The Westland CL.20, also known as the Cierva-Lepere C.31, was a two-seat autogyro designed and built by Westland Aircraft between 1934 and 1938. It followed the unsuccessful Westland C.29, and its design by Georges Lepere with the Cierva Autogiro Company drew on the Cierva-Lepere C.L. 10B, with detailed design by Arthur Davenport and Teddy Petter at Westland. The prototype first flew on 5 February 1935 at Hanworth Aerodrome, flown by Juan de la Cierva. It had a three-bladed folding rotor, a welded steel tube fuselage under a fabric covered light alloy skin, and was powered first by a 70 hp Pobjoy radial engine and later by a more powerful Pobjoy Niagara III. Lateral control was oversensitive and the machine could not climb above about 300 feet, so although six further airframes were made the programme was abandoned and the prototype was scrapped in 1938.
Facts
Engine Class Comparison
Body StyleAircraft (no road body style) 1 Connections
Of Make
Source Westland CL.20 (Wikipedia)
In the Other Atlases
Manufactured By
Also in Business Atlas: the manufacturer of this subject.
Source Westland CL.20 (Wikipedia)LeadQuote, Lead
was a two-seat autogyro designed and built by Westland Aircraft between 1934 and 1938
Sources
1. Westland CL.20 (Wikipedia)
Development, first flight
Juan de la Cierva flew the prototype on its first flight on 5 February 1935
Lead
was a two-seat autogyro designed and built by Westland Aircraft between 1934 and 1938
Design, powerplant
The CL.20 was initially powered by a 70 hp (52 kW) Pobjoy radial engine
Development, fate
the flying prototype was scrapped in 1938
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