Einfahren des Fahrwerks

Details

Veröffentlichungs-Nr.

EP3702270

Aktenzeichen

EP20159482

Anmeldetag

26. Februar 2020

Veröffentlichung

9. Juli 2025

Erteilung

9. Juli 2025

Rechtsraum

EP

IPC

B64C25/10B64C25/28B64C25/26B64C25/60

Abstract

Disclosed is a landing gear system (100) for an aircraft, the landing gear system comprising: a landing gear (130) that is movable between an extended position and a retracted position, the landing gear comprising an extendible strut (136); a position sensor (140) configured to detect a position of a part of the extendible strut and output a signal indicative of the position; and a landing gear controller (150) that is communicably connected to the position sensor and is configured, in use, to: receive the signal from the position sensor; and, on the basis of the signal, determine that the strut has extended and the landing gear is in contact with the ground and automatically cause performance of at least a portion of a procedure to move the landing gear from the extended position to the retracted position

Anmelder

Firma

Airbus Operations Limited

Land

🇬🇧 Großbritannien

Fachgebiete