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Westland CL.20

Lighter-Than-Air Craft and Rotorcraft

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
Year
1935 1
Engine Class
Piston 1
Status
Scrapped 1
Comparison
Body Style
Aircraft (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)Lead
Quote, 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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