JUAN DE LA CIERVA
Cierva's first successful autogyro
'Juan de la Cierva' (21 September 1895 – 9 December 1936) was a Spanish civil engineer and pilot. His most famous accomplishment was the invention in 1919 of the Autogiro, a type of aircraft that later came to be called an autogyro. After four years of experimentation, la Cierva developed the articulated rotor which resulted in the world's first successful flight of a stable rotary-wing aircraft in 1924 with his La Cierva C-6 prototype.
De la Cierva was born in Murcia, Spain to a wealthy family. After several successful experiments with aviation as a boy, he eventually earned a civil engineering degree. He moved to England in 1925, where with the support of Scottish industrialist James G. Weir, he established the 'Cierva Autogiro Company'.
At the outbreak of the Spanish Civil War, De la Cierva supported the forces of Francisco Franco, helping the rebels to obtain the De Havilland DH-89 'Dragon Rapide' which flew General Franco from the Canary Isles to Morocco.
De la Cierva died in an airliner accident near London at age 41. On the morning of 9 December 1936, he boarded a Dutch DC-2 of KLM at Croydon Airfield, bound for Amsterdam. After some delay caused by heavy fog, the airliner took off at about 10.30 a.m., but it crashed on the roof of a building at the end of the runway and was set on fire.
| Contents |
| Legacy |
| See also |
| External links |
Legacy
Technology developed for the Autogiro was utilized by experimenters in the development of the helicopter, the first fully successful example of which, the FA-61, was flown in 1936 by Cierva Autogiro Company licensee Focke-Achgelis. The Autogiro also led directly to the Cierva C.38 Gyrodyne, which utilized a powered rotor for hovering and low speed flight, and a side-mounted propeller for torque correction and propulsion in cruise flight. As airspeed increased, propeller power increased while rotor power automatically decreased which reduced rotor collective pitch to autorotative angle with the rotor remaining parallel to the flightpath. As airspeed reduced, propeller power decreased while rotor power automatically increased which increased rotor collective pitch to non-autorotative angles. The Fairey Gyrodyne, first flown in 1948, established the superiority of this configuration over that of the helicopter, which De la Cierva consistently rejected as too mechanically complicated, even though he agreed with the requirement for hovering performance.
See also
★ La Cierva C-9
★ La Cierva C-6
External links
★ U.S. Centennial of Flight - Juan de la Cierva
This article provided by Wikipedia. To edit the contents of this article, click here for original source.
psst.. try this: add to faves

العربية
中国
Français
Deutsch
Ελληνική
हिन्दी
Italiano
日本語
Português
Русский
Español