发明名称 Sandwich structure with shear stiffness between skins and compliance in the thickness direction
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.
申请公布号 EP2636592(B1) 申请公布日期 2016.07.13
申请号 EP20130156842 申请日期 2013.02.26
申请人 THE BOEING COMPANY 发明人 GRIP, ROBERT E;BROWN, JOHN J
分类号 B64C1/12;B64D27/26;B64D29/00;F01D25/26;F02C7/20 主分类号 B64C1/12
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