a fixed tailplane was added. Cody took the machine to the Wolverhampton and Bournemouth meetings in June and July, but his flying was limited and no prize money was won. In August he arrived at Lanark with the machine, but he received a second engine on loan from the Green Company. This could not be synchronized, with the other so both were removed. Cody's visit to Lanark was most unsuccessful.

  No.IIB His original French ENV was then fitted and this remained in use until late October. During September he carried nine passengers on various flights, flying 113 miles in the first week and 126 miles in the third. On 30 September 1910 he flew for 1hr 15min and then for 50min. The French-made engine could not be used for the Michelin Contest, for which a ?500 prize and trophy were offered. In late October he refitted the Green on a new single mounting and on 4 November 1910 made an attempt lasting 2hr 25min. He then installed a British ENV, which was on loan, in the first week of November, but after a minor accident on 12 November 1910, this was removed and returned to the ENV company.

  No.IIC. Cody reverted to a single Green and used this until the end of the year, winning the British Empire Michelin Trophy for a flight of 4hr 47min in a closed circuit, calculated as 185.46 miles, on his third attempt on the last day of the year and of the Contest.

  No.IID. Cody exhibited his aircraft at the 1911 Olympia Aero Show, held between 24 March and 1 April. Apart from the various engine changes, to all appearances it had changed very little from its early condition and, by the standards of the day, had proved to be very successful.
  The lateral control was by ailerons aided by differential elevators, operated by sideways movement of the control column. A hand-wheel on the column controlled the rudder. The throttle control was by foot pedal. The undercarriage had spring loaded main legs and buffer wheels at the front; the tail-skid was a long wooden 'kangaroo tail' on which the machine normally rested. Cody could see through the honeycomb radiator, and derived warmth from this and small radiators by his feet. A passenger could be carried on a second plough type seat mounted behind and higher than the pilot.

  No.IIE. (Omnibus) Cody's earlier Michelin Trophy machine was brought back into use at the end of 1911. It flew fitted with an Austro-Daimler engine giving the power that Cody had long been seeking, on 3 January 1912. Twin booms and tail surfaces, reportedly transferred from No.III, were fitted. The performance of the aircraft was greatly improved and later carried Cody and up to four passengers on agricultural type seats mounted in a line at midgap behind him. The aircraft crashed in April 1912 and was not rebuilt.

  Power:
   No.IIA, B and C 60hp Green four-cylinder inline, water-cooled driving a single pusher propeller by Brampton chain. Two engines were fitted briefly but not flown.
   No.IIB. 60-80hp ENV Type C eight-cylinder, water-cooled vee, French-made.
   60hp ENV Type F eight-cylinder, water-cooled vee, British-made driving a 10ft 2in diameter propeller by Brampton chain.
   No.IIE. 120hp Austro-Daimler six-cylinder, inline water-cooled.

  Data
  Span 46ft (49ft including aileron overhang)
  Chord 6ft 6in
  Area 540 sq ft
  Area front 116 sq ft
  elevator
  Area ailerons 101 sq ft
  Gap 8ft 6in
  Length 38ft 6in


P.Lewis British Aircraft 1809-1914 (Putnam)


