Load introduction structure i.e. lining framework, for aircraft i.e. air freighter, has two side frames that are arranged opposite to both side regions of fuselage cell structure, where cell structure decouples introduction structure

摘要

The structure (4) has two side frames (7, 8) that are arranged opposite to both side regions (9, 10) of a fuselage cell structure (1) of an aircraft and connected to a continuous floor surface (6). The fuselage cell structure is provided for decoupling the structure (1). The fuselage cell structure has a set of annular frames (2) that are covered at an outer side with a fuselage cell film (3). The side frames are fastened to the respective annular frames. The side frames are connected by a ceiling framework (13) which is fastened into a ceiling area (14) of the fuselage cell structure.