Aircraft empennage comprising: - A vertical tail plane (2). - A rear fuselage section (1) being attached to the vertical tail plane (2) and comprising a skin (1.1) and internal reinforcing members. - A horizontal tail plane (3) comprising two lateral torsion boxes (31, 32) and a framework (33) located between the two lateral torsion boxes (31, 32) comprising a front spar (34), a rear spar (35) and two ribs (36, 37) extending between the front (34) and the rear spar (35) and each adjacent to a lateral torsion box (31, 32). The framework (33) enclosing a portion of the vertical tail plane (2) along its spanwise direction. The aircraft empennage comprising an attachment assembly attaching the framework (33) to the rear fuselage section (1), the attachment assembly crossing the skin (1.1) and extending between the internal reinforcing members of the rear fuselage section (1) and the framework (33).
AIRCRAFT EMPENNAGE WITH A HORIZONTAL STABILIZER INTERFACING AT THE VERTICAL STABILIZER ROOT
EMPENNAGE D'AERONEF COMPRENANT UN STABILISATEUR HORIZONTAL SERVANT D'INTERFACE A LA RACINE DE STABILISATEUR VERTICAL
2022-08-10
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |
AIRCRAFT EMPENNAGE WITH A HORIZONTAL STABILIZER INTERFACING AT THE VERTICAL STABILIZER ROOT
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