Invention Grant
- Patent Title: Fuel injection assemblies for axial fuel staging in gas turbine combustors
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Application No.: US15838172Application Date: 2017-12-11
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Publication No.: US11187415B2Publication Date: 2021-11-30
- Inventor: Charlie Edmond Jones , James Harper , Matthew Bernard Wilson , Robert Wade Clifford , Yon Han Chong , Benjamin Robert Ryan , Gilbert Otto Kraemer
- Applicant: General Electric Company
- Applicant Address: US NY Schenectady
- Assignee: General Electric Company
- Current Assignee: General Electric Company
- Current Assignee Address: US NY Schenectady
- Agency: Dority & Manning, P.A.
- Main IPC: F23R3/28
- IPC: F23R3/28 ; F23R3/34 ; F23R3/04 ; F23R3/00

Abstract:
An injection assembly for a gas turbine combustor having a liner defining a combustion zone and a secondary combustion zone and a forward casing circumferentially surrounding at least a portion of the liner is provided. The injection assembly includes a thimble assembly and an injector unit. The thimble assembly, which is mounted to the liner, includes a thimble that extends through a thimble aperture in the liner. The injector unit, which is mounted to and extends through the forward casing, includes an injector blade that extends into the thimble. The injection assembly introduces a flow of fuel into a flow of air flowing through the thimble, such that fuel and air are injected into the secondary combustion zone in a direction transverse to a flow of combustion products from the primary combustion zone.
Public/Granted literature
- US20190178497A1 FUEL INJECTION ASSEMBLIES FOR AXIAL FUEL STAGING IN GAS TURBINE COMBUSTORS Public/Granted day:2019-06-13
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