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:
Feb. 07, 2023

Filed:

Nov. 11, 2021
Applicant:

Pratt & Whitney Canada Corp., Longueuil, CA;

Inventors:

Constantinos Ravanis, Candiac, CA;

Vincent Paradis, Longueuil, CA;

Eduardo Hawie, Woodbridge, CA;

Michael Papple, Verdun, CA;

Marc-Antoine Mailloux-Labrousse, St-Lambert, CA;

Othmane Leghzaouni, Boucherville, CA;

Philippe Boyer, Saint-Isidore-de-Laprairie, CA;

Jasrobin Grewal, Pincourt, CA;

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F01D 5/14 (2006.01);
U.S. Cl.
CPC ...
F01D 5/141 (2013.01); F05D 2220/32 (2013.01); F05D 2240/30 (2013.01);
Abstract

A turbine blade for a gas turbine engine has an airfoil including leading and trailing edges joined by spaced-apart pressure and suction sides to provide an external airfoil surface extending from a platform in a spanwise direction to a tip. The external airfoil surface is formed in substantial conformance with multiple cross-sectional profiles of the airfoil defined by a set of Cartesian coordinates set forth in Table 1, the Cartesian coordinates provided by an axial coordinate scaled by a local axial chord, a circumferential coordinate scaled by a local axial chord, and a span location.


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