Aerodynamic surface distension system for high angle of attack f

Details Aerodynamic surface distension system for high angle of attack f Aerodynamic surface distension system for high angle of attack f

1993-02-08

1994-07-05

Huppert, Michael S.

Aeronautics and astronautics

Aircraft control

244199, B64C 500

Patent

active

053260503

ABSTRACT:
A deployable system for assisting flight control under certain flight conditions, such as at high angles of attack, whereby two inflatable membranes are located on the forebody portion of an aircraft on opposite sides thereof. The members form control surfaces for effecting lateral control forces if one is inflated and longitudinal control forces if both are inflated.

REFERENCES:
patent: 2011902 (1935-08-01), Leigh
patent: 2378528 (1945-06-01), Arsandaux
patent: 2601962 (1952-07-01), Douglas
patent: 2912190 (1959-11-01), MacDonough
patent: 2924400 (1960-02-01), Ruget
patent: 2932470 (1960-04-01), Edkins
patent: 3136501 (1964-06-01), Barber
patent: 3586267 (1971-06-01), Ingelman-Sundberg
patent: 4786009 (1988-11-01), Rao et al.
patent: 4917333 (1990-04-01), Murri
"Development of Actuated Forebody Strake Controls . . . " by D. G. Murri et al Oct. 1990 High Angle of Attack Conference-NASA Langley Research Center.

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