Cody Michelin Cup Biplane

  After over a year's experience with the British Army Aeroplane No. 1, S. F. Cody produced a new biplane in 1910 which also combined the knowledge gained from the earlier machine.
  A 60 h.p. Green engine was chosen to power the aircraft, which was a pusher on the general lines of its predecessor. Three-bay unstaggered wings of equal span were fitted, the engine being mounted in the centre-section of the lower set and connected to the two-bladed propeller by a chain-drive. Two seats were mounted in tandem, and the Green's radiator was carried above the engine. In front, two bamboo booms bore the large two-piece elevator, and connection to it was by means of bamboo push-rods from the control-wheel. In its original form the machine was without a fixed tail-plane, but a small horizontal surface was fixed later mid-way up the rudder following trials. Ailerons of very generous area were incorporated for lateral control and were mounted in the first instance on the outermost interplane struts, but were subsequently moved inwards and to the rear so that they were carried by the outer pair of struts at the trailing-edge. These modifications were made during the rebuilding of the machine after a crash at Laffan's Plain during June, 1910, after Cody had qualified for Royal Aero Club Aviator's Certificate No. 9 on 7th June, flying the same aeroplane. A change of engine was made from the Green to a 60 h.p. E.N.V. "F", and the radiator was moved forward so that it was positioned between the front bamboo booms which supported the elevators.
  Cody was going to make an attempt on the ?4,000 prize offered by Baron de Forest for the longest flight into Europe from Britain, but finally did not compete. The contest for the British Empire Michelin Cup No. 1 and its attendant cash prize of ?500 appealed, however, to Cody sufficiently for him to enter to set up the longest distance over a closed-circuit before the finishing date for 1910. His first effort resulted in a flight of 94.5 miles around Laffan's Plain in 2 hrs. 24 mins. and set up new all-British distance and duration records. This was, however, beaten by T. O. M. Sopwith, and Cody tried again during the last week of September, covering 115 miles in 2 hrs. 50 mins. in a 20 m.p.h. wind before being forced to the ground from 35 ft. by a gust. The machine was saved from damage by its sturdy undercarriage of twin main wheels, twin nose wheels and long, sprung skid. Cody's last attempt on the Michelin Prize won it for him and was made on 31st December, 1910, the last day of the contest. For his victory he flew for 4 hrs. 47 mins. over a distance of 185.46 miles, at the same time setting up new British records for duration and distance over a closed circuit.
  
SPECIFICATION

  Description: Two-seat pusher biplane. Wooden structure, fabric covered.
  Manufacturer: S. F. Cody, Laffan's Plain, Farnborough, Hants.
  Power Plant: 60 h.p. Green, 60 h.p. E.N.V. "F".
  Dimensions: Span, 46 ft. Length, 38 ft. 6 ins. Wing area, 540 sq. ft.
  Weights: Empty, 2,200 lb. Loaded, 2,950 lb.
  Performance: Maximum speed, 65 m.p.h. Ceiling, 3,000 ft. Range, 200 miles.


Журнал Flight


Flight, July 2, 1910

THE ACCIDENT TO MR. CODY.

  THE sympathy of all interested in British aviation has been extended to Mr. S. F. Cody, in consequence of the untimely accident which befel him on Thursday of last week while testing his new biplane. The machine had been completed on the previous evening, and was noteworthy for the fact that Mr. Cody had abandoned the system of twin propellers previously employed, while he had fitted duplicate engines, so that in the event of one giving trouble its place could be taken by the other. Early on Thursday morning Mr. Cody started up, and as the machine attained a greater speed than anticipated, when running over the ground, he determined on a flight. The machine gracefully rose to a height of 100 ft., and easily circled round the Plain twice. It then traversed the length of Laffan's Plain, but just when gliding down an unexpected gust of wind caught the machine and caused it to fall about 40 ft. to the ground.
  Mr. Cody was pinned beneath the wreckage, and was unconscious when released. He was immediately taken to his home, where he was found to be suffering from concussion of the brain and severe bruises. He made rapid progress, and on Monday was able to leave his bed, when he expressed a hope that he would be fit again in time for the Bournemouth meeting. Except that it is smaller, the new Cody machine has a very similar appearance to the biplane with which Mr. Cody was so successful last year. The engines are two of the 5o-h.p. 4-cyl. Green type.


Flight, July 16, 1910

Mr. Cody Flying Again.

  RAIDED no doubt by his robust constitution and plucky nature Mr. S. F. Cody made a very rapid recovery from his recent severe accident, so much so that on Friday of last week he was able to once more mount his machine and make a satisfactory trial trip, about three miles in length; before packing up the machine for transport to Bournemouth, where he was flying on Wednesday.


Flight, September 10, 1910

Mr. S. F. Cody in the Air Again.

  AT the latter end of last week, Mr. S. F. Cody made a successful flight at Aldershot with his new biplane.


