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. 19, 2019

Filed:

Oct. 07, 2016
Applicant:

General Electric Company, Schenectady, NY (US);

Inventors:

Thomas Ory Moniz, Loveland, OH (US);

Joseph George Rose, Mason, OH (US);

Patrick Sean Sage, West Chester, OH (US);

Jeffrey Donald Clements, Mason, OH (US);

Jeffrey Glover, Cincinnati, OH (US);

Assignee:

General Electric Company, Schenectady, NY (US);

Attorneys:
Primary Examiner:
Int. Cl.
CPC ...
F02C 9/18 (2006.01); F04D 27/02 (2006.01); F02C 7/20 (2006.01); F01D 9/02 (2006.01); F01D 25/24 (2006.01); F02C 3/04 (2006.01); F04D 27/00 (2006.01); F04D 29/52 (2006.01); F02C 6/08 (2006.01); F04D 15/00 (2006.01); F01D 25/16 (2006.01);
U.S. Cl.
CPC ...
F02C 9/18 (2013.01); F01D 9/02 (2013.01); F01D 25/24 (2013.01); F02C 3/04 (2013.01); F02C 6/08 (2013.01); F02C 7/20 (2013.01); F04D 27/009 (2013.01); F04D 27/023 (2013.01); F04D 27/0215 (2013.01); F04D 29/522 (2013.01); F01D 25/162 (2013.01); F04D 15/0011 (2013.01); F05D 2220/32 (2013.01); F05D 2240/14 (2013.01); F05D 2240/35 (2013.01); F05D 2240/40 (2013.01); F05D 2260/606 (2013.01);
Abstract

A gas turbine engine includes a first compressor, a casing surrounding the first compressor, and a liner extending forward from the first compressor. The gas turbine engine also includes a core turbine frame assembly extending between the liner and the casing and a bleed air assembly. The bleed air assembly includes a bleed valve positioned in the liner, and a duct in airflow communication with the bleed valve and defining in outlet. The duct is positioned within the core turbine frame assembly and extends to the casing.


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