Aircraft crosswind control apparatus

Details Aircraft crosswind control apparatus Aircraft crosswind control apparatus

B - Operations, Transporting

64

C

B64C 5/16 (2006.01) B64C 5/08 (2006.01)

Patent

CA 2134407

The present invention relates to a control system for an aircraft to compensate for crosswinds on landings. In one embodiment, the control system includes two mutually identical control surfaces having common end points, respectively; and an actuator to move completely the two mutually identical control surfaces, as needed to compensate for the crosswinds on landing.

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