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:
May. 28, 2019

Filed:

May. 20, 2016
Applicant:

United Technologies Corporation, Farmington, CT (US);

Inventors:

Russell J. Bergman, Windsor, CT (US);

Jeffrey Michael Jacques, East Hartford, CT (US);

Daniel Belotto, Palm Beach Gardens, FL (US);

Assignee:

United Technologies Corporation, Farmington, CT (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F01D 9/02 (2006.01); F01D 11/00 (2006.01); F01D 25/24 (2006.01); F02C 3/04 (2006.01);
U.S. Cl.
CPC ...
F01D 9/02 (2013.01); F01D 11/005 (2013.01); F01D 25/24 (2013.01); F01D 25/246 (2013.01); F02C 3/04 (2013.01); F05D 2220/32 (2013.01); F05D 2240/12 (2013.01); F05D 2240/55 (2013.01); F05D 2250/14 (2013.01);
Abstract

A turbine vane for a gas turbine engine includes an outer platform including a first side spaced circumferentially apart from a second side, a forward end and an aft end. The first side includes a first gusset extending between the forward end and the aft end. The first gusset defines a first radius beginning at the forward end that transitions into an elliptical curve toward the aft end. An inner platform is also included. An airfoil extends between the outer platform and the inner platform. A gas turbine engine is also disclosed.


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