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:
Aug. 06, 2024

Filed:

Nov. 08, 2022
Applicants:

Airbus Operations Sas, Toulouse, FR;

Airbus Sas, Blagnac, FR;

Airbus Operations Gmbh, Hamburg, DE;

Inventors:

Thomas Josset, Toulouse, FR;

Didier Poirier, Blagnac, FR;

Holger Bammann, Hamburg, DE;

Thomas Scherer, Hamburg, DE;

Assignees:

Airbus Operations SAS, Toulouse, FR;

Airbus SAS, Blagnac, FR;

Airbus Operations GmbH, Hamburg, DE;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64D 41/00 (2006.01); B60L 58/33 (2019.01); B64D 13/06 (2006.01); H01M 8/04007 (2016.01); H01M 8/04029 (2016.01); H01M 8/04111 (2016.01); H01M 8/04664 (2016.01); H01M 8/04746 (2016.01);
U.S. Cl.
CPC ...
B64D 41/00 (2013.01); B60L 58/33 (2019.02); B64D 13/06 (2013.01); H01M 8/04029 (2013.01); H01M 8/04074 (2013.01); H01M 8/04111 (2013.01); H01M 8/04664 (2013.01); H01M 8/04753 (2013.01); H01M 8/04776 (2013.01); B60L 2200/10 (2013.01); B64D 2013/0611 (2013.01); B64D 2041/005 (2013.01); H01M 2250/20 (2013.01);
Abstract

An auxiliary power unit for an aircraft. It includes an air compressor coupled to an air-drawing device for drawing in air from outside the aircraft, the compressor supplying compressed air to a manifold. The manifold is configured to supply air to an environmental control system and a start-up module of at least one propulsion system of the aircraft running on hydrogen. The manifold is also configured to supply air to a fuel cell stack arranged to provide an electric generation function configured to power non-propulsive systems of the aircraft, the fuel cell stack also being supplied with hydrogen from a tank supplying hydrogen to the at least one propulsion system of the aircraft.


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