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:
Dec. 10, 2019

Filed:

Dec. 06, 2016
Applicant:

General Electric Company, Schenectady, NY (US);

Inventor:

Keith Cletus Belsom, Laurens, SC (US);

Assignee:

GENERAL ELECTRIC COMPANY, Schenectady, NY (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02C 7/28 (2006.01); F23R 3/60 (2006.01); F01D 9/04 (2006.01); F01D 11/00 (2006.01); F01D 9/02 (2006.01); F02C 3/14 (2006.01); F23R 3/46 (2006.01);
U.S. Cl.
CPC ...
F02C 7/28 (2013.01); F01D 9/023 (2013.01); F01D 9/041 (2013.01); F01D 11/003 (2013.01); F02C 3/14 (2013.01); F23R 3/46 (2013.01); F23R 3/60 (2013.01); F05D 2220/3212 (2013.01); F05D 2240/55 (2013.01); F23R 2900/00012 (2013.01);
Abstract

A gas turbine engine includes a gas turbine and a plurality of combustors each in fluid communication with the gas turbine. The gas turbine engine includes a first seal disposed between the gas turbine and the plurality of turbine combustors. The first seal is configured to sealingly engage with the gas turbine and at least two of the plurality of turbine combustors. The gas turbine engine also includes a second seal disposed between the gas turbine and the plurality of turbine combustors. The second seal is configured to sealingly engage with the gas turbine and at least two of the plurality of turbine combustors.


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