Invention Grant
- Patent Title: Method of balancing a gas turbine engine rotor
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Application No.: US14531438Application Date: 2014-11-03
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Publication No.: US09638037B2Publication Date: 2017-05-02
- Inventor: Paul Stone , Richard Ivakitch
- Applicant: Pratt & Whitney Canada Corp.
- Applicant Address: unknown Longueuil, Quebec
- Assignee: PRATT & WHITNEY CANADA CORP.
- Current Assignee: PRATT & WHITNEY CANADA CORP.
- Current Assignee Address: unknown Longueuil, Quebec
- Agency: Norton Rose Fulbright Canada
- Main IPC: F01D5/02
- IPC: F01D5/02 ; G01M1/30 ; G01M1/34 ; G01M1/32 ; G01M1/36

Abstract:
A method of balancing a gas turbine engine rotor, including axisymmetrically removing an annular portion of the balancing flange exceeding that required to provide the unbalance correction, and creating the unbalance correction by non-axisymmetrically removing material from the balancing flange. In one embodiment, the configuration of a theoretical notch in the balancing flange that would create the unbalance correction is determined. The unbalance correction is created by removing material from the balancing flange to create a protuberance protruding radially from a remainder of the balancing flange, the protuberance having a height corresponding to the depth of the theoretical notch, a circumferential width corresponding to the arc angle of the theoretical notch, and a circumferential position diametrically opposed to the circumferential position of the theoretical notch. A gas turbine engine rotor is also discussed.
Public/Granted literature
- US20160123150A1 METHOD OF BALANCING A GAS TURBINE ENGINE ROTOR Public/Granted day:2016-05-05
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