Aircraft empennage, comprising:- a rear fuselage section (1),- a trimmable horizontal tail plane (2) comprising a first and a second lateral torsion box (21, 22), each comprising a front spar (211, 221) and a rear spar (212, 222),- a front fitting (4) and a rear fitting (5),- an actuator (3) acting on the front fitting (4) for a rotation of the trimmable horizontal tail plane (2) around a hinge axis (11) passing through the rear fitting (5),- the front fitting (4) comprising a first and a second front fitting units (41, 42) being joined to the front spars (211, 221) of the lateral torsion boxes (21, 22), and- the actuator (3) comprising a first and a second actuator units (31, 32), each acting on the first front fitting unit (41) and the second front fitting unit (42) respectively.
AIRCRAFT EMPENNAGE
FLUGZEUGLEITWERK
EMPENNAGE D'AÉRONEF
07.05.2025
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |
Mounting assembly for aircraft empennage and aircraft empennage
Europäisches Patentamt | 2024
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