Flight, September 17, 1910

Mr. Cody Again Flying.

  SEVERAL times during last week Mr. S. F. Cody was practicing on his new biplane. On Tuesday he made a fine flight at Aldershot, passing over South Camp, the Long Valley, Bourley Woods, Pyestock, Laffan's Plain and Farnborough, being in the air about 25 mins. in all. On Friday again he was up for about half an hour, flying round the district, and altogether his very substantial machine is shaping well.


Flight, October 1, 1910

A Good Flight by Cody.

  IN the course of a forty minute flight on Tuesday evening, at Farnborough, Mr. S. F. Cody was mostly flying across country. In the afternoon he made a shorter trip with Mr. Mervyn O'Gorman, Superintendent of the Balloon Factory, as a passenger.


Flight, November 12, 1910

THE CODY BIPLANE.

  AMONG pioneers in aviation S. F. Cody deserves much credit. He has fought an up-hill fight against great odds, and he has forced success to come to him as a reward not only for perseverance but for real original work. Alone among the designers of aeroplanes has he succeeded in building a really large machine, and if there are some who have been wont, facetiously, to call it the "flying cathedral," nevertheless, their humour is born of admiration, for the machine does fly, and in the hands of its designer oftentimes performs remarkably well. This particular department of design - the large-sized aeroplane - S. F. Cody has made particularly his own, and he intends to devote the greater part of his private time to its further development, although now that he has decided to place his machine on the market commercially, the standard models will be built on smaller lines. Two sizes have so far been decided upon, the smaller of which, fitted with a 30-35-h.p. engine, will be sold for L1,000, and the larger, fitted with a 50-60-h.p. engine, for L1,200. In both cases flights will be guaranteed, and the purchasers will be trained as pilots free of charge, or they can have a professional pilot trained for them if they do not wish to control the machine themselves. So far, however, we have yet to meet the sportsman aviator and his paid chauffeur - he is a type unborn - but he will put in an appearance later on, sure enough.
  From a practical point of view, the Cody biplane is remarkable mainly for its strength. It is subjected to very severe strains on Laffan's Plain, over which Mr. Cody has secured flying rights, and the starting ground itself is uneven enough to give a great machine like this a very severe jolting. It is, therefore, to the undercarriage that the eyes of the engineer are almost inevitably directed after he has taken in at a glance the general proportions of the structure that it has got to carry. The chassis in question is an interesting and ingenious piece of work; it supports the machine on the ground by the aid of two pneumatic-shod wheels and a trailing skid arranged "kangaroo-tail" fashion. Between the wheels and joining the trailing-skid is a single central skid that normally remains about 8 ins. clear of the ground. The trailing-skid is reinforced by a top batten, so that it is to all intents and purposes a laminated structure, for all the time that the machine is running over the ground it is constantly pressing on the surface, and acts as a very useful brake after a descent. The main central skid only comes into action if the landing has been so forced as to result in a severe shock, in which case the wheels rise against the pressure of their long helical springs, and allow the full weight of the machine to be directly borne upon the skid. On one occasion quite recently a forced descent was made, and the machine charged a fallen tree trunk. The upturned end of the skid, which is provided with a pair of small wheels, cleared the trunk, and the entire machine glissaded bodily over the obstacle without doing any damage to the chassis, and not very much to the tree itself. Supported above the under chassis are two horizontal bearers to which the spars of the lower main planes are attached, and immediately above these again come two other bearers of less span, which carry the engine. The engine thus rests centrally upon the lower main plane, and it drives the large single propeller by means of a chain.
  Directly in front of the engine, and about on a level with the cylinders, is the passenger's seat, for the Cody biplane is essentially a passenger-carrying machine, while in front and a little below the passenger's seat is the pilot's seat. Both are of the pressed-steel kind commonly employed on agricultural machines, and it has often been rather a surprise to us that Mr. Cody has not provided something a little more luxurious for his own comfort; the passenger can, at any rate, hold on to the framework until the machine is safely in the air.
(To be continued.)


