Fuselage of an aircraft or spacecraft and corresponding...

B - Operations – Transporting – 64 – C

Patent

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Details

B64C 1/06 (2006.01)

Patent

CA 2676440

The invention relates to a fuselage (1) of an air- or spacecraft. The fuselage (1) comprises at least one shell element (2) and one insulation element (5). The insulation element (5) is configured as a passive, watertight insulation element and can be mounted on an inner side (9) of the at least one shell element (2) in a completely air- and watertight manner. The invention furthermore relates to a respective aircraft or spacecraft.

La présente invention concerne un fuselage (1) d'aéronef ou d'engin spatial. Ce fuselage (1) comprend au moins un élément coque (2) et un élément d'isolation (5). L'élément d'isolation (5) est configuré en élément d'isolation passive, étanche à l'eau, avec la possibilité de se monter sur la face intérieure (9) de l'élément coque considéré (2) de façon complètement étanche à l'air et à l'eau. L'invention concerne également un aéronef ou un engin spatial correspondant.

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