17984641. GAS TURBINE COMBUSTION SECTION HAVING AN INTEGRATED FUEL CELL ASSEMBLY simplified abstract (General Electric Company)

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GAS TURBINE COMBUSTION SECTION HAVING AN INTEGRATED FUEL CELL ASSEMBLY

Organization Name

General Electric Company

Inventor(s)

Seung-Hyuck Hong of Clifton Park NY (US)

Richard L. Hart of Broadalbin NY (US)

Honggang Wang of Clifton Park NY (US)

Anil Raj Duggal of Niskayuna NY (US)

Michael Anthony Benjamin of Cincinnati OH (US)

GAS TURBINE COMBUSTION SECTION HAVING AN INTEGRATED FUEL CELL ASSEMBLY - A simplified explanation of the abstract

This abstract first appeared for US patent application 17984641 titled 'GAS TURBINE COMBUSTION SECTION HAVING AN INTEGRATED FUEL CELL ASSEMBLY

Simplified Explanation

The patent application describes a combustion section with a casing that houses a combustion liner, creating a passageway for a fuel cell assembly. The fuel cell assembly includes a fuel cell that processes air and fuel to produce output products for the combustion chamber.

  • The combustion section defines axial, radial, and circumferential directions.
  • The casing contains a diffusion chamber.
  • The combustion liner within the diffusion chamber defines a combustion chamber.
  • A passageway is formed between the combustion liner and the casing.
  • A fuel cell assembly is located in the passageway.
  • The fuel cell extends at an angle between the inlet and outlet ends relative to a radial projection line.

Potential Applications

This technology could be applied in aerospace propulsion systems, power generation, and industrial heating processes.

Problems Solved

This innovation helps improve combustion efficiency, reduces emissions, and enhances overall system performance.

Benefits

The technology offers increased fuel efficiency, lower emissions, and improved energy conversion rates.

Potential Commercial Applications

Potential commercial applications include aircraft engines, power plants, and industrial furnaces.

Possible Prior Art

One possible prior art could be the use of fuel cells in combustion systems for energy generation, but the specific configuration described in the patent application may be novel.

Unanswered Questions

How does the fuel cell assembly affect the overall size and weight of the combustion section?

The article does not provide information on the impact of the fuel cell assembly on the size and weight of the combustion section. This could be crucial for applications where space and weight constraints are significant factors.

What are the potential maintenance requirements for the fuel cell assembly in this configuration?

The article does not address the maintenance needs of the fuel cell assembly within the combustion section. Understanding the maintenance requirements is essential for assessing the long-term viability and cost-effectiveness of this technology.


Original Abstract Submitted

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.