Flight, November 19, 1910

THE CODY BIPLANE.
(Concluded from page 925.)

  CENTRALLY in front of the pilot's seat is a steering-wheel on an inclined column, arranged in exactly the same way as a steering-wheel on a motor car. As far as turning the wheel for steering is concerned, the operations are likewise analogous. The wheel is connected with the rudder, which is carried on an outrigger at the rear of the machine.
  In addition to the rotary motion of the steering-wheel, the steering-column itself is mounted on a universal trunnion about one-third of its length from the bottom, and it is thus capable of acting as a powerful lever for the manipulation of the elevator and balancing planes. The elevator on the Cody biplane differs constructionally from that on any other machine in being divided into two parts, which are placed side by side; each half is connected to the control-lever by means of a bamboo rod, and the connections are such that the two planes can be made to operate in unison or in opposite directions. When they operate in unison the device is an elevator pure and simple, but when one half is tilted and the other dipped the action is supplementary to that of the balancing planes mounted in the gap of the main planes under the trailing edge. This double elevator, and its use as a balancer, is quite a special feature of the Cody machine, and is one of the several original ideas of its designer. The balancing action is obtained by a sideways motion of the steering-column, which so thrusts on the bamboo connections of the elevators as to move these two members in opposite directions. Simultaneously a supplementary mechanism, consisting of a rock-shaft and a lever, pulls down the trailing edge of one of the balancers against the action of a spring. The arrangement of the balancing-planes on the Cody biplane is such that they are normally held in a horizontal position by springs, and only one of them can therefore be pulled into a position of positive lift by the control; the other balancer, although it may be dipped by the action of the spring, cannot exert a downward thrust, by virtue of this attitude, of a greater magnitude than the springs themselves can support. Interconnected with the balancer mechanism is the rudder - which, as already explained, is capable of independent operation by turning the steering-wheel - and this member is likewise put over in synchronism with the balancing movements. It will be observed, as an outstanding feature of the Cody control, that the balancing forces are brought to bear upon the machine at several points, and it can be readily appreciated that in large aeroplanes of this kind such a feature may be very desirable in order to guard against failure through undue local stress. With the exception of the rather small horizontal tail plane, which is quite flat - and can really almost be regarded more as a member for trussing the rudder, to which it is permanently fixed, than as a factor of great importance in the stability of the machine - all the planes on the Cody biplane are cambered to carry load. And, in connection with the camber of the main planes, there is another original feature which it is only fait to designate as the "Cody curve."
  The section of the main planes is very peculiar, and it is rather curious that the peculiarity in question would scarcely ever be observed even by the expert eye, for it is scarcely visible on the finished machine, although very pronounced in an individual rib. One of the accompanying sectional sketches shows a main plane rib, and it will be noticed that the underside is cambered more abruptly than the top side, so that the two laths of which the rib is built up touch one another at a point about one-third of the chord from the leading edge. The attitude of the main planes in respect to the normal axis of flight is such that the upper surface is practically tangential to the line of flight in the vicinity of the leading edge, consequently the lower surface has a dipping front edge and the upper surface has not. Mr. Cody claims for this particular system of construction that it produces the most efficient plane that he has ever tried.
  The main planes are built up in sections of 8 ft. span each, and they are divisible into these sections when the machine is dismantled or transport. The joint between sections is completed by a rectangular steel sleeve, and the spigoting ends of the spars are fitted with steel ferrules.
  Steel traps are also employed to brace the spars to the main ribs, which occur at these joints. The upright struts separating the upper and lower main planes coincide with the main ribs, and a very ingenious fastening has been employed for their attachment. The struts themselves are of stream line section, and their tapered extremities are spliced into hollow steel ferrules. The ferrule rests upon the cylindrical collar of a specially shaped bolt that passes through the steel strap binding the main spar to the main rib, and has, above the collar, a spherical head that is enclosed by the ferrule. A bolt fastens the ferrule to the spherical head of the bolt, but the joint is essentially a loose connection, and in principle belongs to the ball-socket type. The remainder of the bracing is, of course, effected by steel wires arranged diagonally, and it is also important to remark that the end thrust on the main spars is taken by diagonal wires that tie the spars to the axle of the undercarriage.
  When the machine rises off the ground the pressure of the springs used for the suspension of the wheels thrusts down upon these diagonal tie wires, and puts 2 cwt. of tension on to them.
  Silver spruce is mainly used in the construction, but the outriggers carrying the elevator and tail are of bamboo. The tail outrigger is hinged, so that the tail can be folded against the main planes in order to save room in accommodation. The undercarriage is made entirely of hickory.
  The power plant on the Cody biplane, as illustrated, consists of a 65-h.p. E.N.V. engine, which drives by a single chain a propeller of 10 ft. 2 ins. diameter and to ft. 8 ins. pitch. The speed of the propeller is 600 r.p.m. when the engine is running at 1,200 r.p.m. One very interesting point in connection with the machinery on the Cody biplane is the presence of a radiator immediately in front of the pilot, and Mr. Cody asserts that he has found great benefit from this in cold weather through the air being slightly warmed before it strikes his body. The degree to which aeroplane pilots suffer from the cold while flying is sufficiently well-known to make an idea of this sort well worthy of consideration.
  The following summary of some of the principal dimensions and minor details of construction will supplement the data given on the full-page drawing. The span of the main plains is 46 ft., and the main spars have an inverted dihedral of 9 ins. The chord is 6 ft. 6 ins., and the camber 4 ins. in height one third from the leading edge. The gap is 8 ft. 6 ins. The whole of the centre portion of the machine is designed to be accommodated in a railway truck without dismantling. The centre of gravity is located approximately on the front spar. With the exception of a few fittings in the centre of the machine, aluminium is not used in the construction. In every case where bamboo is employed the cane is bound with cord in the middle of each section. The upper bamboo strut carrying the elevator is 3 ins. in diameter, and those beneath are 2 ins. in diameter each. The bamboo poles used for operating the elevator are about 1 1/2 ins. in diameter. The vertical struts in the gap of the main planes have a 4 3/4 by 1 1/8 in. section. They weigh 5 1/2 lbs. each, including the nuts and bolts at their extremities. Between the upper and lower surfaces of the main planes the ribs are trussed by diagonal wires. The planes are surfaced with Pegamoid.


