Helicopter anti-torque control system utilizing exhaust gas

Details Helicopter anti-torque control system utilizing exhaust gas Helicopter anti-torque control system utilizing exhaust gas

1991-03-06

1993-08-03

Peters, Jr., Joseph F.

Aeronautics and astronautics

Aircraft, heavier-than-air

Helicopter or auto-rotating wing sustained, i.e., gyroplanes

244 52, 23926529, B64C 1502, B64C 2706, B64C 2782

Patent

active

052321835

ABSTRACT:
A helicopter anti-torque control system which relies on engine exhaust. Included is a force generating apparatus and a force directing apparatus. The force generating apparatus is at least partly driven by engine exhaust. The force directing apparatus takes outside air delivered to it by the force generating apparatus and directs it from the helicopter as a right-side or left-side force.

REFERENCES:
patent: 2486272 (1963-12-01), Gazda
patent: 2518697 (1950-08-01), Lee
patent: 3015460 (1962-01-01), Christenson
patent: 3807662 (1974-04-01), Velazquez
patent: 3957226 (1976-05-01), Daggett, Jr.
patent: 4200252 (1980-04-01), Logan
patent: 4660785 (1987-04-01), Munski
patent: 4948068 (1990-08-01), Van Horn

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