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