RUMPFSTRUKTUR, BEINHALTEND EIN BAUTEIL MIT RIPPEN-UND QUERTRÄGERELEMENT
摘要
The present invention provides a fuselage structure for an aircraft or spacecraft with an outer skin. The fuselage structure comprises a rib element for stiffening the outer skin and ad cross member element. Here the rib element is bent in the shape of an arc to correspond to an inner contour of the outer skin. The cross member element connects two arc sections of the rib element transversely to each other. The cross member element has a higher strength than the rib element. From another point of view the invention provides an aircraft with such a fuselage structure.
申请公布号
AT506254(T)
申请公布日期
2011.05.15
申请号
AT20080774243T
申请日期
2008.06.24
申请人
AIRBUS OPERATIONS GMBH;DEUTSCHES ZENTRUM FUER LUFT- UND RAUMFAHRT E.V.
发明人
WESTPHAL, PHILIPP;DOLZINSKI, WOLF-DIETRICH;ROMING, THORSTEN;SCHROEER, THORSTEN;KOHLGRUEBER, DIETER;LUETZENBURGER, MARIUS