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:
Aug. 20, 2019

Filed:

Feb. 09, 2016
Applicant:

Safran Aircraft Engines, Paris, FR;

Inventors:

Henri-Marie Damevin, Moissy-Cramayel, FR;

Philippe Jacques Pierre Fessou, Moissy-Cramayel, FR;

Vianney Christophe Marie Maniere, Moissy-Cramayel, FR;

Michael Franck Antoine Schvallinger, Moissy-Cramayel, FR;

Assignee:

SNECMA, Paris, FR;

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01D 9/04 (2006.01); F01D 5/14 (2006.01); F02K 3/06 (2006.01); F04D 29/54 (2006.01); F04D 29/66 (2006.01); F04D 29/68 (2006.01); F01D 25/16 (2006.01);
U.S. Cl.
CPC ...
F01D 9/041 (2013.01); F01D 5/141 (2013.01); F01D 25/162 (2013.01); F02K 3/06 (2013.01); F04D 29/544 (2013.01); F04D 29/667 (2013.01); F04D 29/681 (2013.01); F05D 2220/32 (2013.01); F05D 2240/123 (2013.01); F05D 2260/97 (2013.01); Y02T 50/673 (2013.01);
Abstract

The invention relates to a turbine engine air flow guide assembly including: a structural arm (); and a guide vane () on the lower surface of the structural arm, comprising a leading edge (), a trailing edge (), and a camber line (), said vane and arm extending radially about an axis (X-X) of the turbine engine and defining therebetween an air flow channel. The structural arm () comprises: an upstream end () having a guide vane profile () and comprising a leading edge () aligned with that of the vane; and a shoulder () located on the lower surface of the arm, defining a neck in the channel. The assembly is characterized in that the area (A) of the section of the channel at the neck is between 0.7 and 0.9 times the area (A) of the section of the channel at the leading edges.


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