A cargo door arrangement (1) for an aircraft and an aircraft comprising such a cargo door arrangement. The cargo door arrangement comprises a fuselage portion (2) , a cargo door (3) and a locking mechanism. The fuselage portion comprises a skin portion (5) , at least one fuselage former (6) and an opening. The cargo door (3) comprises at least one door former (8). The locking mechanism comprises a first engagement element (11), a second engagement element (12)and a connecting means (13). The first engagement element (11) has a tapered portion and is rigidly connected to the door former (8). The second engagement element (12) comprises a tapered cavity having a shape matching the shape of the tapered portion and is rigidly connected the fuselage former (6). In the closed position the tapered portion is engageable with the cavity.
Cargo door arrangement
Frachttüranordnung
Système de porte de fret
2015-05-06
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |