Flugzeug mit trimmbarer Höhenflosse mit den Schwenkelementen auf der Vorderseite

Details

Veröffentlichungs-Nr.

EP2889216

Aktenzeichen

EP13382578

Anmeldetag

31. Dezember 2013

Veröffentlichung

19. September 2018

Erteilung

19. September 2018

Rechtsraum

EP

IPC

B64C5/02B64C1/26B64C13/28

Abstract

The invention provides an aircraft with a trimmable horizontal stabilizer (13) that not requires a cut-out in resistant areas of the rear fuselage and that occupies less space that in conventional horizontal stabilizers. The rear fuselage (5) comprises at least a first section (9) having a resistant fuselage and a second section (11), aft of the first section, having a non-resistant fuselage (i.e. a fairing). The load-bearing structure (30) of the horizontal stabilizer and the trimming actuator (50) are disposed inside said second section (11). The pivot element (41) is mounted on its forward side and coupled to the first section (9) of the rear fuselage. The connection fitting (21) is mounted on its rearward side and the trimming actuator (50) is disposed so that it exerts a force in the direction of the Z-axis of the aircraft on the connection fitting (21) during a trimming operation.

Anmelder

Firma

Airbus Operations S.L.

Land

🇪🇸 Spanien

Fachgebiete