发明名称 |
Method for coupling stiffening profile elements and structural component |
摘要 |
This invention provides a coupling method for coupling a first and a second stiffening profile element for an outer skin of an aircraft or space craft. In a first step the stiffening profile elements are arranged on the outer skin in such a manner that the stiffening profile elements oppose each other with their respective front sides and enclose within themselves a cavity. Furthermore, a fixing hole is formed through a wall of at least one of the stiffening profile elements in the cavity inside a coupling zone of the stiffening profile element. An access opening is formed through the wall in the cavity along the coupling zone. A coupling strap, which couples the stiffening profile elements together, is fastened to the coupling zone by means of a fastening element guided through the fixing hole. |
申请公布号 |
US8715808(B2) |
申请公布日期 |
2014.05.06 |
申请号 |
US20080666605 |
申请日期 |
2008.06.19 |
申请人 |
ROMING THORSTEN;SCHROEER THORSTEN;KIRSTEIN HAUKE;GENSCH HINNIK;TACKE STEFAN;AIRBUS OPERATIONS GMBH |
发明人 |
ROMING THORSTEN;SCHROEER THORSTEN;KIRSTEIN HAUKE;GENSCH HINNIK;TACKE STEFAN |
分类号 |
B32B3/06;B32B3/10;B32B3/24;B32B3/28;B32B5/12;B32B7/08;B64C1/06;B64F5/00 |
主分类号 |
B32B3/06 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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