发明名称 |
AIRCRAFT HAVING A FORCE TRANSMISSION ELEMENT BETWEEN A CABIN STRUCTURAL ELEMENT AND A PRIMARY STRUCTURE |
摘要 |
The invention relates to an aircraft comprising a force transmission element which detachably connects a cabin structural segment to an aircraft primary structure and which comprises a cabin bearing element and a structure bearing element, the cabin bearing element being connected to the cabin structural segment and the structure bearing element being connected to the aircraft primary structure. The force transmission element is designed in such a manner that a force transmission can take place between the cabin structural segment and the aircraft primary structure with at least one degree of freedom of movement.
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申请公布号 |
US2011133027(A1) |
申请公布日期 |
2011.06.09 |
申请号 |
US20090936714 |
申请日期 |
2009.03.20 |
申请人 |
AIRBUS OPERATIONS GMBH |
发明人 |
GRAEBER ULRIKE;GROSSE-PLANKERMANN PETER;PAETZ MARTIN;BECKER HOLGER |
分类号 |
B64D11/00;B23P11/00;B64C1/06 |
主分类号 |
B64D11/00 |
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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