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:
Jan. 14, 2020

Filed:

May. 01, 2018
Applicant:

Florida Turbine Technologies, Inc., Jupiter, FL (US);

Inventors:

Ross H Peterson, Palm Beach Gardens, FL (US);

John A Orosa, Palm Beach Gardens, FL (US);

Robert A Ress, Jr., Carmel, IN (US);

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F16C 7/06 (2006.01); F16C 37/00 (2006.01); F02C 7/06 (2006.01); F02C 7/18 (2006.01); F02C 7/28 (2006.01); F16C 19/36 (2006.01); F16C 33/80 (2006.01);
U.S. Cl.
CPC ...
F16C 37/007 (2013.01); F02C 7/06 (2013.01); F02C 7/18 (2013.01); F02C 7/28 (2013.01); F16C 19/361 (2013.01); F16C 33/80 (2013.01); F05D 2220/323 (2013.01); F05D 2240/50 (2013.01); F05D 2240/55 (2013.01); F05D 2260/221 (2013.01); F16C 2360/24 (2013.01);
Abstract

An aero gas turbine engine with a fan stage and a bearing rotatably supporting the fan stage, where the bearing is cooled by passing cooling air through the bearing, and the spent bearing cooling air is re-injected into the air flow path at a location where the effect is minimalized. The location is just downstream from a leading edge of a stator vane and along a pressure side surface of the vane. A fine mist of oil can be discharged into the bearing cooling air to also lubricate the bearing, where both the oil and the spent cooling air is reintroduced into the air flow path.


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