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:
Jul. 23, 2024
Filed:
Feb. 23, 2021
Applicant:
Safran Helicopter Engines, Bordes, FR;
Inventors:
Nicolas Roland Guy Savary, Moissy-Cramayel, FR;
Christophe Lailhacar, Moissy-Cramayel, FR;
Olivier Lamaison, Moissy-Cramayel, FR;
Stéphane Lavignotte, Moissy-Cramayel, FR;
Assignee:
SAFRAN HELICOPTER ENGINES, Bordes, FR;
Primary Examiner:
Int. Cl.
CPC ...
F23R 3/28 (2006.01); F02C 7/22 (2006.01); F02C 9/26 (2006.01);
U.S. Cl.
CPC ...
F23R 3/283 (2013.01); F02C 7/222 (2013.01); F02C 9/26 (2013.01); F02C 7/22 (2013.01);
Abstract
A combustion assembly for a gas turbine includes a flame tube and a fuel supply including a flow rate limiter supplying an injector. The flow rate limiter and the fuel injector are formed in one piece.
Savary, Nicolas Roland Guy. (2024). Integral flow rate limiter and fuel injector for a gas turbine combustor (U.S. Patent No. 12044410). U.S. Patent and Trademark Office. https://idiyas.com/patent/badge/12044410
Data source: USPTO (United States Patent and Trademark Office) public patent records. Weekly synchronization. How IDiyas builds this profile