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:
Feb. 24, 2026
Filed:
Jan. 18, 2023
Applicant:
Safran Aircraft Engines, Paris, FR;
Inventors:
Jacques Auriol, Moissy-Cramayel, FR;
Pierre-Alain Jean Philippe Reigner, Moissy-cramayel, FR;
Assignee:
SAFRAN AIRCRAFT ENGINES, Paris, FR;
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64D 33/00 (2006.01); B60L 7/06 (2006.01); B64D 31/00 (2024.01); F02K 1/66 (2006.01); F02K 1/76 (2006.01);
U.S. Cl.
CPC ...
B64D 33/00 (2013.01); B60L 7/06 (2013.01); B64D 31/00 (2013.01); F02K 1/66 (2013.01); F02K 1/76 (2013.01); F05D 2260/70 (2013.01); F05D 2260/901 (2013.01);
Abstract
Method for braking an aircraft turbine engine including a fan or a propeller connected to a turbine by a shaft and an electric generator connected to the shaft, the method comprising the following steps:
Quick Actions:
Auriol, Jacques. (2026). Method for braking an aircraft turbine engine (U.S. Patent No. 12559248). U.S. Patent and Trademark Office. https://idiyas.com/patent/badge/12559248
Data source: USPTO (United States Patent and Trademark Office) public patent records. Weekly synchronization. How IDiyas builds this profile