首页> 外国专利> DOUBLE OVER CENTER CRANKSHAFT FLAP MECHANISM

DOUBLE OVER CENTER CRANKSHAFT FLAP MECHANISM

机译:双重中心曲轴挡板机构

摘要

A flap actuation mechanism incorporates a flap bracket attached to a flap and coupled to an underwing structure with a pivotal coupling. A crankshaft is configured for over center rotation has aligned inboard and outboard crank arms extending from axially spaced inboard and outboard journals disposed in the underwing structure and configured to rotate about a rotation axis of the inboard and outboard journals. A crank pin connected between the inboard and outboard crank arms. An actuating rod has a first end rotatably coupled to the crank pin and a second end coupled to the flap bracket. Rotation of the crankshaft displaces the actuating rod to cause rotation of the flap bracket and the flap.
机译:翼片致动机构包括附接到翼片的翼片支架,并通过枢转耦合连接到腔室的腔结构。曲轴构造成用于上中心旋转已经从轴向间隔开的内侧和舷外轴颈延伸的内侧旋转,并且构造成围绕舷内和舷外轴颈的旋转轴线旋转。连接在内侧和舷外曲柄臂之间的曲柄销。致动杆具有可旋转地连接到曲柄销的第一端和连接到翼片支架的第二端。曲轴的旋转使致动杆置于旋转支架和翼片的旋转。

著录项

  • 公开/公告号US2021061442A1

    专利类型

  • 公开/公告日2021-03-04

    原文格式PDF

  • 申请/专利权人 THE BOEING COMPANY;

    申请/专利号US201916560773

  • 发明设计人 KEVIN R. TSAI;BRYAN J. GRUNER;

    申请日2019-09-04

  • 分类号B64C9/02;B64C9/18;B64C13/30;

  • 国家 US

  • 入库时间 2022-08-24 17:30:29

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