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:
Nov. 10, 2020

Filed:

Mar. 07, 2018
Applicant:

General Electric Company, Schenectady, NY (US);

Inventors:

Kyle Robert Snow, Loveland, OH (US);

Andrew Michael Tompkins, Cincinnati, OH (US);

Andrew Michael Watson, Cincinnati, OH (US);

Philip Joseph Ogston, Cincinnati, OH (US);

Christopher Michael Thompson, West Chester, OH (US);

Assignee:

General Electric Company, Schenectady, NY (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F01D 3/04 (2006.01); F01D 21/14 (2006.01); F01D 21/00 (2006.01); F01D 25/16 (2006.01); F16C 19/10 (2006.01); G01H 9/00 (2006.01); G01L 5/00 (2006.01); F16C 19/52 (2006.01); G01L 19/12 (2006.01); F02C 7/06 (2006.01); F16C 19/02 (2006.01); F16C 19/16 (2006.01);
U.S. Cl.
CPC ...
F01D 21/14 (2013.01); F01D 3/04 (2013.01); F01D 21/003 (2013.01); F01D 25/16 (2013.01); F16C 19/10 (2013.01); F16C 19/522 (2013.01); F16C 19/527 (2013.01); G01H 9/004 (2013.01); G01L 5/0019 (2013.01); G01L 19/12 (2013.01); F02C 7/06 (2013.01); F05D 2220/323 (2013.01); F05D 2240/52 (2013.01); F05D 2260/15 (2013.01); F05D 2270/334 (2013.01); F05D 2270/54 (2013.01); F16C 19/02 (2013.01); F16C 19/163 (2013.01); F16C 2233/00 (2013.01); F16C 2326/43 (2013.01); F16C 2360/23 (2013.01);
Abstract

Rotor thrust balancing systems for turbomachines and methods of using the same are generally disclosed. For example, a rotor thrust balancing system for a turbomachine, wherein the turbomachine defines a centerline extending the length of the turbomachine. The system includes a rotating drive shaft, a thrust bearing, and a first waveguide sensor. The rotating drive shaft couples a turbine section and a compressor section of the turbomachine. The thrust bearing supports the rotating drive shaft of the turbomachine. The thrust bearing includes a plurality of ball bearings, an inner race coupled to the rotating drive shaft, and an outer race coupled to a fixed structure. The first waveguide sensor is coupled to the outer race at a first end of the waveguide sensor. The waveguide sensor communicates a vibrational frequency from the thrust bearing to a second end of the waveguide sensor.


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