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. 14, 2023

Filed:

Dec. 15, 2020
Applicant:

Pratt & Whitney Canada Corp., Longueuil, CA;

Inventors:

Daniel Lecuyer, St-Bruno-de-Montarville, CA;

Michael Paolucci, Kirkland, CA;

Francis Gemme, Saint-Lambert, CA;

Assignee:
Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01D 5/14 (2006.01); F01D 9/02 (2006.01);
U.S. Cl.
CPC ...
F01D 9/02 (2013.01); F01D 5/147 (2013.01); F01D 5/141 (2013.01); F01D 5/143 (2013.01); F05D 2220/32 (2013.01); F05D 2230/00 (2013.01); F05D 2240/12 (2013.01); F05D 2240/24 (2013.01); F05D 2240/80 (2013.01); F05D 2250/71 (2013.01);
Abstract

An airfoil for a gas turbine engine, which has an airfoil body extending in a spanwise direction and in a chordwise direction, a platform located at an inner end and/or an outer end of the airfoil body, and a fillet at a junction between the airfoil body and the platform. The fillet has a radius distribution at a given chordwise location, the radius distribution varying from the platform to the airfoil body in the spanwise direction. The radius distribution defines a local minimum, the radius of the fillet at the given chordwise location increasing from the local minimum along the spanwise direction toward both of the airfoil and the platform. A local maximum of the radius distribution is offset from the local minimum along the spanwise direction, the radius decreasing from the local maximum along the spanwise direction toward both of the airfoil and the platform.


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