B - Operations – Transporting – 64 – C
Patent
B - Operations, Transporting
64
C
B64C 1/14 (2006.01) B64C 1/00 (2006.01) B64C 1/10 (2006.01) B64D 9/00 (2006.01)
Patent
CA 2383895
An aircraft fuselage (10) comprising a cargo storage compartment (18), a rear bulkhead (16) at the rear of the compartment for withstanding internal air pressure in the fuselage, a closeable opening (20) in the rear bulkhead (18) through which an elongate item of cargo (25) can be passed, and an opening (26) in the rear of the fuselage (10) through which the said item (25) passes to be despatched from the aircraft with the fuselage (10) de-pressurised.
L'invention concerne un fuselage d'aéronef (10) comprenant un compartiment de stockage du fret (18), une cloison (16) située à l'arrière du compartiment et prévue pour résister à la pression d'air intérieur dans le fuselage, une ouverture (20) qui peut être fermée située dans la cloison arrière (18) à travers laquelle des objets allongés de fret (25) peuvent être passés, et une ouverture (26) à l'arrière du fuselage (10), par laquelle lesdits objets (25) passent afin être déchargés de l'aéronef une fois le fuselage (10) dépressurisé.
Bae Systems Plc
Fetherstonhaugh & Co.
LandOfFree
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