发明授权
US3593620A Redundant control system for actuation of flight control surfaces 失效
用于执行飞行控制表面的冗余控制系统

Redundant control system for actuation of flight control surfaces
摘要:
A redundant control system including a two-part housing, each part containing one or more output pistons extending into associated cylinders in the other part and two or more separate fluid circuits for actuating different pistons thus to physically isolate one system from another so that should a failure occur in one system it will not affect the other system. The porting to one or more of the cylinders is through the pistons associated therewith.
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