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Cornu helicopter

From Wikipedia, the free encyclopedia
Experimental helicopter built in France
Cornu helicopter No. II
General information
TypeExperimental aircraft
ManufacturerPaul Cornu
Number built1
History
First flight13 November1907

TheCornu helicopter was an experimentalhelicopter built inFrance, and is widely credited with the first free flight of a rotary-wingaircraft when it took to the air on 13 November 1907. Built bybicycle-makerPaul Cornu, it was an open-framework structure built around a curvedsteel tube that carried arotor at either end, and theengine andpilot in the middle. Power was transmitted to the rotors by adrive belt that linked both rotors and spun them in opposite directions. Control was to be provided by cables that could alter the pitch of the rotor blades, and by steerable vanes at either end of the machine intended to direct the downwash of the rotors.

The Cornu helicopter is reported to have made a number of short hops, rising perhaps 1.5 or 2 metres (5–7 feet) into the air and staying aloft for something less than one minute. This was long enough for Cornu to learn that the control systems he had designed were ineffective, and he abandoned the machine soon thereafter.

Modern engineering analyses have demonstrated that the Cornu helicopter could not have been capable of sustained flight. Nevertheless, in order to commemorate the centenary of his achievement, a replica of the helicopter was constructed by theÉcole supérieure des techniques aéronautiques et de construction automobile (ESTACA) and presented to theMusée de l'Air et de l'Espace where it was placed on display on 15 December 2007.

A further replica was built by the Hubschraubermuseum Bückeburg (Helicopter Museum of Bückeburg) to pay homage to the merits of Paul Cornu. Since 13 November 2007 it is shown there.

Specifications

[edit]
Paul Cornu in his open frame helicopter

General characteristics

  • Crew: One pilot
  • Gross weight: 260 kg (573 lb)
  • Powerplant: 1 × Antoinette , 18 kW (24 hp)
  • Main rotor diameter: 2 × 6.00 m (19 ft 8 in)
  • Main rotor area: 56.5 m2 (608 sq ft)

Performance

  • Cruise speed: 0 km/h (0 mph, 0 kn)
  • Endurance: 0 hours 0.5 minutes
  • Service ceiling: 2.0 m (7.0 ft)

References

[edit]
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