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:
Feb. 04, 2020

Filed:

Oct. 11, 2016
Applicant:

General Electric Company, Schenectady, NY (US);

Inventors:

Thomas Ory Moniz, Loveland, OH (US);

Daniel Robert Dwyer, West Chester, OH (US);

Mark John Laricchiuta, West Chester, OH (US);

Jeffrey Donald Clements, Mason, OH (US);

Brandon Wayne Miller, Liberty Township, OH (US);

Assignee:

General Electric Company, Schenectady, NY (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01D 25/20 (2006.01); F01D 25/18 (2006.01); F01D 11/02 (2006.01); F01D 11/04 (2006.01); F02C 6/06 (2006.01); F02C 7/06 (2006.01); F02C 3/04 (2006.01);
U.S. Cl.
CPC ...
F01D 25/20 (2013.01); F01D 11/02 (2013.01); F01D 11/04 (2013.01); F01D 25/18 (2013.01); F01D 25/183 (2013.01); F02C 6/06 (2013.01); F02C 7/06 (2013.01); F02C 3/04 (2013.01);
Abstract

A gas turbine engine includes a fan section and a core turbine engine operable with the fan section. The gas turbine engine also includes a sump pressurization assembly including a valve, a first duct in airflow communication with the valve and a first pressurized air source, and a second duct in airflow communication with the valve and a second pressurized air source. Further, the sump pressurization assembly includes a supply duct selectively in airflow communication with the first duct and the second duct through the valve. The supply duct is located at least partially inward of a core air flowpath of the core turbine engine for pressurizing a sump of the gas turbine engine.


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