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Actuator, actuator system and aircraft landing gear

机译:执行器,执行器系统和飞机起落架

摘要

An actuator which is operable in response to one of an electrical and an electro-mechanical input signal is provided. The actuator includes an outer casing defined about a central axis, an output shaft disposed within the casing, the output shaft being axially moveable over a stroke length. Further, the actuator also includes a drive mechanism co-operable with the output shaft to drive the output shaft along a part of the stroke length, wherein the actuator is configured such that the output shaft is drivable along all or part of the remainder of the stroke length by external loading while being unconstrained by the drive mechanism.
机译:提供了一种致动器,其可响应于电和机电输入信号之一而操作。该致动器包括围绕中心轴线限定的外壳,设置在该外壳内的输出轴,该输出轴可在行程长度上轴向移动。此外,致动器还包括可与输出轴配合以沿行程长度的一部分驱动输出轴的驱动机构,其中,致动器构造成使得输出轴可沿马达的其余部分的全部或一部分驱动。在不受驱动机构约束的情况下,由外部负载产生的行程长度。

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