| Wibault 260 R.2 | |
|---|---|
 | |
| Role | Long range reconnaissance aircraft |
| National origin | France |
| Manufacturer | Société des Avions Michel Wibault |
| Designer | Michel Wibault |
| First flight | S1 1930 |
| Number built | 2 |
The Wibault 260 R.2 was a contender for a French government contract for a long range, two seat reconnaissance aircraft, issued in 1928. There were eight prototypes in the 1931-2 contest and the Wibault was not selected for production.
The French R.2 specification of 1928 called for an all-metal two seat reconnaissance aircraft, fast and with a rapid climb rate and large radius of action. It led to prototypes from eight manufacturers, the Amiot 130, Breguet 33, Latécoère 490, Les Mureaux 111, Nieuport-Delage Ni-D 580, Potez 37, Weymann WEL-80 and the Wibault 260. One of the terms of the specification required the manufacturers to use a Hispano-Suiza 12Nb water-cooled V-12 engine. [1] [2]
The Wibault 260 was an all-metal monoplane with a parasol, cantilever wing. In plan the wing was largely trapezoidal out to blunt tips, with most of the sweep on the trailing edges, though it had a short span centre-section with an unswept leading edge and a deep cut-out in the trailing edge to improve the field of view from the cockpit. The thickness/chord ratio of the outer panels decreased progressively towards the tips. There was no dihedral. High aspect ratio ailerons filled the entire trailing edges. Wing and fuselage were joined by a pair of outward leaning, approximately N-form cabane struts between the outer ends of the centre-section and the upper fuselage. The wings were built around two spars and dural skinned. [3]
Its fuselage was constructed entirely in duralumin, with four longerons which defined its rectangular cross-section. Its water-cooled 480 kW (650 hp) Hispano-Suiza 12Nb upright V-12 engine was in the nose within a pointed engine cowling with bulges around the two cylinder blocks. Its shallow radiator curved around the underside of the forward fuselage at the rear of the engine. A 500 l (110 imp gal; 130 US gal) fuel tank was behind the fire wall. Aft, the pilot's cockpit was under the wing cut-out with a forward view under the wing and equipped with two fixed machine guns firing through the propeller disk. The observer/gunner's position was immediately behind the pilot and was equipped with photographic and radio equipment, together with two flexibly mounted machine guns. [3]
The empennage was conventional, with a triangular plan tailplane mounted near the top of the fuselage and braced on each side with a strut to the lower fuselage. Its angle of incidence could be adjusted in flight by the pilot. The elevators were narrow and rectangular apart from central cut-outs to allow operation of the trapezoidal rudder, which extended down to the keel and was mounted on a triangular fin. [3]
The Wibault 260 had fixed, conventional steel landing gear with a track of 2.60 m (8 ft 6 in), its wheels fitted with brakes. Upward sloping half-axles met centrally under the fuselage at the vertex of a transverse V-strut and, on each side, a faired, long displacement oleo leg and a faired drag strut, both from the lower fuselage longeron, carried the outer end of the axle. The tailskid also had an oleo strut. [3]
The date of the Wibault 260's first flight is not known but it was flying by mid-1930. [4] In early November 1930 Ribière gave a "trés belle" (very fine) demonstration of it at Villacoublay. [5]
The S.T.I.Aé Concours des avions de grande reconnaissance (Long range reconnaissance aircraft competition) at Villacoublay began in April 1931 [2] and, unusually, lasted about a year. [6] The French government had paid in March 1930 for two Wibault 260s to be built for the contest [7] but the winner was the ANF Les Mureaux 111, [6] so the Wibault did not go into production.
Data from Les Ailes August 1930 [3]
General characteristics
Performance
Armament
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