首页> 外国专利> Mounting to actuate a rotatable axis component, mounting to control an aircraft, canar mounting to an aircraft, aircraft, method of rotating an axis rotatable component of rotation

Mounting to actuate a rotatable axis component, mounting to control an aircraft, canar mounting to an aircraft, aircraft, method of rotating an axis rotatable component of rotation

机译:用于致动可旋转的轴线部件的安装,用于控制飞机的安装,用于飞机的运河安装,飞机,旋转轴线可旋转部件的方法

摘要

"ASSEMBLY TO MAKE AN AIRCRAFT COMPONENT AROUND A ROTATION SHAFT, ASSEMBLY TO CONTROL AN AIRCRAFT, ASSEMBLY 39 TO AN AIRCRAFT, AIRCRAFT, METHOD OF MAKING AN ACCESSORIES AROUND A ROTATION SHAFT ". Equipment and methods for operating rotatable components are disclosed. In one embodiment, an assembly for actuating a rotatable member includes an extendable actuator having a first and a second end, and a drive member having a first portion pivotally coupled to the second end, and a second end. non-pivotally coupled portion with the rotatable component. The second part of the drive member is situated away from the first part. The drive member further includes a third part spaced apart from the first and second parts in a nonlinear orientation. The assembly further includes a reaction pivot having a pivotably coupled anchor end to the first extendable actuator end, and a pivotably coupled drive end to the third part of the drive member.
机译:“组装成围绕旋转轴的飞机组件,组装控制飞机,将<39>组装成旋转轴的附件的方法”。公开了用于操作可旋转部件的设备和方法。在一个实施例中,一种用于致动可旋转构件的组件包括:具有第一端和第二端的可延伸致动器;以及驱动构件,其具有可枢转地联接至第二端的第一部分;以及第二端。与可旋转部件的非枢轴连接的部分。驱动构件的第二部分远离第一部分。驱动构件还包括第三部分,该第三部分以非线性取向与第一部分和第二部分间隔开。该组件还包括反作用枢轴,该反作用枢轴具有可枢转地联接至第一可延伸致动器端的锚固端和可枢转地联接至驱动构件的第三部分的驱动端。

著录项

  • 公开/公告号BRPI0402700A

    专利类型

  • 公开/公告日2004-11-30

    原文格式PDF

  • 申请/专利权人 THE BOEING COMPANY;

    申请/专利号BR2004PI02700

  • 发明设计人 KELLY T. JONES;

    申请日2004-04-29

  • 分类号B64C39/12;

  • 国家 BR

  • 入库时间 2022-08-21 22:18:22

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