Hybridelektrische und Rein Elektrische Flugzeugantriebssysteme

Details

Veröffentlichungs-Nr.

EP4714828

Anmeldetag

17. Mai 2022

Veröffentlichung

25. März 2026

Rechtsraum

EP

IPC

B64D27/24

Abstract

A system for an aircraft (1) comprises an electric energy module (108) and a connector module (114c) operatively connected to the electric energy module (108). The connector module (114c) is structured to attach the electric energy module (108) to the aircraft (1) when the connector module (114c) is in an engaged mode while in use, and operable between the engaged mode and a disengaged mode, the connector module (114c) being in the disengaged mode while in use disengaging the electric energy module (108) from the aircraft (1).

Anmelder

Firma

Pratt & Whitney Canada Corp.

Land

🇨🇦 Kanada

Fachgebiete