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. 16, 2020

Filed:

May. 10, 2016
Applicant:

General Electric Company, Schenectady, NY (US);

Inventors:

Daniel Waslo, Marblehead, MA (US);

Michael Richardson-Bach, Marblehead, MA (US);

Assignee:

General Electric Company, Schenectady, NY (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02C 9/18 (2006.01); F01D 5/04 (2006.01); F02C 3/08 (2006.01); F02C 3/05 (2006.01); F02C 6/08 (2006.01); F01D 5/02 (2006.01); F01D 9/04 (2006.01); F01D 25/12 (2006.01); F02C 3/04 (2006.01);
U.S. Cl.
CPC ...
F02C 9/18 (2013.01); F01D 5/02 (2013.01); F01D 5/04 (2013.01); F01D 9/04 (2013.01); F01D 25/12 (2013.01); F02C 3/04 (2013.01); F02C 3/05 (2013.01); F02C 3/08 (2013.01); F02C 6/08 (2013.01); F05D 2220/32 (2013.01); F05D 2240/127 (2013.01); F05D 2260/20 (2013.01); F05D 2260/209 (2013.01); Y02T 50/676 (2013.01);
Abstract

The present disclosure is directed to a system for bleeding air from a compressed gas path of a gas turbine engine. The system includes an impeller positioned at a downstream end of a compressor in the gas turbine engine. The impeller includes an impeller hub, an impeller arm coupled to the impeller hub, and a plurality of circumferentially spaced apart impeller vanes extending radially outwardly from the impeller arm. The impeller arm defines an impeller arm aperture extending therethrough. A vortex spoiler is positioned radially inwardly from the impeller arm and defines a vortex spoiler passage extending radially therethrough. Bleed air flows from the compressed gas path radially inwardly through both the impeller arm aperture and the vortex spoiler passage.


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