首页> 外国专利> METHOD OF MINIMISING LOADS IN A SANDWICH STRUCTURE WITH SHEAR STIFFNESS BETWEEN SKINS AND COMPLIANCE IN THE THICKNESS DIRECTION

METHOD OF MINIMISING LOADS IN A SANDWICH STRUCTURE WITH SHEAR STIFFNESS BETWEEN SKINS AND COMPLIANCE IN THE THICKNESS DIRECTION

机译:最小化厚度方向顺应性的夹层结构中荷载最小化的方法

摘要

A method of minimising loads in a sandwich structure (10), which includes a first skin (18), a second skin (20), a first hinge member (32) and a second hinge member (42). The first hinge member is movably coupled to the first skin and a first skin joint (40). The second hinge member is movably coupled to the second skin and second skin joint (50). The first hinge member and the second member are movably coupled to one another and a member joint (52) located between the first and second skin joint.
机译:一种最小化夹层结构(10)中的载荷的方法,该结构包括第一表皮(18),第二表皮(20),第一铰链构件(32)和第二铰链构件(42)。第一铰链构件可移动地联接至第一蒙皮和第一蒙皮接头(40)。第二铰链构件可移动地联接至第二蒙皮和第二蒙皮接头(50)。第一铰链构件和第二构件彼此可移动地联接,并且构件铰链(52)位于第一和第二蒙皮接头之间。

著录项

  • 公开/公告号EP3053824A1

    专利类型

  • 公开/公告日2016-08-10

    原文格式PDF

  • 申请/专利权人 THE BOEING COMPANY;

    申请/专利号EP20160159740

  • 发明设计人 GRIP ROBERT E;BROWN JOHN J;

    申请日2013-02-26

  • 分类号B64C1/12;B64D27/26;B64D29;F01D25/26;F02C7/20;

  • 国家 EP

  • 入库时间 2022-08-21 14:48:43

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