Method for steering an aircraft

Aeronautics and astronautics – Aircraft – steering propulsion – Fluid

Patent

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Details

244199, 244207, 244214, B64C 1500, B64C 350

Patent

active

042679907

ABSTRACT:
The present aircraft steering method makes use of additional lift gained by ontrolling the separating of vortical flows from the leading edges of the wings for the purpose of controlling the aircraft about its pitch axis, its roll axis, and its yaw axis. The vortical flows are selectively or differentially separated from the leading edge of the wings by raising or lowering leading edge flaps and/or blowing a flowing medium over the wing surfaces substantially in parallel to the leading edge.

REFERENCES:
patent: 1290136 (1919-01-01), Eaton
patent: 2503585 (1950-04-01), Loedding
patent: 3090584 (1963-05-01), Kuchemann et al.
patent: 3480234 (1969-11-01), Cornish
patent: 3831885 (1974-08-01), Kasper
patent: 4161300 (1979-07-01), Schwaerzler et al.

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