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. 26, 2009

Filed:

Dec. 07, 2005
Applicants:

Christopher E. Wolfe, Niskayuna, NY (US);

Douglas F. Beadie, Greer, SC (US);

Kenneth N. Whaling, Simpsonville, SC (US);

David W. Ball, Easley, SC (US);

Kevin T. Mcgovern, Simpsonville, SC (US);

Ravi Praveen Eluripati, Greenville, SC (US);

Omprakash Samudrala, Clifton, NY (US);

Inventors:

Christopher E. Wolfe, Niskayuna, NY (US);

Douglas F. Beadie, Greer, SC (US);

Kenneth N. Whaling, Simpsonville, SC (US);

David W. Ball, Easley, SC (US);

Kevin T. McGovern, Simpsonville, SC (US);

Ravi Praveen Eluripati, Greenville, SC (US);

Omprakash Samudrala, Clifton, NY (US);

Assignee:

General Electric Company, Schenectady, NY (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F02C 6/08 (2006.01); F02C 6/04 (2006.01); F02C 7/12 (2006.01);
U.S. Cl.
CPC ...
Abstract

A gas turbine engine system. The system includes a compressor with a first compressor stage and a second compressor stage, a turbine with a first turbine stage and a second turbine stage, a first flow path connecting the first compressor stage and the first turbine stage, a second flow path connecting the second compressor stage and the second turbine stage, a crossover flow path connecting the first flow path and the second flow path, and an ejector positioned about the crossover flow path and the first flow path. The ejector may be a variable motive nozzle ejector.


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