Tail structure for an aircraft or spacecraft

Details Tail structure for an aircraft or spacecraft Tail structure for an aircraft or spacecraft

B - Operations, Transporting

64

C

B64C 1/10 (2006.01) B64C 1/26 (2006.01)

Patent

CA 2650512

The present invention provides a tail structure (1) for an aircraft or spacecraft, which adjoins a fuselage section (2) of the aircraft or spacecraft, and comprises a support construction (3) for supporting at least one craft component {40, 41) , and a bulkhead unit (5) intended for the pressure-tight sealing of the fuselage section (2) and able to be coupled both to the support construction (3) and to the fuselage section (2) so as to form a force flow path between the at least one craft component (40, 41) and the fuselage section (2) .

L'invention concerne une structure de queue (1) pour un aéronef ou un astronef, attenante à un tronçon de fuselage (2) de l'aéronef ou de l'astronef, et comprenant une structure support (3) servant à supporter au moins un composant (40, 41) de l'aéronef ou de l'astronef, et un module de cloison (5) destiné à assurer l'étanchéité à la pression du tronçon de fuselage (2) et susceptible d'être simultanément couplé à la structure support (3) et au tronçon de fuselage (2) pour former un chemin de transfert de force entre ledit au moins un composant (40, 41) de l'aéronef ou de l'astronef et le tronçon de fuselage (2).

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