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:
Nov. 24, 2020

Filed:

Jun. 09, 2017
Applicant:

Safran Aircraft Engines, Paris, FR;

Inventors:

Pradeep Cojande, Melun, FR;

Hanna Reiss, Pontault-Combault, FR;

Assignee:
Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01D 9/04 (2006.01); F01D 1/04 (2006.01); F04D 29/54 (2006.01); F01D 5/14 (2006.01);
U.S. Cl.
CPC ...
F01D 9/04 (2013.01); F01D 1/04 (2013.01); F01D 5/141 (2013.01); F01D 9/041 (2013.01); F04D 29/544 (2013.01); F05B 2250/71 (2013.01); F05D 2220/36 (2013.01); F05D 2240/121 (2013.01); Y02T 50/673 (2013.01);
Abstract

A set of turbomachine guide vanes including plural vanes arranged around an annulus, each vane having a leading edge extending between root and tip ends, the leading edge offset between these two ends being greater than 10% of the blade height. A tangential stacking of the guide vanes towards the suction face side, the curve of tangential stacking, of the position, in the direction tangential to the annulus, of centers of gravity of successive vane cross sections along the vane height, is a curve that increases constantly towards the suction face side. The curve, near the vane tip end, has an accentuated gradient towards the suction face side compared with the rest of the curve, and has a mean gradient near the vane tip end that is greater than at least 1.2 times the mean gradient of the curve over the portion between 30% and 90% of the vane height.


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