Structural component and fuselage of an aircraft or spacecraft

Details Structural component and fuselage of an aircraft or spacecraft Structural component and fuselage of an aircraft or spacecraft

B - Operations, Transporting

64

C

B64C 1/06 (2006.01)

Patent

CA 2699643

A supporting component (10) is provided for reinforcing the skin of an aircraft or spacecraft, for example a stringer or former, this component being configured as a closed profile (hollow profile) (3), such that a system medium (M) can be conducted through the structural component. In this respect, the hollow profile (3) itself serves as a load-bearing component.

La présente invention concerne un composant porteur (10) servant à rigidifier la peau d'un engin aérospatial, comme par exemple une lisse ou un couple. Ce composant est réalisé en profilé fermé (profilé creux) (3) de façon à pouvoir y faire circuler un fluide système (M). Cela fait que le profilé creux (3) sert lui-même de composant porteur de charges.

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