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.
Patent No.:
Date of Patent:
May. 06, 2025
Filed:
Sep. 28, 2023
Applicants:
Airbus Sas, Blagnac, FR;
Airbus Operations Sas, Toulouse, FR;
Inventors:
Assignees:
Airbus SAS, Blagnac, FR;
Airbus Operations SAS, Toulouse, FR;
Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F02C 7/22 (2005.12); B64D 37/30 (2005.12); F02C 3/20 (2005.12); F02C 3/22 (2005.12); B64D 27/12 (2005.12); B64D 29/02 (2005.12); B64D 29/08 (2005.12);
U.S. Cl.
CPC ...
F02C 7/222 (2012.12); B64D 37/30 (2012.12); F02C 3/20 (2012.12); F02C 3/22 (2012.12); B64D 27/12 (2012.12); B64D 29/02 (2012.12); B64D 29/08 (2012.12);
Abstract
A propulsive assembly for an aircraft with an engine system with a core in a casing and having a combustion chamber and a turbine with blades, a supply line supplying dihydrogen, an injector manifold equipped with injectors which dip into the combustion chamber, and a distribution network with several bypass lines distributed around the casing, a rear manifold connected to the supply line and to the bypass lines and a front manifold connected to the bypass lines and to the injector manifold, in which the rear manifold is at the rear of the turbine and the front manifold is at the front of the turbine.