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:
Mar. 22, 2022

Filed:

Apr. 27, 2017
Applicant:

Safran Aircraft Engines, Paris, FR;

Inventors:

Cédric Zaccardi, Moissy-Cramayel, FR;

Kaëlig Merwen Orieux, Moissy-Cramayel, FR;

William Henri Joseph Riera, Moissy-Cramayel, FR;

Assignee:
Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01D 9/04 (2006.01); F02K 3/06 (2006.01);
U.S. Cl.
CPC ...
F01D 9/042 (2013.01); F02K 3/06 (2013.01); F05D 2220/36 (2013.01); F05D 2250/15 (2013.01); F05D 2300/603 (2013.01); Y02T 50/60 (2013.01);
Abstract

The invention relates to a straightening assembly for an air flow of a turbomachine, comprising two respectively coaxial radially inner and outer shrouds (), between which extend the vanes () made of composite material attached, at a first end portion () thereof, to the radially inner shroud and at a second end portion () thereof, to the radially outer shroud (), with the vanes () comprising a useful portion extending between the two end portions (). According to the invention, for each vane () in a plane perpendicular to the axis of the radially inner and outer shrouds (), a straight line passing through a junction between said first and second end portions () and the useful portion forms, with a radius of the radially inner shroud passing through the junction between said first end portion and the useful portion of said vane (), an angle α such that 0°<α≤90°.


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