Gas turbine combustion section having an integrated fuel cell assembly
Number of patents in Portfolio can not be more than 2000
United States of America
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Mar 4, 2025
Grant Date -
May 16, 2024
app pub date -
Nov 10, 2022
filing date -
Nov 10, 2022
priority date (Note) -
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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 stack that has a plurality of fuel cells each extending 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 assembly further includes an electrical circuit that is electrically coupled to the plurality of fuel cells and that extends through the casing.
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