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:
May. 23, 2017

Filed:

Sep. 13, 2016
Applicant:

Rolls-royce Plc, London, GB;

Inventors:

Stephen Gallimore, Lincoln, GB;

Paul Fletcher, Rugby, GB;

John Richard Webster, Derby, GB;

Alan Robert Maguire, Derby, GB;

Assignee:

ROLLS-ROYCE plc, London, GB;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F16C 27/04 (2006.01); G01M 13/04 (2006.01); F01D 25/16 (2006.01); F16C 41/02 (2006.01); F16C 25/08 (2006.01); F16C 19/52 (2006.01); F16C 27/08 (2006.01); F16C 33/58 (2006.01); F16C 19/54 (2006.01); F16C 19/16 (2006.01);
U.S. Cl.
CPC ...
G01M 13/04 (2013.01); F01D 25/162 (2013.01); F16C 19/522 (2013.01); F16C 19/542 (2013.01); F16C 25/083 (2013.01); F16C 27/08 (2013.01); F16C 33/586 (2013.01); F16C 41/02 (2013.01); F05D 2240/52 (2013.01); F05D 2260/83 (2013.01); F05D 2300/501 (2013.01); F16C 19/16 (2013.01); F16C 19/54 (2013.01); F16C 2233/00 (2013.01); F16C 2237/00 (2013.01); F16C 2360/23 (2013.01); Y02T 50/671 (2013.01);
Abstract

A method of determining the axial load on load-sharing thrust bearings including: providing first and second thrust bearings, each including an inner race and an outer race supported by at least one resilient element; applying a test axial load to each of the first and second thrust bearings to elastically deform the at least one resilient element so as to axially displace the outer race; determining the test axial displacement of each outer race to obtain calibration data comprising values of axial load versus axial displacement; applying an in-service axial load to the first and second thrust bearings to elastically deform the resilient elements so as to axially displace the respective outer races; measuring the in-service axial displacement of each outer race; and based on the measured in-service axial displacements, inferring from the calibration data the values of the in-service axial loads on the first and second thrust bearings.


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