Method and apparatus for minimizing dynamic structural loads of an aircraft

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United States of America Patent

PATENT NO 9242723
APP PUB NO 20150028162A1
SERIAL NO

14125031

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Abstract

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A method of dynamically alleviating loads generated on an aircraft by a disturbance of gust and/or turbulence. The method comprises monitoring, during flight of the aircraft, to automatically detect a disturbance due to gust and/or turbulence and determining an incidence angle or angle of attack of the disturbance. When a disturbance due to gust and/or turbulence is detected, automatically generating control commands for deflecting control surfaces dependent on the incidence angle or angle of attack, and applying the control commands to deflect the control surfaces.

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Patent Owner(s)

  • EADS DEUTSCHLAND GMBH

International Classification(s)

Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Wildschek, Andreas Riemerling, DE 6 63

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