Flugzeugstromsystem

EP4005920 Art B1 26. Februar 2025

Anmelder: Airbus Operations Limited 🇬🇧

Details

Veröffentlichungs-Nr.: EP4005920
Aktenzeichen: EP21205122
Anmeldetag: 27. Oktober 2021
Veröffentlichung: 26. Februar 2025
Erteilung: 26. Februar 2025
Rechtsraum: EP
IPC: B64C25/40

Abstract

Aircraft power system (200) comprising a hydraulic reservoir (210), a bidirectional hydraulic pump (212) for pumping hydraulic fluid to and from the reservoir (210), and an electric motor (230). The electric motor (230) is connectable to a first driveable component of the aircraft such that the electric motor (230) is arranged to drive the first driveable component of the aircraft. The hydraulic pump is connectable to the first driveable component of the aircraft such that the hydraulic pump is arranged to pump hydraulic fluid from the reservoir (210) to drive the first driveable component of an aircraft. Thus, in a first driveable mode of operation, the first driveable component is driven by both the electric motor (230) and the hydraulic pump (212).

Anmelder

Firma: Airbus Operations Limited
Land: 🇬🇧 Großbritannien

🇩🇪 Airbus Operations

Deutsche Tochtergesellschaft des europäischen Luft- und Raumfahrtkonzerns Airbus mit Standorten wie Hamburg. Entwickelt und fertigt Flugzeugstrukturen und Komponenten für die zivile Luftfahrt.

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Fachgebiete

Luft- & Raumfahrttechnik

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