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Dewoitine D.480

From Wikipedia, the free encyclopedia
Dewoitine D.48
RoleSide-by-side sport andtraining aircraft
Type of aircraft
National originFrance
ManufacturerConstructions Aéronautiques Émile Dewoitine
First flight1932
Number built2

TheDewoitine D.480 was a French single engineside-by-side sports andtraining aircraft built in the early 1930s. Two were completed and flew with several differentradial engines. One remained active through the 1950s.

Design

[edit]

The D.480 was designed to a government programme for a side-by-side trainer forflying schools. It was of mixed construction, with a wooden wing and metalfuselage. Its one-piececantileverlow wing wastrapezoidal out toelliptical tips, tapered strongly in thickness from root to tip and had significantdihedral. The wing was built around a singlespruce andplywoodspar and entirely ply skinned. Highaspect ratioailerons filled over half thetrailing edges, with ground-adjustable trimmingflaps near the roots.[1][2]

The metal-skinned fuselage was based on fourlongerons, giving it a slightly rounded square cross-section. It was always intended that the D.48 series should be able to accommodate a variety of radial engines in the 67–112 kW (90–150 hp) range and the first prototype, type D.480, had a 71 kW (95 hp)Salmson 7Ac seven cylinder engine in the nose, enclosed in acowling which exposed its cylinder heads for cooling.[1] A second example, designated D.481, was built at the same time as the first and was identical apart from its 75 kW (100 hp)Lorraine 5Pa radial, similarly cowled.[3] Pilot and pupil sat side by side with dual controls in an opencockpit close to the wingleading edge. Behind them the fuselage tapered to a convention tail. The horizontal tail was roughly elliptical in plan and mounted on top of the fuselage, far enough forward to need only a small space between theelevators forrudder movement. Its deep, full rudder was hinged on a blunted triangularfin.[1]

The D.480 had afixed, conventional undercarriage with a track of 2.80 m (9 ft 2 in). Each mainwheel was mounted on a stub axle at the vertex of a V-strut hinged on the lower fuselage longeron, with a near-vertical sprung leg, with anoleo strutshock absorber, to the wing spar. The tailwheel was on a long, hinged leg close to the rear fuselage with a short, vertical shock absorber.[1]

Development

[edit]

Both examples had official pre-flight structural checks made in January 1932;[4] the D.481 at least flew that same month.[3] They were registered asF-AKFF andF-AKFG. One of the pair was displayed at the December 1932Paris Aero Salon after receiving a 101 kW (135 hp)Salmson 9NC nine-cylinder radial, housed under a long-chord,NACA-stylecowling.[5][6] The type number of this variant is not known for certain but recreated French civil aircraft registers show that both spent part of the lives as D.482s.[7]

The register also indicates that one flew for a time as a military aircraft;[8] Dewoitine had argued that it would make a good introductorytrainer.[1] It returned to the civil register asF-AQMO in May 1938, operated by an aero club nearToulouse.[8] It survivedWorld War II and in the 1950s, its engine uncowled, carried advertising material for a biscuit manufacturer.[9]

F-AKFG eventually became a type D.483,[7] though little is known about this variant.

Variants

[edit]
Dewoitine D.480
Salmson 7Ac powered, as described. Registered asF-AKFF.
Dewoitine D.481
75 kW (100 hp)Lorraine 5Pa five cylinder radial engine with three blade propeller. Registered asF-AKFG.
Dewoitine D.482
D.480 and D.481 re-designated.
Dewoitine D.483
Second D.482 re-designated.

Specifications (D.480)

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Data from Les Ailes June 1932[1]

General characteristics

  • Crew: Two
  • Length: 7.395 m (24 ft 3 in)
  • Wingspan: 12.700 m (41 ft 8 in)
  • Height: 2.830 m (9 ft 3 in)
  • Wing area: 19 m2 (200 sq ft) including 2 m2 (22 sq ft) of fuselage underside
  • Empty weight: 646 kg (1,424 lb) equipped, without fuel
  • Gross weight: 909 kg (2,004 lb)
  • Fuel capacity: 120 L (26 imp gal; 32 US gal)
  • Powerplant: 1 ×Salmson 7Ac 7-cylinder air-cooledradial, 71 kW (95 hp)
  • Propellers: 2-bladed

Performance

  • Maximum speed: 175 km/h (109 mph, 94 kn) at ground level
  • Minimum control speed: 84 km/h (52 mph, 45 kn)
  • Range: 600 km (370 mi, 320 nmi)
  • Service ceiling: 4,500 m (14,800 ft)

References

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  1. ^abcdefFrachet, André (23 June 1932)."Le monoplan Dewoitine D. 48".Les Ailes (575): 3.
  2. ^"Le biplace côte à côte Dewoitine 480".L'Aéronautique (385): 360. December 1932.
  3. ^abBruno Parmentier."Dewoitine D.481". Retrieved18 February 2004.
  4. ^Frachet, André (14 January 1932)."D'aérodrome en aérodrome - À Toulouse-Francazal".Les Ailes (552): 12.
  5. ^Hirschauer, L.; Dolfus, Ch (1933).Le Année Aéronautique 1932-1933. London: Dunod. p. 214.
  6. ^Frachet, André (December 1932)."L'avion école Dewoitine".L'Aérophile.40 (XII): 360.
  7. ^abMartin, Bernard; Sparrow, Dave; Espérou, Robert (September 2012). "The French civil register from 1922".Air Britain Archive: 2012/135.
  8. ^ab"Golden Years of Aviation". Retrieved2 November 2015.
  9. ^"Dewoitine 482 no.1 F-AQMO". Retrieved13 July 2016.
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