Electromechanical actuation system and method

Details Electromechanical actuation system and method Electromechanical actuation system and method

2008-10-08

2011-12-06

Collins, Timothy D (Department: 3644)

Aeronautics and astronautics

Aircraft, heavier-than-air

Helicopter or auto-rotating wing sustained, i.e., gyroplanes

C244S099400, C244S099900, C244S017130, C244S017270

Reexamination Certificate

active

08070091

ABSTRACT:
Electromechanical actuation systems and methods are provided. The electromechanical actuation system includes first, second, and third linear actuators having respective first, second, and third ranges of motion and an output member coupled to the first, second, and third linear actuators such that a position of a selected portion of the output member is based on actuation of the first, second, and third linear actuators.

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