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:

Jan. 19, 2018
Applicant:

United Technologies Corporation, Farmington, CT (US);

Inventors:

Matthew D. Teicholz, Mystic, CT (US);

Francis Parnin, Suffield, CT (US);

Richard Alan Weiner, Farmington, CT (US);

Katherine A. Knapp Carney, Tolland, CT (US);

Assignee:

RAYTHEON TECHNOLOGIES CORPORATION, Farmington, CT (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02C 7/06 (2006.01); F01D 25/20 (2006.01); F02C 7/14 (2006.01); F01M 1/16 (2006.01); F16H 57/04 (2010.01); F02C 3/107 (2006.01); F02C 7/36 (2006.01); F01M 13/04 (2006.01);
U.S. Cl.
CPC ...
F02C 7/06 (2013.01); F01D 25/20 (2013.01); F01M 1/16 (2013.01); F02C 3/107 (2013.01); F02C 7/14 (2013.01); F02C 7/36 (2013.01); F16H 57/0435 (2013.01); F01M 2013/0472 (2013.01); F05D 2260/53 (2013.01); F16N 2250/08 (2013.01);
Abstract

A method of controlling lubrication flow to a first engine component, a second engine component and a lubrication tank of a gas turbine engine according to an example of the present disclosure includes, among other things, determining more than one condition experienced by the gas turbine engine, comparing with a processor on a controller the more than one condition against an engine performance model stored in memory on the controller, wherein the engine performance model includes stored relationship values between the more than one condition and a position of a scheduling valve, the scheduling valve disposed between the lubricant tank and the first engine component and between the lubricant tank and the second engine component, pumping a lubricant from the lubricant tank through a conduit to the scheduling valve using a pump, and controlling the position of the scheduling valve to vary a flow of the lubricant to two or more of the first engine component, the second engine component and the lubrication tank based upon the comparing of the more than one condition experienced by the gas turbine engine.


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