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:
Mar. 03, 2020

Filed:

Aug. 18, 2015
Applicant:

General Electric Company, Schenectady, NY (US);

Inventor:

Thomas Lee Becker, Jr., Symmes Township, OH (US);

Assignee:

General Electric Company, Schenectady, NY (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02C 6/08 (2006.01); F02C 9/18 (2006.01); F02K 3/075 (2006.01); F02C 3/13 (2006.01); F02C 7/32 (2006.01); F02C 3/04 (2006.01); F02C 7/36 (2006.01);
U.S. Cl.
CPC ...
F02C 9/18 (2013.01); F02C 3/04 (2013.01); F02C 3/13 (2013.01); F02C 6/08 (2013.01); F02C 7/32 (2013.01); F02K 3/075 (2013.01); F02C 7/36 (2013.01); F05D 2220/32 (2013.01); F05D 2220/62 (2013.01); F05D 2270/101 (2013.01);
Abstract

A gas turbine engine is provided having a compressor section, a combustion section, and a turbine section. The compressor section includes one or more compressors and the turbine section includes one or more turbines. The one or more compressors and the one or more turbines are each rotatable about a longitudinal centerline of the gas turbine engine. Additionally, a bleed air flowpath is provided extending between an inlet in airflow communication with the compressor section and an outlet. An auxiliary turbine is positioned in airflow communication with the bleed air flowpath for extracting energy from a flow of bleed air through the bleed air flowpath.


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