An aircraft structure 101 comprising a skin panel 111, having an outer surface forming an external face of the structure, and an inner surface internal to the structure, the aircraft structure 101 also comprising a plurality of stringers 150 extending along a length of the inner surface of the skin panel, and an inner panel 112 spaced apart from the inner surface of the skin panel 111, so as to form an internal cavity adjacent to the skin panel, and wherein the stringers 150 are located within the cavity.
Aircraft structure comprising a skin panel
2017-07-11
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |