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:
Jun. 22, 2021

Filed:

May. 15, 2017
Applicant:

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

Inventors:

Russell B. Jones, North Palm Beach, FL (US);

Joseph D. Brostmeyer, Jupiter, FL (US);

Justin T. Cejka, Palm Beach Gardens, FL (US);

John E. Ryznic, Jupiter, FL (US);

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02C 3/13 (2006.01); F02C 3/00 (2006.01); F02C 6/00 (2006.01); F01D 15/10 (2006.01); F01D 17/14 (2006.01); F02C 7/18 (2006.01); F02C 9/18 (2006.01); F02C 9/22 (2006.01);
U.S. Cl.
CPC ...
F02C 3/13 (2013.01); F01D 15/10 (2013.01); F01D 17/14 (2013.01); F02C 3/00 (2013.01); F02C 6/00 (2013.01); F02C 7/18 (2013.01); F02C 9/18 (2013.01); F02C 9/22 (2013.01); F05D 2220/32 (2013.01); F05D 2220/76 (2013.01); F05D 2230/80 (2013.01); F05D 2240/35 (2013.01); F05D 2260/202 (2013.01); F05D 2260/211 (2013.01);
Abstract

A process for retrofitting an industrial gas turbine engine of a power plant where an old industrial engine with a high spool has a new low spool with a low pressure turbine that drives a low pressure compressor using exhaust gas from the high pressure turbine, and where the new low pressure compressor delivers compressed air through a new compressed air line to the high pressure compressor through a new inlet added to the high pressure compressor. The old electric generator is replaced with a new generator having around twice the electrical power production. One or more stages of vanes and blades are removed from the high pressure compressor to optimally match a pressure ratio split. Closed loop cooling of one or more new stages of vanes and blades in the high pressure turbine is added and the spent cooling air is discharged into the combustor.


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