Flight, December 31, 1910

THE BRITISH MICHELIN CUP.

Mr. S. F. Cody Scores 115 Miles.

  A VERY fine effort was made by Mr. Cody on the 22nd inst. at Aldershot to win the British Michelin Cup for this year. For 2 hrs. and 50 mins. he steered his large biplane round a marked course over Laffan's Plain, being officially observed on behalf of the Royal Aero Club by Lieut. Fox, R.E. Although Mr. Cody did not beat Mr. Sopwith's duration record of 3 hrs. 12 mins., it is claimed that he covered a greater distance, about 115 miles. A 20-mile wind was blowing, and at the end of the Plain, opposite to that on which the hangar is erected, the wind was particularly gusty and uncertain, with a result that the turn there had to be made very carefully. On one side lay a clump of trees and on the other a flag-post, whilst between these were some iron railings. Time after time the machine escaped the trees by about eight feet, and frequently it was hurled to within six feet from the ground from a height of 30 to 35 ft. This really splendid flight was brought to an equally sensational climax. After being 2 hrs. 50 mins. In the air, the machine was hurled down to the ground with a crash, from a height of well over 35 ft. In spite of this the machine was found to be quite undamaged, and Mr. Cody none the worse for what was probably the finest bit of airmanship he has ever displayed. The biplane was fitted with a Green engine, which ran perfectly throughout the trip.


Flight, January 28, 1911

FROM THE BRITISH FLYING GROUNDS.

Laffan's Plain.

