A rear fuselage section of an aircraft comprises at least one closed frame constructed as a unitary body, and a horizontal tail plane comprising a box-type central element and two lateral torsion boxes, said horizontal tail plane trimmable with respect to a pivot axis. The horizontal tail plane is mounted at the closed frame and the pivot axis is contained in a horizontal plane below the lowest end of said closed frame.
Rear fuselage section of an aircraft
2016-11-01
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |
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