Method and apparatus for controlling force fights in a...

Details Method and apparatus for controlling force fights in a... Method and apparatus for controlling force fights in a...

B - Operations, Transporting

64

C

B64C 11/50 (2006.01) B64C 29/00 (2006.01) G05D 17/00 (2006.01)

Patent

CA 2322097

The tilt rotor aircraft comprises an airframe, a pair of wing members coupled to the airframe, a pair of cooperating tilt rotor assemblies carried by the pair of wing members operate in a plurality of modes of operation, a flexible and elongated rotating shaft extending between the pair of cooperating tilt rotor assemblies, a plurality of assemblies for generating at least one signal indicative of an amount of twist on the flexible and elongated shaft, a controller for receiving the at least one signal and generating command signals, and a plurality of actuators for receiving the command signals and for compensating for the twist in the flexible and elongated shaft.

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