Energieverteilungssystem für ein Flugzeug auf dem Boden

Details

Veröffentlichungs-Nr.

EP3876380

Aktenzeichen

EP20211052

Anmeldetag

1. Dezember 2020

Veröffentlichung

14. August 2024

Erteilung

14. August 2024

Rechtsraum

EP

IPC

H02J4/00

Abstract

A power distribution system is provided for an aircraft on the ground, comprising a first electrical load, operably coupled to the aircraft on the ground and configured to receive at least a first portion of a predetermined maximum input power provided by a power supply; at least one second electrical load, electrically coupleable to the aircraft on the ground and configured to receive at least a second portion of said predetermined maximum input power provided by said power supply, and a controller, adapted to monitor at least one parameter of the power consumed by any one of said first electrical load and said at least one second electrical load, and control the power consumption of at least said first electrical load so that the total power consumption of said first electrical load and said at least one second electrical load does not exceed said predetermined maximum input power; wherein said predetermined maximum input power is provided via a single power line between said power supply and an input port of said first electrical load.

Anmelder

Firma

Illinois Tool Works INC.

Land

🇺🇸 USA

Fachgebiete