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Swivel Device for Actuator of Full-Scale Aircraft Static Tests

机译:全尺寸飞机静态测试执行器的旋转装置

摘要

PURPOSE: A swivel device for a hydraulic actuator is provided to apply an angular load to an angular hydraulic actuator by using a two-way rotating link including first and second pins, which are axially rotated. CONSTITUTION: A lower rotating member(3) is coupled to an upper portion of a hydraulic actuator(8). The center portion of the lower rotating member(3) is protruded such that a middle rotating member(1) is connected to the lower rotating member(3) through a lower rotating pin(4'). An upper rotating pin(4) is installed at an upper portion of the lower rotating pin(4') in such a manner that the upper rotating pin(4) is connected to an upper rotating member(2). The upper rotating pin(4) and the lower rotating pin(4') are positioned between the upper and lower rotating members(2,3). Two stud bolts(6) are installed at both sides of the upper rotating member(2).
机译:目的:提供一种用于液压致动器的旋转装置,以通过使用双向旋转连杆来向角液压致动器施加角负载,该双向旋转连杆包括轴向旋转的第一和第二销。组成:下旋转部件(3)连接到液压执行器(8)的上部。下旋转构件(3)的中心部分突出,使得中间旋转构件(1)通过下旋转销(4')连接到下旋转构件(3)。上部旋转销(4)以使得上部旋转销(4)连接到上部旋转构件(2)的方式安装在下部旋转销(4')的上部。上部旋转销(4)和下部旋转销(4')位于上部和下部旋转构件(2,3)之间。在上部旋转部件(2)的两侧安装了两个双头螺栓(6)。

著录项

  • 公开/公告号KR20030050319A

    专利类型

  • 公开/公告日2003-06-25

    原文格式PDF

  • 申请/专利权人 KOREA AEROPACE RESEARCH INSTITUTE;

    申请/专利号KR20010080732

  • 发明设计人 KIM SEONG CHAN;KIM TAE UK;

    申请日2001-12-18

  • 分类号G01M1/16;

  • 国家 KR

  • 入库时间 2022-08-21 23:46:50

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