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. In a further aspect a structural component is provided with an aircraft or space craft, with an outer skin, a first and a second stiffening profile element which are arranged on the outer skin so that the stiffening profile elements oppose each other with their respective front sides and enclose within themselves a cavity, with a fixing hole through a wall of at least one of the stiffening profile elements in the cavity, which hole is formed within a coupling zone of the stiffening profile element, with an access opening in the cavity through the wall, which is formed along the coupling zone, and with a coupling strap which couples the stiffening profile elements together and is fastened to the coupling zone by means of a fastening element guided through the fixing hole. |
申请公布号 |
WO2009000734(A2) |
申请公布日期 |
2008.12.31 |
申请号 |
WO2008EP57758 |
申请日期 |
2008.06.19 |
申请人 |
AIRBUS DEUTSCHLAND GMBH;ROMING, THORSTEN;SCHROEER, THORSTEN;KIRSTEIN, HAUKE;GENSCH, HINNIK;TACKE, STEFAN |
发明人 |
ROMING, THORSTEN;SCHROEER, THORSTEN;KIRSTEIN, HAUKE;GENSCH, HINNIK;TACKE, STEFAN |
分类号 |
B64C1/06;B64F5/00 |
主分类号 |
B64C1/06 |
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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