Invention Publication
- Patent Title: GAS TURBINE COMBUSTION SECTION HAVING AN INTEGRATED FUEL CELL ASSEMBLY
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Application No.: US17984641Application Date: 2022-11-10
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Publication No.: US20240159397A1Publication Date: 2024-05-16
- Inventor: Seung-Hyuck Hong , Richard L. Hart , Honggang Wang , Anil Raj Duggal , Michael Anthony Benjamin
- Applicant: General Electric Company
- Applicant Address: US NY Schenectady
- Assignee: General Electric Company
- Current Assignee: General Electric Company
- Current Assignee Address: US NY Schenectady
- Main IPC: F23R3/00
- IPC: F23R3/00 ; F23R3/28 ; H01M8/04089 ; H01M8/2457

Abstract:
A combustion section defines an axial direction, a radial direction, and a circumferential direction. The combustion section includes a casing that defines a diffusion chamber. A combustion liner is disposed within the diffusion chamber and defines a combustion chamber. The combustion liner is spaced apart from the casing such that a passageway is defined between the combustion liner and the casing. A fuel cell assembly is disposed in the passageway. The fuel cell assembly includes a fuel cell that extends between an inlet end and an outlet end. The inlet end receives a flow of air and fuel and the outlet end provides output products to the combustion chamber. The fuel cell extends at an angle between the inlet end and the outlet end relative to a radial projection line.
Public/Granted literature
- US12078350B2 Gas turbine combustion section having an integrated fuel cell assembly Public/Granted day:2024-09-03
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