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 (16) to an aircraft primary structure (5) and which comprises a cabin bearing element (110) and a structure bearing element (114), the cabin bearing element (110) being connected to the cabin structural segment (16) and the structure bearing element (114) being connected to the aircraft primary structure (5). The force transmission element (106) is designed in such a manner that a force transmission can take place between the cabin structural segment (16) and the aircraft primary structure (5) with at least one degree of freedom of movement.
申请公布号 WO2009124832(A3) 申请公布日期 2010.01.21
申请号 WO2009EP53301 申请日期 2009.03.20
申请人 AIRBUS OPERATIONS GMBH;GRAEBER, ULRIKE;GROSSE-PLANKERMANN, PETER;PAETZ, MARTIN;BECKER, HOLGER 发明人 GRAEBER, ULRIKE;GROSSE-PLANKERMANN, PETER;PAETZ, MARTIN;BECKER, HOLGER
分类号 B64C1/06 主分类号 B64C1/06
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