The patent badge is an abbreviated version of the USPTO patent document. The patent badge does contain a link to the full patent document.

The patent badge is an abbreviated version of the USPTO patent document. The patent badge covers the following: Patent number, Date patent was issued, Date patent was filed, Title of the patent, Applicant, Inventor, Assignee, Attorney firm, Primary examiner, Assistant examiner, CPCs, and Abstract. The patent badge does contain a link to the full patent document (in Adobe Acrobat format, aka pdf). To download or print any patent click here.

Date of Patent:
Feb. 20, 2018

Filed:

Nov. 21, 2014
Applicants:

Airbus Operations Gmbh, Hamburg, DE;

Airbus Defence and Space Gmbh, Ottobrunn, DE;

Inventors:

Claus Hoffjann, Hamburg, DE;

Christian Wolff, Ottobrunn, DE;

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F02K 7/08 (2006.01); B64D 27/24 (2006.01); F01D 15/10 (2006.01); F02K 3/02 (2006.01); F02K 3/06 (2006.01); F02C 7/32 (2006.01); F02K 7/10 (2006.01); H01M 8/24 (2016.01); H01M 8/04014 (2016.01); H01M 8/04089 (2016.01); H01M 8/04082 (2016.01); B64D 41/00 (2006.01); H01M 8/1018 (2016.01);
U.S. Cl.
CPC ...
F02K 7/08 (2013.01); B64D 27/24 (2013.01); F01D 15/10 (2013.01); F02C 7/32 (2013.01); F02K 3/025 (2013.01); F02K 3/06 (2013.01); F02K 7/10 (2013.01); H01M 8/1018 (2013.01); H01M 8/24 (2013.01); B64D 2041/005 (2013.01); F05D 2220/10 (2013.01); F05D 2220/76 (2013.01); H01M 8/04014 (2013.01); H01M 8/04097 (2013.01); H01M 8/04201 (2013.01); H01M 2008/1095 (2013.01); H01M 2250/20 (2013.01); H01M 2300/0082 (2013.01); Y02E 60/50 (2013.01); Y02T 50/44 (2013.01); Y02T 50/64 (2013.01); Y02T 90/32 (2013.01); Y02T 90/36 (2013.01);
Abstract

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


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