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Caudron Type H

From Wikipedia, the free encyclopedia
Caudron Type H
General information
TypeMilitary amphibious biplane
National originFrance
ManufacturerCaudron
Number built2
History
First flightlate 1912-early 1913

TheCaudron Type H was a collective name for three different Caudron designs of 1912–1913. One of these was anamphibious three-seatbiplane built for theFrench military. Two were completed, one appearing at the Paris Aero Salon in November 1912.

Design and development

[edit]

TheCaudron brothers used the designations H and M to distinguishhydravions (seaplanes) frommonoplanes in their catalogue for distribution at the 1912 Paris Salon.[1] The H category included three different designs: a two-seat development of thepusher configurationCaudron-Fabre biplane, built forClaude Graham-White; atractor configurationtwo-bay biplane;[2] and a large, three-seat, three-bay biplane which was the only Caudron seaplane displayed at the Salon.[2][3] Apart from the evidence of a few photographs, rather little detail has survived about the first two but more is known about the Salon aircraft, described below.[2]

Apart from its tractor engine, the Salon machine had the same layout as all other Caudron biplane designs from theType C of 1912 to theG.4 of 1915. Its wings were rectangular in plan apart from their rounded tips; the upper span was 45% greater than the lower. There was nostagger, so the three sets of parallelinterplane struts on each side were vertical.[2][4]Roll control was bywing warping.[3]

In common with the other Caudron biplanes, the Salon Type H did not have a conventionalfuselage. Instead, a pair of girders, each tapering in profile and with two vertical cross-members, were mounted parallel to each other in plan. On all types the upper members were attached to the upper wing; on landplanes the lower member passed under the lower wing and supported the landing wheels, but on Caudron seaplanes they were kept out of the water by joining the lower wing.[2] A rectangular plantailplane was placed just under the upper girder members at the extreme tail, with three small, rectangular vertical tails on its upper surface between the girders in a departure from the Caudron norm.[4]

The three crew were accommodated in a flat-sidednacelle, mounted above the lower wing, with a semi-cowled, 52 kW (70 hp)Gnome Lambda seven-cylinderrotary engine in the nose and the pilot placed at about mid-chord. The aircraft was amphibious, with short, broad, single-steppedfloats, each mounted on pairs of N-form struts under the central wing bays, assisted by two smaller, unstepped floats attached to the lower tailboom girders under the tailplane. The main, underwing floats had single mainwheels largely within them, set about two-thirds of the way back and enclosed above by roughly semicircular covers. The floats were not sprung and the only springing in the wheeled gear was in the pneumatic tyres. The Caudron brotherspatented this arrangement.[2][5]

It is not known if the first of the two examples built had flown before the Type H was exhibited at the Salon in November 1912.[2] It was marked as a military machine, possibly intended for use in theFrench colonial empire, and was received by the French military on 14 February 1913 with serial CC5.[2][5] At least one of the two was modified to have a land undercarriage with pairs of main wheels and a long skid on a wire braced N-form strut under each of the inner interplane struts pairs.[2]

The first example flew at an event hosted by theBoulogne Aero-Club on 14 July 1913, taking off from the beach, though on different, longer floats.[2]

Specifications (1912 Salon)

[edit]

Data from Hauet (2001), p.39[2]

General characteristics

  • Crew: three
  • Length: 10.0 m (32 ft 10 in)
  • Upper wingspan: 14.0 m (45 ft 11 in)
  • Lower wingspan: 9.6 m (31 ft 6 in)
  • Wing area: 35 m2 (380 sq ft)
  • Empty weight: 400 kg (882 lb)
  • Gross weight: 660 kg (1,455 lb)
  • Powerplant: 1 ×Gnome Lambda , 7-cylinderrotary in tractor configuration, 52 kW (70 hp)
  • Propellers: 2-bladed Integrale[3]

Performance

  • Maximum speed: 80 km/h (50 mph, 43 kn) . Flight[3] gives 97 km/h (60 mph)
  • Time to altitude: 15 min to 500 m (1,640 ft)

References

[edit]
  1. ^Hauet, André (2001).Les Avions Caudrons. Vol. 1. Outreau: Lela Presse. p. 2.ISBN 2 914017-08-1.
  2. ^abcdefghijkHauet (2001).Les Avions Caudrons. pp. 39–42.
  3. ^abcd"A Tabular Description of the Aeroplanes at the Fourth Paris Salon".Flight.IV (45): 1023. 9 November 1912.
  4. ^ab"Quatrième Exposition Internationale de Locomotion Aérienne".L'Aérophile.20 (22): 509. 15 November 1912.
  5. ^ab"The Paris Aero Salon - Caudron".Flight.IV (44): 999. 2 November 1912.
Caudron aircraft
Letter designators & Early
Gaston Caudron (G) types
René Caudron (R) types
Numerical Designations
Messerschmitt-Caudron
Names
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