Cierva C.6

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Cierva C.6 in flight

The Cierva C.6 was the sixth autogiro designed by engineer Juan de la Cierva, and the first one to travel a "major" distance. Cierva, the engineer responsible for the invention of the autogiro, had spent all his funds in the research and creation of his first five prototypes. So, in 1923, he turned to the Cuatro Vientos Aerodynamics Laboratory chief, Commander Emilio Herrera, who succeeded in persuading General Francisco Echagüe, the director of the Military Aviation Aeronautics Department, to take over the second stage in the research and development of Cierva's Autogiros.

After several wind tunnel tests, Military Aviation built a Cierva C.6 autogiro in an Avro 504 frame. This machine, piloted by Captain Joaquín Loriga Taboada, performed three flights, all of them in March 1924. One of those flights, the eight minute trip from Cuatro Vientos airfield to Getafe airfield (10.5 km / 7 miles), was considered a giant's step and the "leap into glory" of Cierva's autogiros.

The Cierva C.6 prototype was fitted with ailerons mounted in two small wings, elevators and rudder. This complete three-axis control scheme was needed because the pilot had only limited control over the rotor (See Helicopter rotor). Only the front propeller was powered, so this aircraft could not hover, and could lose control at low speed. The vertical axis rotor spun freely; the faster the autogiro flew, the faster the rotor would spin and the greater lift it produced.

A replica of the Cierva C.6 was built to be shown in Murcia pavilion in Seville Expo '92 World's Fair. That replica can be now be seen in Museo del Aire (Spain), Cuatro Vientos, Madrid, Spain.

Variants

Cierva C.6: Prototype.
Cierva C.6A: Powered by an 82-kW (110-hp) Le Rhône 9Ja rotary piston engine.
Cierva C.6B
Cierva C.6C: Powered by a 97-kW (130-hp) Clerget 9B rotary piston engine. Built in the United Kingdom as Avro Type 574.
Cierva C.6D: Powered by a 97-kW (130-hp) Clerget 9B rotary piston engine. Built in the United Kingdom as the Avro Type 575.

Specifications (C.6)

General characteristics

Crew: 1 or 2
Length: 29 ft 6 in (9 m)
Max takeoff weight: 1,984 lb (900 kg)
Powerplant: 1 × Le Rhône 9Ja 9-cyl. air-cooled rotary piston engine, 110 hp (82 kW)
Main rotor diameter: 32 ft 10 in (10 m)
Main rotor area: 845.5 sq ft (78.55 m²)
Propellers: 2-bladed wooden propeller

Performance

Maximum speed: 54 kn (62 mph; 100 km/h)

References

Original pictures and data of this article were taken from "Museo del Aire", Cuatro Vientos, Madrid, Spain

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v t e Aircraft produced by Cierva/Cierva Autogiro Company/Weir

C.1 C.2 C.3 C.4 C.5 C.6 C.7 C.8 C.9 C.10 C.11 C.12 C.14 C.17 C.18 C.19 C.20 C.21 C.24 C.25 C.26 C.27 C.28 C.29 C.30 C.31 C.32 C.33 C.34 C.37 C.39 C.40 W.4 W.5 W.6 W.9 W.11 W.14 CR Twin

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Cierva C.6

Variants

Specifications (C.6)

References

See also