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:
Apr. 03, 2018

Filed:

May. 29, 2014
Applicant:

Pratt & Whitney Canada Corp., Longueuil, CA;

Inventors:

Jiemin Wang, Mississauga, CA;

Cameron Walters, Newmarket, CA;

Ron Robinson, Brampton, CA;

Jeffrey Bernard Heyerman, Oakville, CA;

David Beamish, Mississauga, CA;

Assignee:

PRATT & WHITNEY CANADA CORP., Longueuil, QC, CA;

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01D 5/02 (2006.01); G01M 1/32 (2006.01);
U.S. Cl.
CPC ...
F01D 5/027 (2013.01); G01M 1/32 (2013.01); F05D 2230/60 (2013.01); F05D 2260/81 (2013.01); Y10T 29/49321 (2015.01);
Abstract

A method of balancing a spool of a gas turbine engine, the spool including a forward rotor assembly and an aft rotor assembly separated by a spacer, the method comprising: balancing the forward rotor assembly and the aft rotor assembly independently from one another using conventional balancing techniques; and mathematically modeling the spool; applying a modeled axial load to the modeled spool to determine a trim weight which would balance the spool when subjected to the modeled axial load; and physically placing the trim weight to one of the forward rotor assembly and the aft rotor assembly.


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