Hochauftriebssystemarchitektur, Zugehöriges Hochauftriebssystem, Flugzeug und Verfahren zur Überwachung eines Hochauftriebssystems

Details

Veröffentlichungs-Nr.

EP4799922

Anmeldetag

12. Februar 2026

Veröffentlichung

2. September 2026

Rechtsraum

EP

IPC

B64C9/02, B64D45/00

Abstract

This high lift system architecture (22), comprises: - a first rotational sensor (46), configured to be installed on a torque transmission arrangement (24) and to measure a first angular position (A1) of the torque transmission arrangement (24), at a first measurement point (M1); - a second rotational sensor (48), configured to be installed on the torque transmission arrangement (24) and to measure a second angular position (A2) of the torque transmission arrangement (24), at a second measurement point (M2); and - an actuation control device (50), comprising: + an acquisition module (56), configured for acquiring the first angular position (A1) from the first rotational sensor (46) and the second angular position (A2) from the second rotational sensor (48), and + a determination module (58), configured for determining a torque (T) applied to the torque transmission arrangement (24) as a function of said acquired first (A1) and second (A2) angular positions.

Anmelder

Firma

Airbus Operations GmbH

Land

🇩🇪 Deutschland

Fachgebiete