Patent ID: 8944374
Filing Date: 2015-02-03
Classification: B64C,B64D

Abstract:
1. A cabin system for an aircraft fuselage, comprising: a plurality of lining components for lining an interior side of the aircraft fuselage and comprising at least a ceiling lining and a lateral lining; and a plurality of cabin equipment components configured to be fixed in the aircraft; wherein the cabin equipment components hold outer edges of the lining components so that the lining components are held under tension between the cabin equipment components in the aircraft fuselage, thereby fixing a cabin defined by the plurality of lining components and the plurality of cabin equipment components to the aircraft fuselage; wherein at least the ceiling lining and the lateral lining are under tension in circumferential direction as a result of being fixed between the plurality of cabin equipment components; and wherein at least one cabin equipment component is configured as an overhead bin arranged above passenger seats, edges of the ceiling lining and the lateral lining being connected to the overhead bin.