Movatterモバイル変換


[0]ホーム

URL:


Jump to content
WikipediaThe Free Encyclopedia
Search

Cierva C.7

From Wikipedia, the free encyclopedia
C.7
Cierva C.7 atL'Aeronatique in January 1927
RoleExperimental autogyro
Type of aircraft
ManufacturerLoring Workshops
DesignerJuan de la Cierva
First flightNovember 15, 1926
Primary userSpanish Air Ministry

TheCierva C.7 was an experimental autogiro designed byJuan de la Cierva and built in the late 1920s.

Development history

[edit]

On January 7, 1927, the Cierva C.6C was flying at 30 m (98 ft), when one of its blades detached from the hub. The autogyro began to descend vertically at almost normal speed for autorotation. At 6 m (20 ft) from the ground, a second rotor blade came off. The pilot Courtney was fortunately only slightly bruised. The reaction of the BritishAir Ministry to this accident, was the suspension of all autogyro flights in Great Britain until a solution was found to the detachment of the blades in flight.

Juan de la Cierva designed a newrotor with a secondlinkage on the hub to correct the overstrain to eliminate cyclic stresses. To the existing one of abatement that eliminated the problem of lift asymmetry, a second one was added, which was designated as adrag joint, which allowed the blade to oscillate in the plane of rotation. He could not carry out the tests with this new configuration with the prohibition against flight still in place, so de la Cierva moved toMadrid to work on the C.7; there it was fitted with a new double-jointed rotor head. After carrying tests, including flights with Juan de la Cierva as a passenger, it was concluded that the appropriate solution had been reached. In addition it gave a much smoother flight.[1][2]

Variants

[edit]
C.7
Two-seater gyroplane with a 300 hp Hispano Suiza engine.
C.VII
Denomination given by the Loring company.

Specifications (C.6)

[edit]

Data from[3]

General characteristics

  • Crew: one
  • Length: 29 ft 6 in (9 m)
  • Max takeoff weight: 1,984 lb (900 kg)
  • Powerplant: 1 ×Hispano-Suiza 8F 9-cyl. air-cooled rotary piston engine, 300 hp (220 kW)
  • Main rotor diameter: 32 ft 10 in (10 m)
  • Main rotor area: 845.5 sq ft (78.55 m2)
  • Propellers: 2-bladed fixed-pitch wooden propeller

Performance

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

See also

[edit]

Related lists

References

[edit]
Wikimedia Commons has media related toCierva C.7.
  1. ^Enciclopedia Ilustrada de la Aviación: Vol.5 (Edit. Delta ed.), Barcelona, 1983, p. 1153,ISBN 84-85822-52-8{{citation}}: CS1 maint: location missing publisher (link)
  2. ^"Página nueva 2".tiroalcorcon.com. Archived fromthe original on 27 August 2008. Retrieved12 January 2022.
  3. ^Volumen número 12 de la colección Arca del Ateneo. (1996,ISBN 84-88175-10-8).
Cierva aircraft
Juan de la Cierva (Spain)
Cierva Autogiro Company (UK)
Weir Group
Cierva Autogiro Company and Rotorcraft
Retrieved from "https://en.wikipedia.org/w/index.php?title=Cierva_C.7&oldid=1106294100"
Categories:
Hidden categories:

[8]ページ先頭

©2009-2025 Movatter.jp