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:
Feb. 04, 2025

Filed:

Dec. 12, 2022
Applicant:

Safran Aircraft Engines, Paris, FR;

Inventors:

Eva Julie Lebeault, Moissy-Cramayel, FR;

Laurent Soulat, Moissy-Cramayel, FR;

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02C 6/20 (2006.01); B64C 11/20 (2006.01); F01D 9/04 (2006.01); B64C 11/08 (2006.01); F02C 7/20 (2006.01);
U.S. Cl.
CPC ...
F01D 9/041 (2013.01); B64C 11/20 (2013.01); F02C 6/206 (2013.01); B64C 11/08 (2013.01); F02C 7/20 (2013.01); F05D 2220/325 (2013.01);
Abstract

An aircraft including at least one unducted turbine engine for the propulsion of the aircraft. The turbine engine comprising: a rotor and a stator comprising a plurality of stator blades extending radially with respect to the longitudinal axis, each stator blade being defined, in a plane transverse to the longitudinal axis, by an angular position; and at least one aerodynamic obstruction positioned close to the turbine engine. The stator of the turbine engine comprises stator blades having a first chord, referred to as conventional blades, and at least one stator blade having a second chord larger than the first chord, referred to as the elongate blade, said at least one elongate blade being positioned in an interference angular range defined opposite the aerodynamic obstacle, so as to increase the straightening of the airflow from the rotor in the interference angular range.


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