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. 07, 2019

Filed:

Sep. 30, 2015
Applicant:

General Electric Company, Schenectady, NY (US);

Inventors:

Narendra Digamber Joshi, Guilderland, NY (US);

Christian Lee Vandervort, Voorheesville, NY (US);

Krishan Lal Luthra, Guilderland, NY (US);

Ronald Scott Bunker, West Chester, OH (US);

Joel Meier Haynes, Niskayuna, NY (US);

Venkat Eswarlu Tangirala, Niskayuna, NY (US);

Assignee:

GENERAL ELECTRIC COMPANY, Schenectady, NY (US);

Attorneys:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F02C 1/00 (2006.01); F02C 3/34 (2006.01); F02C 1/08 (2006.01); F01D 5/18 (2006.01); F23R 3/00 (2006.01); F02C 6/00 (2006.01); F02C 7/18 (2006.01); F23C 9/08 (2006.01); F01D 25/32 (2006.01);
U.S. Cl.
CPC ...
F01D 5/186 (2013.01); F01D 25/32 (2013.01); F02C 3/34 (2013.01); F02C 6/003 (2013.01); F02C 7/185 (2013.01); F23C 9/08 (2013.01); F23R 3/002 (2013.01); F02C 1/005 (2013.01); F02C 1/08 (2013.01); F05D 2260/213 (2013.01); F05D 2260/61 (2013.01); F05D 2300/6033 (2013.01); F23M 2900/05004 (2013.01); F23N 2021/12 (2013.01); F23R 2900/03041 (2013.01); F23R 2900/03341 (2013.01); Y02E 20/14 (2013.01); Y02E 20/16 (2013.01);
Abstract

A turbine assembly is provided. The turbine assembly includes a gas turbine engine including at least one hot gas path component formed at least partially from a ceramic matrix composite material. The turbine assembly also includes a treatment system positioned to receive a flow of exhaust gas from the gas turbine engine. The treatment system is configured to remove water from the flow of exhaust gas to form a flow of treated exhaust gas, and to channel the flow of treated exhaust gas towards the at least one hot gas path component. The at least one hot gas path component includes a plurality of cooling holes for channeling the flow of treated exhaust gas therethrough, such that a protective film is formed over the at least one hot gas path component.


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