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:
Dec. 12, 2023

Filed:

Aug. 01, 2022
Applicants:

Airbus Sas, Blagnac, FR;

Airbus Operations Sas, Toulouse, FR;

Inventors:

Lionel Czapla, Toulouse, FR;

Antoine Abele, Toulouse, FR;

Benjamin Thubert, Toulouse, FR;

Alexis Pissavin, Blagnac, FR;

Abhishek Verma, Toulouse, FR;

Alistair Forbes, Toulouse, FR;

Jorge A. Carretero Benignos, Taufkirchen, DE;

Benedikt Bammer, Danauworth, DE;

Assignees:

Airbus SAS, Blagnac, FR;

Airbus Operations SAS, Toulouse, FR;

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F02C 7/224 (2006.01); B64D 37/04 (2006.01); B64D 37/30 (2006.01); F02C 3/22 (2006.01); B64D 37/34 (2006.01); F02C 7/22 (2006.01); F02C 9/40 (2006.01);
U.S. Cl.
CPC ...
F02C 7/224 (2013.01); B64D 37/04 (2013.01); B64D 37/30 (2013.01); B64D 37/34 (2013.01); F02C 3/22 (2013.01); F02C 7/222 (2013.01); F02C 9/40 (2013.01); F05D 2220/323 (2013.01); F05D 2260/213 (2013.01); F05D 2260/232 (2013.01); F05D 2260/606 (2013.01);
Abstract

An aircraft including a fuselage, a wing structure, at least one turbomachine running on hydrogen and generating thrust at a propulsion unit distant from the fuselage, at least one fuel tank positioned in the fuselage and configured to store hydrogen in the cryogenic state, at least one hydrogen supply device connecting the fuel tank and the turbomachine and including at least one pump positioned in the fuselage in the vicinity of the fuel tank, at least one hydrogen heating system positioned in the fuselage in the vicinity of the pump. This solution makes it possible to reduce a length of the complex double-walled pipes configured for carrying the hydrogen in the cryogenic state between the fuel tank and the hydrogen heating system.


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