Gas turbine combustion section having an integrated fuel cell assembly
Patent
·
OSTI ID:2541929
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 stack having a plurality of fuel cells each extending between an inlet end and an outlet end. Each fuel cell of the plurality of fuel cells includes an air channel and a fuel channel each fluidly coupled to the combustion chamber.
- Research Organization:
- General Electric Company, Schenectady, NY (United States)
- Sponsoring Organization:
- USDOE Advanced Research Projects Agency - Energy (ARPA-E)
- DOE Contract Number:
- AR0001344
- Assignee:
- General Electric Company (Schenectady, NY)
- Patent Number(s):
- 11,923,586
- Application Number:
- 17/984,721
- OSTI ID:
- 2541929
- Country of Publication:
- United States
- Language:
- English
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