The present invention relates to an aircraft fuselage section (1) in whose outer skin construction (4) at least one door opening (5) is provided, which has a width (6), such that it is divided by at least one rib (3) of the fuselage skeleton of the aircraft fuselage section (7) into multiple opening areas (7).
申请公布号
WO2007115690(A8)
申请公布日期
2007.12.27
申请号
WO2007EP02770
申请日期
2007.03.28
申请人
AIRBUS DEUTSCHLAND GMBH;DEHN, MARTIN;WUGGETZER, INGO;IPEK, UGUR;MUEHLICH, CHRISTOPH
发明人
DEHN, MARTIN;WUGGETZER, INGO;IPEK, UGUR;MUEHLICH, CHRISTOPH
