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:
Jun. 03, 2025

Filed:

Dec. 07, 2022
Applicant:

Safran Aircraft Engines, Paris, FR;

Inventors:

Raul Martinez Luque, Moissy-Cramayel, FR;

Damien Bernard Emeric Guegan, Moissy-Cramayel, FR;

Antoine Claude Baudouin Raoul Marie Secondat De Montesquieu, Moissy-Cramayel, FR;

Laurent Soulat, Moissy-Cramayel, FR;

Michael Franck Antoine Schvallinger, Moissy-Cramayel, FR;

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02C 9/22 (2006.01); F01D 17/16 (2006.01);
U.S. Cl.
CPC ...
F02C 9/22 (2013.01); F01D 17/16 (2013.01); F05D 2220/323 (2013.01);
Abstract

Aircraft turbine engine including two coaxial annular walls defining between them a main annular duct for the flow of a primary airflow; —a rotor blading extending radially through the first duct; —an annular separator arranged downstream of the rotor blading and configured to divide the primary airflow into two to form the secondary air flows; —first variable guide vanes which are distributed around the shaft and each comprise a leading edge which is located upstream of the separator and trailing edges which are located in the secondary airflows; —and fixed guide vanes which are distributed around the shaft in the external airflow and downstream of the first variable vanes.


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