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