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. 26, 2019

Filed:

Dec. 21, 2015
Applicant:

Pratt & Whitney Canada Corp., Longueuil, CA;

Inventors:

Ignatius Theratil, Mississauga, CA;

Krishna Prasad Balike, Mississauga, CA;

Richard Ivakitch, Toronto, CA;

Sean Michael Kelly, Milton, CA;

Peter Townsend, Mississauga, CA;

Ronald Dutton, Mississauga, CA;

Paul Stone, Guelph, CA;

Robert Venditti, Woodbridge, CA;

Daniel Fudge, Vaughan, CA;

Milica Kojovic, Oakville, CA;

Aldo Abate, Longueuil, CA;

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F04D 29/66 (2006.01); F01D 5/16 (2006.01); F04D 29/32 (2006.01); F04D 29/38 (2006.01); F01D 5/14 (2006.01); F01D 5/28 (2006.01);
U.S. Cl.
CPC ...
F04D 29/666 (2013.01); F01D 5/16 (2013.01); F01D 5/141 (2013.01); F01D 5/28 (2013.01); F04D 29/324 (2013.01); F04D 29/384 (2013.01);
Abstract

A compressor rotor for a gas turbine engine is described which includes sets of blades having different airfoil thickness distributions, each including a frequency modifier forming a thickness differential relative to a baseline blade thickness. The frequency modifiers provide different natural vibration frequencies for each of the blades, and facilitate modifying natural vibration frequency separation between adjacent blades of the compressor rotor.


Find Patent Forward Citations

Loading…