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Страна: Великобритания

Год: 1912

Единственный экземпляр

Варианты

P.Lewis British Aircraft 1809-1914 (Putnam)

Cody Military Trials Biplane

   After the crash of his monoplane, Cody removed its 120 h.p. Austro-Daimler engine and installed it in a biplane which was then entered as No. 31 in the Military Trials held on Salisbury Plain during August, 1912.
   The machine differed little in appearance from previous Cody biplanes, but featured tapered rudders with small, fixed pairs of horizontal tail surfaces on each side of them. The large six-cylinder engine occupied most of the lower wings' centre-section and drove a propeller 10 ft. 8 ins. in diameter. Four seats were fitted, the pilot occupying the front one with one passenger behind him, the two remaining seats being placed on the lower wings, one on each side of the engine. No ailerons were employed, and wing-warping was used for lateral control. The twin front elevators were carried on bamboo outriggers, with bamboo push-rods controlling them from the enclosed pilot's position. All flying controls were on the single-wheeled column, a foot pedal being used for acceleration of the engine.
   After the numerous tests had been carried out, the Cody biplane was declared the winner of the 1912 Military Trials and was awarded ?5,000 prize money. Its next success was in the contest for the 1912 British Empire Michelin Cup No. 2 and ?600, for which the Austro-Daimler engine was removed and replaced by a 100 h.p. Green to bring the machine into the all-British category to comply with the regulations of the competition. There were no other comers, and Cody won the event for the third year in succession by covering about 220 miles of the cross-country circuit in 3 hrs. 26 mins.
   Dihedral was incorporated later in the wings, and Lt. L. C. Rogers-Harrison, R.F.C., was trained specially to be able to handle the difficult machines, of which two had been ordered for the Royal Flying Corps. On 28th April, 1913, he crashed at Farnborough in the second of them and was killed. The machine differed in having a slight increase in the dihedral, elevators which were mounted slightly higher and rudders which were moved closer together so as to be in the slipstream of the propeller. Both of the R.F.C. aircraft were fitted with 120 h.p. Austro-Daimler engines, and one was shown at the 1913 Olympia Aero Show which had flown for 7,000 miles, afterwards being handed over to the R.F.C. to be used first by No. 2 Squadron and then by No. 4 Squadron.

SPECIFICATION

   Description: Two/four-seat pusher biplane. Wooden structure, fabric covered.
   Manufacturer: S. F. Cody, Laffan's Plain, Farnborough, Hants.
   Power Plant: 120 h.p. Austro-Daimler, 100 h.p. Green.
   Dimensions: Span, 43 ft. Length, 37 ft. 9 ins. Wing area, 430 sq. ft.
   Weights: Empty, 1,850 lb. Loaded, 2,850 lb.
   Performance:
   (120 h.p. Austro-Daimler) Maximum speed, 72.5 m.p.h. Climb, 288 ft. in 1 min., 1,000 ft. in 3.5 mins. Ceiling, 6,00 ft. Range, 336 miles.
   (100 h.p. Green) Maximum speed, 70 m.p.h. Range, 500 miles.
   Price: ?1,500.

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Описание:

  • P.Lewis British Aircraft 1809-1914 (Putnam)
  • M.Goodall, A.Tagg British Aircraft before the Great War (Schiffer)
  • Журнал Flight