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:
Jul. 15, 2025

Filed:

Feb. 15, 2024
Applicant:

General Electric Company, Schenectady, NY (US);

Inventors:

Timothy Deryck Stone, Liberty Township, OH (US);

Gregory Michael Laskowski, Rowley, MA (US);

Robert Proctor, West Chester, OH (US);

Curtis Stover, Mason, OH (US);

Robert Francis Manning, Newburyport, MA (US);

Victor Hugo Silva Correia, Milton Mills, NH (US);

Jared Peter Buhler, Tewksbury, MA (US);

Robert Carl Murray, Rotterdam, NY (US);

Corey Bourassa, Mechanicville, NY (US);

Byron Andrew Pritchard, Jr., Loveland, OH (US);

Jonathan Russell Ratzlaff, Loveland, OH (US);

Assignee:

General Electric Company, Evendale, OH (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B01D 45/16 (2006.01); B04C 3/06 (2006.01); F01D 5/18 (2006.01); F01D 9/06 (2006.01); F02C 6/08 (2006.01); F02C 7/052 (2006.01); F02C 7/18 (2006.01); B04C 3/00 (2006.01); F02K 3/04 (2006.01);
U.S. Cl.
CPC ...
B01D 45/16 (2013.01); B04C 3/06 (2013.01); F01D 5/189 (2013.01); F01D 9/065 (2013.01); F02C 6/08 (2013.01); F02C 7/052 (2013.01); F02C 7/18 (2013.01); B04C 2003/003 (2013.01); B04C 2003/006 (2013.01); F02K 3/04 (2013.01); F05D 2260/607 (2013.01); Y02T 50/60 (2013.01);
Abstract

A turbine engine having a compressor section, a combustor section, a turbine section, and a rotatable drive shaft. A bypass conduit couples the compressor section to the turbine section. At least one centrifugal separator is fluidly coupled to the bypass stream, where the at least one centrifugal separator includes a body, a center body, a separator inlet, and a separator outlet fluidly coupled with the turbine section to output a reduced-particle stream that is provided to the turbine section for cooling. The centrifugal separator includes an angular velocity increaser, a flow splitter, a first outlet passage defined by an inner annular wall that receives the reduced-particle stream, and an angular velocity decreaser located downstream of the flow splitter. A second outlet passage receives the concentrated-particle stream.


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