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. 18, 2025

Filed:

Jul. 19, 2023
Applicant:

Pratt & Whitney Canada Corp., Longueuil, CA;

Inventors:

Dikran Mangardich, Richmond Hill, CA;

Krishna Prasad Balike, Brampton, CA;

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F01D 5/34 (2006.01); F01D 5/06 (2006.01);
U.S. Cl.
CPC ...
F01D 5/34 (2013.01); F01D 5/06 (2013.01); F05D 2220/323 (2013.01); F05D 2240/80 (2013.01); F05D 2260/94 (2013.01);
Abstract

An integrally bladed rotor for an aircraft engine includes a hub and a circumferential array of blades extending from the hub. Each blade has an airfoil extending from a gaspath side of a platform provided at a periphery of the hub. The platform has a radial thickness T. An edge of the airfoil is disposed at an axial distance Lfrom an adjacent axial edge of the platform. A projection extends radially inwardly from an interior side of the platform opposite to the gaspath side. The projection has an axial thickness t, a radial height h from the interior side of the platform, and an axial distance Lfrom the adjacent axial edge of the platform. T is a radial thickness of the platform at an axial location of the projection, and


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