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. 21, 2013

Filed:

Jan. 31, 2012
Applicants:

Kathleen R. Phillips, Coventry, CT (US);

Thomas G. Phillips, Coventry, CT (US);

Ethan K. Stearns, Mansfield, CT (US);

Federico Papa, Ellington, CT (US);

Inventors:

Kathleen R. Phillips, Coventry, CT (US);

Thomas G. Phillips, Coventry, CT (US);

Ethan K. Stearns, Mansfield, CT (US);

Federico Papa, Ellington, CT (US);

Assignee:

United Technologies Corporation, Hartford, CT (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F02C 7/06 (2006.01); F02C 1/00 (2006.01); F02K 99/00 (2009.01); F01D 25/18 (2006.01); F02K 9/64 (2006.01);
U.S. Cl.
CPC ...
F01D 25/18 (2013.01); F02K 9/64 (2013.01);
Abstract

A lubricant supply system for a gas turbine engine has a lubricant lube pump delivering lubricant to an outlet line. The outlet line is split into at least a hot line and into a cool line, with the hot line directed primarily to locations associated with an engine that are not intended to receive cooler lubricant, and the cool line directed through one or more heat exchangers at which lubricant is cooled. The cool line then is routed to a fan drive gear for an associated gas turbine engine. A method and apparatus are disclosed.


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