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. 31, 2019

Filed:

Apr. 06, 2016
Applicant:

General Electric Company, Schenectady, NY (US);

Inventors:

Brad Wilson VanTassel, Easley, SC (US);

Peter Paul Pirolla, Greer, SC (US);

Assignee:

General Electric Company, Schenectady, NY (US);

Attorneys:
Primary Examiner:
Int. Cl.
CPC ...
F02C 9/18 (2006.01); F01D 25/24 (2006.01); F02C 3/04 (2006.01); F02C 7/18 (2006.01); F02C 9/16 (2006.01); F01D 5/08 (2006.01); F01D 5/18 (2006.01); F01D 9/06 (2006.01); F02K 3/02 (2006.01); F02C 6/08 (2006.01);
U.S. Cl.
CPC ...
F02C 9/18 (2013.01); F01D 5/08 (2013.01); F01D 5/187 (2013.01); F01D 9/065 (2013.01); F01D 25/24 (2013.01); F01D 25/246 (2013.01); F02C 3/04 (2013.01); F02C 6/08 (2013.01); F02C 7/18 (2013.01); F02C 9/16 (2013.01); F02K 3/02 (2013.01); F05D 2220/32 (2013.01); F05D 2250/71 (2013.01); F05D 2260/231 (2013.01); F05D 2260/606 (2013.01); F05D 2260/96 (2013.01); Y02T 50/676 (2013.01);
Abstract

An air bypass system for a gas turbine engine includes a nozzle for a gas turbine engine. The air bypass system includes the nozzle having an inner band, an outer band, and an airfoil extending between the inner band and the outer band. The airfoil defines an internal passage. A diaphragm includes an inner wall, a first rail, and a second rail, which collectively define a diaphragm cavity. The first rail defines a first rail aperture. A manifold is positioned in the diaphragm cavity. The manifold and the diaphragm collectively define a manifold chamber in fluid communication with the first rail aperture. A tube extends through the internal passage defined by the airfoil and into the diaphragm cavity. The tube is in fluid communication with the manifold chamber. Compressed air flows through the tube into the manifold chamber and exits the chamber through the first rail aperture.


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