  ON Thursday of last week Mr. de Havilland had his biplane out, and was flying for two hours around Laffan's Plain. Although a stiffish northerly breeze was blowing, it was noticeable that the machine was flying much more steadily than on his previous trip. On Monday Mr. Cody was out, and made several trips with passengers, including Major Sir Alexander Bannerman and Lieut. Cammell. In one of these trips he chased after the "Beta," and succeeded in getting past her.


Flight, March 4, 1911

MODELS.

Model Cody Biplane.

I have pleasure in enclosing a photo of a model of Mr. S. F. Cody's aeroplane. It is built to scale 1/2 in. to 1 ft., from drawings published in your journal November 12th, 1910. The framework is made of white pine, and braced with strong thread.
Wandsworth. F. FISHER.


Flight, April 1, 1911.

Third International Aero Exgibition at Olympia - 1911.

THE EXHIBITS ANALYSED.

<...>
  The Cody biplane is similarly a balanced machine, but it differs from the present Wright type in having an elevator. The elevator on the Cody machine is a cambered plane, and normally carries some of the load for convenience in control, although it is not essential from constructional considerations that it should do so. The engine on the Cody biplane is carried on the lower plane, and, within reason, both it and the pilot can have their positions altered in order to effect any degree of balance that may be required. In practice, as has been mentioned, Mr. Cody prefers that the elevator should be loaded a little, as he considers that it facilitates control.
<...>


Flight, April 8, 1911.

Model Cody.

  I have pleasure in sending you a photo of a model of Mr. Cody's biplane which I have made and flown. I have to thank your paper for some of the chief dimensions. The machine is built of split cane joined with thread and braced with wire. I am experiencing some trouble with the motor. I cannot get the elastic to hold for any length of time. Perhaps one of your readers would be good enough to give some advice.
Westcliff-on-Sea. RIVERS SHERMAN.

