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Separate, high-lift, rotationally driven spoiler

机译:独立的,高扬程的旋转扰流板

摘要

A rotationally driven high lift separate spoiler deployment link mechanism (304), comprising: a rotatable actuator (312) operable to couple a high lift separate spoiler (306) to a dynamic body (302) of fluids in a hinge line (418) of a rotationally driven high lift separate spoiler and the rotatable and operable actuator to move said rotationally driven high lift separate spoiler; a vault flange door link (506) arranged to be coupled to said separate rotary actuated high lift spoiler and a vault flange door (310), and operable to rotate a vault flange door in response to a rotary actuator of the rotary actuator; and a drop panel link (512) arranged to engage said rotationally driven high lift separate spoiler and a drop panel (308) operable to move a drop panel in response to rotary actuation.
机译:旋转驱动的高升程分离器扰流器部署连杆机构(304),包括:可旋转致动器(312),该可旋转致动器(312)可操作地将高升程分离器扰流器(306)耦合到铰链线(418)中的流体的动态体(302)。旋转驱动的高升程独立扰流板和可旋转且可操作的致动器,以移动所述旋转驱动的高升程独立扰流板;拱顶法兰门连杆(506),其布置成联接至所述单独的旋转致动的高举升扰流板和拱顶法兰门(310),并且可操作以响应于旋转致动器的旋转致动器而旋转拱顶法兰门;放置面板连杆(512),其布置成与所述旋转驱动的高升程独立扰流板接合,以及放置面板(308),可操作以响应于旋转致动而移动放置面板。

著录项

  • 公开/公告号ES2636777T3

    专利类型

  • 公开/公告日2017-10-09

    原文格式PDF

  • 申请/专利权人 THE BOEING COMPANY;

    申请/专利号ES20130167503T

  • 发明设计人 KORDEL JAN A.;SAKURAI SEIYA;

    申请日2013-05-10

  • 分类号B64C9/14;B64C9/18;

  • 国家 ES

  • 入库时间 2022-08-21 13:35:06

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