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:
Oct. 29, 2019
Filed:
Sep. 29, 2015
Applicant:
Safran Aircraft Engines, Paris, FR;
Inventors:
Simon Pierre Claude Charbonnier, Moissy-Cramayel, FR;
Matthieu Yoann Perrier, Moissy-Cramayel, FR;
Assignee:
SAFRAN AIRCRAFT ENGINES, Paris, FR;
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F03B 1/04 (2006.01); F01D 5/14 (2006.01); F01D 9/04 (2006.01); F01D 17/16 (2006.01); F01D 25/16 (2006.01); F02C 9/18 (2006.01); F04D 29/54 (2006.01); F04D 29/56 (2006.01);
U.S. Cl.
CPC ...
F01D 5/142 (2013.01); F01D 9/041 (2013.01); F01D 17/162 (2013.01); F01D 25/162 (2013.01); F02C 9/18 (2013.01); F04D 29/544 (2013.01); F04D 29/542 (2013.01); F04D 29/563 (2013.01); Y02T 50/671 (2013.01); Y02T 50/673 (2013.01);
Abstract
A stator of an aircraft turbine engine, comprising an annular row of fixed vanes and an annular row of arms, wherein the trailing edges of the fixed vanes are positioned substantially in a first transverse plane that is positioned downstream of a second transverse plane that passes substantially through the leading edges of the arms.
Charbonnier, Simon Pierre Claude. (2019). Stator of an aircraft turbine engine (U.S. Patent No. 10458247). U.S. Patent and Trademark Office. https://idiyas.com/patent/badge/10458247
Data source: USPTO (United States Patent and Trademark Office) public patent records. Weekly synchronization. How IDiyas builds this profile