Flugzeug mit einem Hybridem-Elektrischem Antriebssystem mit im Rumpf Beherbergtem Stromspeicher

Details

Veröffentlichungs-Nr.

EP3750793

Aktenzeichen

EP20179823

Anmeldetag

12. Juni 2020

Veröffentlichung

5. April 2023

Erteilung

5. April 2023

Rechtsraum

EP

IPC

B64C1/18B64C3/38B64D27/24B64D27/02

Abstract

An aircraft comprising a fuselage (20) and an electrical system (101) having an electric storage (103) and an electric-motor controller (121) electrically connected to the electric storage (103), wherein the electric-motor controller (121) is positioned in a wing above the fuselage, wherein the electric storage (103) is positioned on a bottom side of a cabin opposite from the electric-motor controller (121), wherein the electrical system includes at least one conductor extending from the electric storage (103), up a first side of a cabin wall to the electric-motor controller (121), the aircraft further comprising a hybrid electric propulsion system, wherein the electrical system is part of the hybrid electric propulsion system, wherein the hybrid electric propulsion system includes a heat engine (104).

Anmelder

Firma

Hamilton Sundstrand Corporation

Land

🇺🇸 USA

Fachgebiete