Device for increasing the stability of helicopters placed on boa

Aeronautics and astronautics – Aircraft – heavier-than-air – Helicopter or auto-rotating wing sustained – i.e. – gyroplanes

Patent

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Details

244100R, 244115, B64C 2506

Patent

active

052094316

ABSTRACT:
The invention relates to a device for increasing the stability, especially the lateral stability, of a helicopter placed on board (1) having a tricycle landing gear (2, 6), when it is set down on a moving platform.
The device comprises two lateral stabilizers (13), each equipped with a wheel (16) for support on the platform and connected to the structure of the helicopter by an essentially rigid support, comprising a leg (17), about the axis of which the wheel (16) can turn, the leg (17) itself being connected to the structure by a rigid and transverse component which may be a pivot axle if the leg can be raised, or a slidingly fitted arm if the stabilizer (13) is additional. The stabilizers may also be integrated into a towing trolley.
Application to the equipment of helicopters placed on board, having a tricycle landing gear.

REFERENCES:
patent: 2826434 (1958-03-01), Echols
patent: 3049253 (1962-08-01), Cabral
patent: 4537369 (1985-08-01), Perry

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