Steuerungssystem für ein Flugzeug

Details

Veröffentlichungs-Nr.

EP4082898

Aktenzeichen

EP21171623

Anmeldetag

30. April 2021

Veröffentlichung

17. Juli 2024

Erteilung

17. Juli 2024

Rechtsraum

EP

IPC

B64C13/40

Abstract

A control system for an aircraft is proposed, comprising a hydraulic pump, a first hydraulic line, a second hydraulic line, at least one first actuator coupled with a first control surface, at least one second actuator coupled with a second control surface, and at least one third actuator coupled with a third control surface, wherein the first control surface and the second control surface are arranged at a distance to each other and symmetrically relative to a symmetry axis, wherein the third control surface is arranged substantially on the symmetry axis, wherein the first hydraulic line and the second hydraulic line are connected to the hydraulic pump, wherein the at least one first actuator is connected to the first hydraulic line, wherein the at least one second actuator is connected to the second hydraulic line, wherein the at least one third actuator is connected to the first hydraulic line downstream of the at least one first actuator at a junction point, and wherein the first hydraulic line at least partially comprises a larger diameter than the second hydraulic line.

Anmelder

Firmen

Airbus Operations GmbH
Airbus Operations S.A.S.

Land

🇩🇪 Deutschland

Fachgebiete