P.Lewis - British Aircraft 1809-1914 /Putnam/
Mr. S. F. Cody flying over Laffan's Plain on his modified biplane last week, before the serious accident which befel him later. Mr. Cody, who uses a Green engine, employs only one propeller now.
Cody Michelin Cup Biplane in its first form with 60 h.p. Green.
Журнал - Flight за 1910 г.
Mr. S. F. Cody, as we have recorded, is once more doing practical work with his new biplane, our photograph shows Mr. Cody in flight passing over the Basingstoke Canal.
Журнал - Flight за 1910 г.
BRITISH ARMY AND AERONAUTICS. - Unique photograph of the Army airship "Beta" and Mr. S. F. Cody's new biplane in flight at Aldershot at 7 p.m. on Thursday the week before last. It is gratifying to know that both these craft are equipped with British-built Green engines.
M.Goodall, A.Tagg - British Aircraft before the Great War /Schiffer/
Cody No.IIC and D. The 1910 British Empire Trophy No.l winner with Green engine at Olympia in March 1911.
Журнал - Flight за 1910 г.
Mr. S. F. Cody, on his biplane, competing for the British Michelin Cup at Farnborough Friday of last week. Mr. Cody made a magnificent flight, remaining up for 2 hrs. 24 mins. Mr. Cody also intends to put in a journey for the Baron de Forest Cross-Channel Distance Prize in good time before the worst of the winter weather sets in.
P.Lewis - British Racing and Record-breaking Aircraft /Putnam/
S. F. Cody piloting his biplane with which he won the Michelin Cup No.1 on 31 December, 1910.
Журнал - Flight за 1910 г.
MR. S. F. CODY'S FINE FLIGHT FOR THE BRITISH MICHELIN CUP. - Taking a corner of the course at a fine angle.
Журнал - Flight за 1911 г.
Mr. S. F. Cody on Saturday last carried a passenger on his biplane over Laffan's Plain, standing on the lower main plane, 10 ft. 6 ins. away from himself in the pilot's seat, as seen above in our photograph. Mr. Cody, by this means, wishes to emphasise his claim for the great lateral stability of his machine.
Журнал - Flight за 1911 г.
Mr. S. F. Cody arrives From Brooklands on his biplane for the Hendon Demonstration. - His fine vol plane to the demonstration grounds.
Журнал - Flight за 1911 г.
Mr. S. F. Cody finishing his flight from Brooklands to Hendon.
Журнал - Flight за 1910 г.
Mr. S. F. Cody and Lieut. A . E. Fox, R.E., the official observer on behalf of the Royal Aero Club of Mr. Cody's fine flight for the British Michelin Cup last week. Mr. Cody's biplane is in the background.
Журнал - Flight за 1910 г.
Front view of the Cody biplane, showing the inverted dihedral of the main planes, the extremities of which drop nine inches below the centre.
Журнал - Flight за 1910 г.
Rear view of the Cody biplane.
Журнал - Flight за 1910 г.
Side view of the Cody biplane, showing the arrangement of the under-carriage. Guard wheels are fitted to the extremities of the main plane.
M.Goodall, A.Tagg - British Aircraft before the Great War /Schiffer/
Cody No.II. This smaller biplane, built for use in 1910, survived until April 1912 in various forms. No.IIb illustrated with British ENV Type F engine.
Jane's All The World Aircraft 1913 /Jane's/
CODY (1909). Development of a much earlier machine. This one was a general laughing stock for a long time; but it was the direct predecessor of the machine (not very materially different) which was an easy first in the British Army aeroplane trials, 1912.
Журнал - Flight за 1910 г.
General view of the elevator on the Cody biplane.
Журнал - Flight за 1911 г.
UNDERCARRIAGES AT OLYMPIA. - The Cody.
Журнал - Flight за 1910 г.
On the left one of the balancing planes on the Cody biplane, and on the right the tail of the Cody biplane. The horizontal tail plane is rigidly fixed to the rudder, and moves with it.
Журнал - Flight за 1910 г.
View of the engine and propeller on the Cody biplane.
Журнал - Flight за 1910 г.
Mr. Cody and his propeller.
Журнал - Flight за 1910 г.
Detail view of the under-carriage on the Cody biplane.
Журнал - Flight за 1910 г.
View of the steering-wheel on the Cody biplane.
Журнал - Flight за 1911 г.
Mr. S. F. Cody, with Major Sir Alexander Bannerman, Commandant of the Army Ballon School at Farnborough, as passenger on his biplane, ready for their flight last week,
Журнал - Flight за 1911 г.
Mr. S. F. Cody last week carried three passengers - Mdlle. Armand de Lavette and Messrs. Moreton and Bloomfield - for a flight on his biplane. Our photograph shows the disposition of the party ready for their voyage.
Журнал - Flight за 1910 г.
Front view of the pilot's seat on the Cody biplane, showing Mr. Cody at the wheel. This photograph is taken through the radiator, which protects the pilot to a certain extent in cold weather. That the radiator is no obstruction to the view in this position maybe judged from the above picture.
Журнал - Flight за 1911 г.
Журнал - Flight за 1911 г.
Журнал - Flight за 1910 г.
Diagrammatic sketch illustrating the use of the elevators as balancers on the Cody biplane, and also the simultaneous action of one of the main balancing planes.
Журнал - Flight за 1910 г.
Sketch illustrating how the vertical struts are fastened by a ball-socket joint to the main spars in the Cody biplane. Inset is an illustration of the bolt.
Журнал - Flight за 1910 г.
Sketch illustrating how the steering column simultaneously operates the balancing-planes and the rudder when moved sideways.
Журнал - Flight за 1910 г.
Sketch illustrating how the main ribs are fastened to the main spars by a steel strap on the Cody biplane.
Журнал - Flight за 1910 г.
The Cody rib. Sketch illustrating the peculiar camber of the ribs employed on the Cody biplane. The top surface has its entering edge tangential to the line of flight so that the under surface has a dipping front edge.
Журнал - Flight за 1912 г.
Fig. 6. - Cody Biplane.
P.Lewis - British Aircraft 1809-1914 /Putnam/
Cody Michelin Cup Biplane
Журнал - Flight за 1910 г.
The Cody biplane.