Trimmable horizontal stabilizer

Details Trimmable horizontal stabilizer Trimmable horizontal stabilizer

B - Operations, Transporting

64

C

B64C 3/44 (2006.01) B64C 5/10 (2006.01)

Patent

CA 2656794

A trimmable horizontal stabilizer, which is provided adjacent to the fuselage (10) of an aircraft and has a predetermined aerodynamic profile, and adjacent to which a movable elevator (21) is arranged. The horizontal stabilizer (20) has a load-bearing structure (22) which extends in the span direction and is firmly connected to the fuselage of the aircraft, and movable areas (23, 24) which are connected to the load-bearing structure (22) such that they can move and can be moved independently of the elevator (21) in order to trim the horizontal stabilizer (20) by varying the aerodynamic profile.

Le plan horizontal réglable de la présente invention est disposé de manière adjacente par rapport au fuselage (10) d'un avion et présente un profil aérodynamique prédéterminé et une gouverne de profondeur mobile (21) est agencée de manière adjacente par rapport à ce plan horizontal réglable. Le plan horizontal (20) est doté d'une ossature (22) qui s'étend dans le sens de la longueur et est fermement relié au fuselage de l'avion, et de zones mobiles (23, 24) qui sont reliées à l'ossature (22) de manière à ce qu'elles puissent se déplacer et être déplacées indépendamment de la gouverne de profondeur (21) afin de compenser le plan horizontal (20) en variant le profil aérodynamique.

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