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. 02, 2018

Filed:

Dec. 20, 2013
Applicant:

Pratt & Whitney Canada Corp., Longueuil, CA;

Inventors:

Bruce Alan Calvert, Burlington, CA;

Richard Brian Wirth, Stoney Creek, CA;

Danny Krause, Puslinch, CA;

Assignee:
Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01D 5/02 (2006.01); F01D 17/02 (2006.01); F01D 17/06 (2006.01); G01M 15/14 (2006.01);
U.S. Cl.
CPC ...
F01D 5/027 (2013.01); F01D 17/02 (2013.01); F01D 17/06 (2013.01); F05D 2260/15 (2013.01); G01M 15/14 (2013.01);
Abstract

Devices and methods useful for balancing high-pressure spools of gas turbine engines are disclosed. An exemplary device may comprise: an input shaft configured to be coupled to an output of an accessory gear box driven by a high-pressure spool of a gas turbine engine; a first trigger rotatably coupled to the input shaft at a first speed ratio; and a sensor configured to detect the trigger at each revolution of the trigger. The first speed ratio may permit a rotational speed of the first trigger to be substantially the same as a rotational speed of the high-pressure spool. Upon detection of the trigger, the sensor may generate one or more signals representative of each associated revolution of the high-pressure spool of the gas turbine engine.


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