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. 28, 2018

Filed:

May. 26, 2015
Applicant:

Pratt & Whitney Canada Corp., Longueuil, CA;

Inventors:

Enzo Macchia, Kleinburg, CA;

George Guglielmin, Toronto, CA;

Bhawan Patel, Mississauga, CA;

Joe Lanzino, Orangeville, CA;

Assignee:
Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F04D 29/54 (2006.01); F01D 9/04 (2006.01); F04D 29/32 (2006.01); F01D 5/14 (2006.01); F04D 29/68 (2006.01);
U.S. Cl.
CPC ...
F04D 29/542 (2013.01); F01D 5/145 (2013.01); F01D 9/041 (2013.01); F04D 29/324 (2013.01); F04D 29/681 (2013.01); F05D 2230/232 (2013.01); F05D 2240/122 (2013.01); F05D 2240/127 (2013.01); F05D 2240/304 (2013.01); F05D 2250/11 (2013.01); F05D 2270/17 (2013.01); Y02T 50/671 (2013.01); Y02T 50/673 (2013.01);
Abstract

A stator airfoil of a gas turbine engine according to one embodiment includes at least two winglets projecting transversely from opposed sides of a stator airfoil, respectively. Each winglet includes a leading edge axially and outwardly extending from one of the opposed sides of the stator airfoil and a trailing edge extending from the stator airfoil to join with the leading edge of the winglet. The winglets therefore provide a wide trailing edge thereof to aerodynamically manage boundary layers and micro-shocks of a working fluid.


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