Fuselage structural component of an aircraft or spacecraft,...

Details Fuselage structural component of an aircraft or spacecraft,... Fuselage structural component of an aircraft or spacecraft,...

B - Operations, Transporting

64

C

B64C 1/00 (2006.01)

Patent

CA 2671908

The present invention creates a fuselage structural component (1) of an aircraft or spacecraft, with a non- load-bearing outer skin (2) and a load-bearing inner framework structure (3), wherein a foam layer (4) which effects heat insulation and/or impact protection is arranged between the outer skin (2) and the inner framework structure (3).

La présente invention porte sur un composant structural (1) de fuselage d'aéronef ou de véhicule spatial, comprenant une peau externe (2) non porteuse, et une structure d'ossature (3) interne porteuse. Une couche de mousse (4) servant à l'isolation thermique et/ou à la protection contre les chocs est disposée entre la peau externe (2) et la structure d'ossature le terme (3).

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