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Bracket for mounting/removal of actuators for active vibration control

机译:用于主动振动控制的执行器的安装/拆卸支架

摘要

An active vibration control actuator mount including at least one actuator bracket having an actuator interface member configured to hold one or more active vibration element thereon in one or more predetermined orientations, and an engine mounting structure interface member connected to the actuator interface member, the engine mounting structure interface member being configured to couple the at least one actuator bracket to an engine mounting structure, wherein the at least one actuator bracket is configured for the installation and removal of a respective active vibration element to and from the actuator interface member while a respective one of the at least one actuator bracket remains coupled to the engine mounting structure.
机译:一种主动振动控制致动器支座,包括至少一个致动器支架,该致动器支架具有:致动器接口构件,该致动器接口构件构造成以一个或多个预定方位将一个或多个主动振动元件保持在其上;以及发动机安装结构接口构件,其连接至该致动器接口构件,该发动机安装结构接口构件被构造成将至少一个致动器支架联接到发动机安装结构,其中,至少一个致动器支架被构造成用于将相应的主动振动元件安装到致动器接口构件上以及从致动器接口构件上拆卸相应的主动振动元件,至少一个致动器支架中的一个保持联接到发动机安装结构。

著录项

  • 公开/公告号US9617918B2

    专利类型

  • 公开/公告日2017-04-11

    原文格式PDF

  • 申请/专利权人 THE BOEING COMPANY;

    申请/专利号US201414153238

  • 申请日2014-01-13

  • 分类号F02C7/20;F01D25/04;B64D27/26;

  • 国家 US

  • 入库时间 2022-08-21 13:47:11

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