Motor zum Antrieb eines Flugzeugs und Flugzeug mit mindestens einem Triebwerk und mindestens einem Wasserstofftank

Details

Veröffentlichungs-Nr.

EP2878795

Aktenzeichen

EP13194653

Anmeldetag

27. November 2013

Veröffentlichung

12. Oktober 2016

Erteilung

12. Oktober 2016

Rechtsraum

EP

IPC

F02K3/06F01D15/10B64D27/24H01M8/1018F02K3/02F02C7/32H01M8/24// F01D13/00H01M8/04H01M8/10B64D41/00H01M8/04089H01M8/04014H01M8/04082

Abstract

An engine (2) for propelling an aircraft comprises an annular fuel cell arrangement (8) having at least one fuel cell, at least one electric motor (6) couplable to the fuel cell arrangement (8), at least one fan (4) couplable to the electric motor (6) and a cowling (10) having an inlet (12) and an outlet nozzle (14). The fuel cell arrangement (8) is arranged inside the cowling, the at least one fan (4) is arranged between the inlet (12) and the fuel cell arrangement (8) inside the cowling (10), the electric motor (6) is operable under consumption of electric power delivered by the fuel cell arrangement (8) and the at least one fan (4) is designed to produce a thrust force by creating an accelerated airflow at the outlet nozzle (14). The engine (2) is extremely efficient and comprises a distinct low noise.

Anmelder

Firmen

Airbus Operations GmbH
Airbus Defence and Space GmbH
EADS Deutschland GmbH

Land

🇩🇪 Deutschland

Fachgebiete