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. 11, 2018

Filed:

Sep. 15, 2015
Applicants:

Joseph D Brostmeyer, Jupiter, FL (US);

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

Inventors:

Joseph D Brostmeyer, Jupiter, FL (US);

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

Assignee:
Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01D 15/10 (2006.01); F02C 3/10 (2006.01); F01D 1/04 (2006.01); F02C 3/04 (2006.01); F02C 9/22 (2006.01);
U.S. Cl.
CPC ...
F01D 15/10 (2013.01); F01D 1/04 (2013.01); F02C 3/10 (2013.01); F02C 3/04 (2013.01); F02C 9/22 (2013.01); F05D 2220/32 (2013.01); F05D 2220/3213 (2013.01); F05D 2220/3215 (2013.01); F05D 2220/76 (2013.01);
Abstract

An apparatus and a process for converting a twin spool aero gas turbine engine to an industrial gas turbine engine, where the fan of the aero engine is removed and replaced with an electric generator, a power turbine is added that drives a low pressure compressor that is removed from the aero engine, variable guide vanes are positioned between the high pressure turbine and the power turbine, and a low pressure compressed air line is connected between the outlet of the low pressure compressor and an inlet to the high pressure compressor, where a hot gas flow produced in the combustor first flows through the high pressure turbine, then through the low pressure turbine, and then through the power turbine.


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