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Cierva C.8

From Wikipedia, the free encyclopedia

C.8
The Cierva C.8 in flight
Roleexperimentalautogyro
Type of aircraft
ManufacturerCierva
DesignerJuan de la Cierva
First flight1926
Number built6

TheCierva C.8 is an experimentalautogyro built byJuan de la Cierva in England in 1926 in association withAvro. Like Cierva's earlier autogyros, the C.8s were based on existing fixed-wing aircraft fuselages – in this case, theAvro 552.

Design and development

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The first example, theC.8R (known to Avro as theType 587) was a rebuild of theC.6D, fitted with stub wings and paddle-shaped main rotor blades. This was followed by the new-builtC.8V (orType 586) that was eventually converted back into an Avro 552 after testing. The next model was the definitiveC.8L prototype (orType 575). The Mark II was based on the Lynx-enginedAvro 504N two-seat trainer.[1]

By now, Cierva's efforts were attracting the attention of buyers. The first customer was the BritishAir Ministry, which placed an order for a machine in 1927. This was completed as theType 611, test flown byBert Hinkler atHamble and then delivered to theRoyal Aircraft Establishment by Cierva himself in Britain's first cross-country rotorcraft flight on 30 September that year. The next example was purchased by Air CommodoreJames G. Weir, chairman of Cierva, and flown in the 1928King's Cup Air Race before being used to make demonstration flights around continental Europe.

The two final C.8s were sold in 1928, one to the Italian government, and one to AmericanHarold Pitcairn, who would go on to purchase manufacturing rights for the United States. TheC.8W bought by Pitcairn would make the first autogyro flight in the United States atWillow Grove, Pennsylvania, on 18 December 1928. The C.8W is the oldest autogyro in the United States.[2]

As of 2007, two examples are extant: Weir's machine preserved at theMusée de l'Air et de l'Espace in Paris, and Pitcairn's at theNational Air and Space Museum in Washington, DC.

Variants

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C.8R
C.6D fitted with new wings and rotor blades, powered by a 97-kW (130-hp)Clerget engine. (1 converted)
C.8V
Two-seat model, powered by a 134-kW (180-hp)Wolseley Viper piston engine.
The C.8 on display at theFrench Air and Space Museum
C.8L
(4 built)
C.8L Mk II
Fitted with short-span wings, powered by anArmstrong Siddeley Lynx IV radial piston engine. The aircraft took part in 1928King's Cup Air Race. Built in the United Kingdom as theAvro Type 617. (1 built)
Weymann-Lepère C.18
Version of C.8L Mk II built under license in France.[3]
C.8L Mk III
Two aircraft built for the Italian government in 1928.
C.8W
Powered by a 168-kW (225-hp)Wright Whirlwind radial piston engine. This version was built forHarold Frederick Pitcairn. Original designationC.8L Mk IV. (1 built)

Specifications (C.8 Mark II)

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Data from Jane's all the World's Aircraft 1928,[4] Flight 5 July 1928 p. 543[1]

General characteristics

  • Crew: 1
  • Capacity: 1 plus 50 lb (23 kg)
  • Length: 36 ft (11 m)
  • Wingspan: 23 ft 2 in (7.06 m)
  • Height: 14 ft 9 in (4.50 m)
  • Empty weight: 1,735 lb (787 kg)
  • Gross weight: 2,380 lb (1,080 kg)
  • Fuel capacity: 24 imp gal (29 US gal; 110 L)
  • Powerplant: 1 ×Armstrong Siddeley Lynx IV 7-cylinder air-cooled radial piston engine, 200 hp (150 kW)
  • Main rotor diameter: 39 ft 8 in (12.09 m)
  • Main rotor area: 1,236 sq ft (114.8 m2)
  • Propellers: 2-bladed wooden fixed pitch propeller

Performance

  • Maximum speed: 100 mph (160 km/h, 87 kn)
  • Cruise speed: 85 mph (137 km/h, 74 kn)
  • Minimum control speed: 25 mph (40 km/h, 22 kn)
  • Endurance: 3 hours at cruising speed
  • Rate of climb: 500 ft/min (2.5 m/s)
  • Power/mass: 11.9 lb/hp (7.24 kg/kW)

References

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Notes
  1. ^abFlight 5 July 1928, p. 543
  2. ^Charnov, Dr. Bruce H. "A Critical Re-Examination of the Franklin Institute Rotating Wing Aircraft Meeting of October 28 – 29, 1938Archived 13 May 2016 at theWayback Machine" page 3-4. 62nd Annual Forum,American Helicopter Society, May 2006. Accessed: 30 December 2013.
  3. ^"Weymann-Lepère C.18 - Stingray's List of Rotorcraft".
  4. ^Grey, C.G., ed. (1928).Jane's all the World's Aircraft 1928. London: Sampson Low, Marston & company, ltd. p. 262c.
Bibliography

External links

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Media related toCierva C.8 at Wikimedia Commons

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