The invention provides an aircraft rear structure (10) comprising a substantially flat rear pressure bulkhead (11), with a first side and a second side, opposite to the first side. It also comprises a horizontal stabilizer (21) and a vertical stabilizer (1) which in turn comprises a first spar (2) and a second spar (3). The first spar (2) is attached to a first attachment zone (41) of the second side of the rear pressure bulkhead (11) by means of first attaching means (5, 6), and the second spar (3) is attached to a second attachment zone (42) of the second side of the rear pressure bulkhead (11) by means of second attaching means (7, 8). The second attachment zone (42) being different from the first attachment zone (41).
AIRCRAFT REAR STRUCTURE
FLUGZEUGHECKAUFBAU
STRUCTURE ARRIÈRE D'AVION
2018-02-21
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |