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:
Oct. 19, 2021

Filed:

Mar. 01, 2019
Applicant:

Pratt & Whitney Canada Corp., Longueuil, CA;

Inventor:

Louis Brillon, Varennes, CA;

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02C 7/06 (2006.01); F16C 41/00 (2006.01); F02K 3/06 (2006.01); F01D 25/16 (2006.01); F16C 19/52 (2006.01);
U.S. Cl.
CPC ...
F16C 41/002 (2013.01); F01D 25/16 (2013.01); F02C 7/06 (2013.01); F02K 3/06 (2013.01); F16C 19/52 (2013.01); F05D 2220/323 (2013.01); F05D 2240/50 (2013.01); F05D 2300/20 (2013.01); F16C 2360/23 (2013.01);
Abstract

A gas turbine engine with a rotor having a shaft mounted to the engine with a plurality of electrically insulating bearings is provided. The electrically insulating bearings are coupled to the shaft to support the rotor in the engine. There is at least one electrically conductive bearing coupled to the shaft and that further support the rotor in the engine. An electrically conductive path is defined between the rotor and an electrical ground of the engine. The electrically conductive path is defined through the electrically conductive bearing to reach the electrical ground of the engine. A method for electrostatically discharging a rotor supported in the gas turbine engine is also provided.


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