Operation of a helicopter

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

Patent

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Details

244207, 244 53R, B64C 2700

Patent

active

056496788

ABSTRACT:
In a helicopter having a main rotor, a tail boom and a circulation control slot along one side of the tail boom, and a thruster which is selectively directable at either side or both sides of the rear end of the tail boom, anti-torque and yaw control are effected by generating separate air flow streams of different pressures by means of separate pressure means and conducting said separate air flow streams at said different pressures in separate passages to respectively the circulation control slot and to the thruster.

REFERENCES:
patent: 2518697 (1950-08-01), Lee
patent: 2918232 (1959-12-01), Lippisch
patent: 2932468 (1960-04-01), Kappus
patent: 3990811 (1976-11-01), Danielson
patent: 4200252 (1980-04-01), Logan et al.
patent: 4828203 (1989-05-01), Clifton et al.
patent: 4928907 (1990-05-01), Zuck
patent: 4948068 (1990-08-01), Vanttorn
patent: 5067668 (1991-11-01), Zuck
patent: 5205512 (1993-04-01), Rumberger
patent: 5232183 (1993-08-01), Rumberger
patent: 5240205 (1993-08-01), Allongue

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