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:
Jul. 06, 2021

Filed:

Feb. 04, 2014
Applicant:

United Technologies Corporation, Hartford, CT (US);

Inventors:

Frederick M. Schwarz, Glastonbury, CT (US);

Simon Pickford, Amston, CT (US);

Assignee:

Raytheon Technologies Corporation, Farmington, CT (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01D 25/20 (2006.01); F02C 7/14 (2006.01); F02C 3/107 (2006.01); F01D 25/18 (2006.01); F01D 25/12 (2006.01); F01D 1/02 (2006.01); F01D 15/10 (2006.01); F01D 15/12 (2006.01); F01D 25/08 (2006.01); F01D 25/16 (2006.01);
U.S. Cl.
CPC ...
F01D 25/20 (2013.01); F01D 1/02 (2013.01); F01D 15/10 (2013.01); F01D 15/12 (2013.01); F01D 25/08 (2013.01); F01D 25/125 (2013.01); F01D 25/16 (2013.01); F01D 25/18 (2013.01); F02C 3/107 (2013.01); F02C 7/14 (2013.01); F05D 2220/30 (2013.01); F05D 2260/20 (2013.01); F05D 2260/213 (2013.01); F05D 2260/40311 (2013.01); F05D 2260/98 (2013.01); Y02T 50/60 (2013.01);
Abstract

A turbine engine system includes a first lubricant circuit, a second lubricant circuit, a plurality of engine stages and a shaft. The first lubricant circuit includes a first turbine engine component that is fluidly coupled with a first lubricant heat exchanger. The second lubricant circuit includes a second turbine engine component that is fluidly coupled with a second lubricant heat exchanger, wherein the second lubricant circuit is fluidly separate from the first lubricant circuit. The first turbine engine component includes a gear train, which connects a first of the engine stages to a second of the engine stages. The second turbine engine component includes a bearing. The shaft is supported by the bearing and connected to one of the engine stages.


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