发明名称 Assembling device for a composite panel and structure
摘要 The assembly device comprises several fixings (16) regularly spaced along the interface (I) between the panel (12) and the structure (14). Each fixing comprises a traction screw perpendicular to the interface and a nut buried in the panel. To transmit the most important forces the nuts are arranged in two different rows (R1,R2,R3) parallel to the interface.
申请公布号 EP1234984(A3) 申请公布日期 2003.07.16
申请号 EP20020290405 申请日期 2002.02.20
申请人 AIRBUS FRANCE 发明人 BEQUET, FRANCK
分类号 B64C1/12;B64C3/28;F16B5/01;F16B5/02;(IPC1-7):F16B5/01 主分类号 B64C1/12
代理机构 代理人
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