Stromsystemarchitektur

Details

Veröffentlichungs-Nr.

EP4797476

Anmeldetag

13. Februar 2026

Veröffentlichung

26. August 2026

Rechtsraum

EP

IPC

H02J1/10, B64D27/34, B64D27/35

Abstract

An electrical power system architecture (200) is described herein. In some approaches, an electrical system for an aircraft (100) includes an electrical source (202), an electrical load (204), and a power distribution system (206). The power distribution system (206) includes a plurality of power channels (208) connecting the electrical source (202) to the electrical load (204). The electrical power is distributed in each power channel (208) under normal operating conditions and, in the event of a power channel failure, the electrical power is distributed by a subset of the plurality of power channels (208) such that the aircraft (100) can maintain aircraft flight conditions during the power channel failure.

Anmelder

Firma

GE Aviation Systems Limited

Land

🇬🇧 Großbritannien

Fachgebiete