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AIRCRAFT ENGINE EXHAUST NOZZLE COMPRISING SANDWICH STRUCTURE WITH SHEAR STIFFNESS BETWEEN SKINS AND COMPLIANCE IN THE THICKNESS DIRECTION

机译:包含夹心结构且厚度方向顺应性为夹心结构的飞机发动机排气喷嘴

摘要

A sandwich structure (10) 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 (18) at a first skin joint (40). The second hinge member (42) is movably coupled to the second skin (20) at a second skin joint (50). The first hinge member and the second member are movably coupled to one another at a member joint (52) located between the first and second skin joint. The joints (40, 50, 52) may be rigid or flexible.
机译:夹层结构(10)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表皮(18)。第二铰链部件(42)在第二蒙皮接头(50)处可移动地联接至第二蒙皮(20),第一铰链部件和第二部件以可移动方式彼此联接。在位于第一和第二皮肤接头之间的构件接头(52)处,接头(40、50、52)可以是刚性的或柔性的。

著录项

  • 公开/公告号EP3392133B1

    专利类型

  • 公开/公告日2020-01-29

    原文格式PDF

  • 申请/专利权人 THE BOEING COMPANY;

    申请/专利号EP20180173884

  • 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 11:40:35

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