Gas turbine combustion section having an integrated fuel cell assembly

Patent metadata

Field	Value
Publication number	US-12240613-B2
Application number	US-202217984699-A
Country	US
Kind code	B2
Filing date	Nov 10, 2022
Priority date	Nov 10, 2022
Publication date	Mar 4, 2025
Grant date	Mar 4, 2025

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.

First claim

We claim:

1. A combustion section defining an axial direction, a radial direction, and a circumferential direction, the combustion section comprising:
a casing defining a diffusion chamber;
a combustion liner disposed within the diffusion chamber and defining a combustion chamber, the combustion liner spaced apart from the casing such that a passageway is defined between the combustion liner and the casing; and
a fuel cell assembly disposed in the passageway, the fuel cell assembly comprising a fuel cell stack having a plurality of fuel cells each extending between an inlet end and an outlet end, wherein 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 comprising an electrical circuit electrically coupled to the plurality of fuel cells and extending through the casing, wherein the electrical circuit includes an electrically conducting member disposed at one of a forward end or an aft end of the fuel cell stack, and wherein the electrically conducting member is a first electrically conducting member disposed at one of the forward end or the aft end of the fuel cell stack, and wherein the fuel cell assembly further comprises a second electrically conducting member at the other of the forward end or the aft end of the fuel cell stack.

2. The combustion section as in claim 1 , wherein the fuel cell assembly further comprises at least one structural member that couples the fuel cell assembly to at least one of the casing or the combustion liner of the combustion section.

3. The combustion section as in claim 2 , wherein the at least one structural member is electrically insulating.

4. The combustion section as in claim 1 , wherein the electrical circuit further comprises a strap electrically coupled to the electrically conducting member.

5. The combustion section as in claim 4 , wherein the strap is rigid and welded to the electrically conducting member.

6. The combustion section as in claim 4 , wherein the strap extends from the electrically conducting member and through the casing.

7. The combustion section as in claim 6 , wherein an electric bus electrically couples to the strap outside of the casing.

8. The combustion section as in claim 1 , wherein the combustion liner is electrically insulating.

9. A turbomachine comprising:
a compressor section, a combustion section, and a turbine section arranged in serial flow order, the combustion section comprising:
a casing defining a diffusion chamber;
a combustion liner disposed within the diffusion chamber and defining a combustion chamber, the combustion liner spaced apart from the casing such that a passageway is defined between the combustion liner and the casing; and
a fuel cell assembly disposed in the passageway, the fuel cell assembly comprising a fuel cell stack having a plurality of fuel cells each extending between an inlet end and an outlet end, wherein 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 comprising an electrical circuit electrically coupled to the plurality of fuel cells and extending through the casing, wherein the electrical circuit includes an electrically conducting member disposed at one of a forward end or an aft end of the fuel cell stack, and wherein the electrically conducting member is a first electrically conducting member disposed at one of the forward end or the aft end of the fuel cell stack, and wherein the fuel cell assembly further comprises a second electrically conducting member at the other of the forward end or the aft end of the fuel cell stack.

10. The turbomachine as in claim 9 , wherein the fuel cell assembly further comprises at least one structural member that couples the fuel cell assembly to at least one of the casing or the combustion liner of the combustion section.

11. The turbomachine as in claim 10 , wherein the at least one structural member is electrically insulating.

12. The turbomachine as in claim 9 , wherein the electrical circuit further comprises a strap electrically coupled to the electrically conducting member.

13. The turbomachine as in claim 12 , wherein the strap is rigid and welded to the electrically conducting member.

14. The turbomachine as in claim 12 , wherein the strap extends from the electrically conducting member and through the casing.

15. The turbomachine as in claim 14 , wherein an electric bus electrically couples to the strap outside of the casing.

16. The turbomachine as in claim 9 , wherein the combustion liner is electrically insulating.

Assignees

• Gen Electric

Inventors

• Hong Seung-Hyuck
• Hart Richard L
• Wang Honggang
• Duggal Anil Raj
• Benjamin Michael Anthony

Classifications

• B64D2041/005

  Fuel cells · CPC title

• B64D27/355

  using fuel cells · CPC title

• F23R3/002 Primary

  Wall structures (F23R3/02 and F23R3/007 take precedence) · CPC title

• H01M2250/20

  Fuel cells in motive systems, e.g. vehicle, ship, plane · CPC title

• H01M8/04111

  using a compressor turbine assembly · CPC title