All-axis control of aircraft in deep stall

Details All-axis control of aircraft in deep stall All-axis control of aircraft in deep stall

1976-07-22

1978-07-11

Kelmachter, Barry L.

Aeronautics and astronautics

Aircraft, heavier-than-air

Airplane and helicopter sustained

244 87, 244213, B64C 2728, B64C 1900

Patent

active

040996875

ABSTRACT:
Tilting the stabilizer at an extreme angle to the fuselage, with leading edge down, and varying engine thrust comprise a method for all-axis control of a generally conventional aircraft in deep stall. In an alternative embodiment, tilting the engines upward at an extreme angle to the fuselage and varying engine thrust comprise a method for all-axis control in deep stall.

REFERENCES:
patent: 1533323 (1925-04-01), McCauley
patent: 1964418 (1934-06-01), Alfaro
patent: 2045638 (1936-06-01), Dormoy
patent: 2067634 (1937-01-01), Hafner
patent: 2563757 (1951-08-01), Thorp
patent: 3138353 (1964-06-01), Steiner
patent: 3284027 (1966-11-01), Mesniere

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