Gas turbine engine and fuel cell assembly

Patent metadata

Field	Value
Publication number	US-12584445-B2
Application number	US-202418404322-A
Country	US
Kind code	B2
Filing date	Jan 4, 2024
Priority date	Feb 23, 2023
Publication date	Mar 24, 2026
Grant date	Mar 24, 2026

Abstract

A gas turbine engine is provided. The gas turbine engine includes a turbomachine having a turbomachine having a compressor section, a combustor, and a turbine section arranged in serial flow order, the turbomachine further including an outer casing; and a fuel cell assembly positioned within the outer casing of the turbomachine, the fuel cell assembly including a fuel cell, an inlet line in fluid communication with an inlet of the fuel cell, and an output products line in fluid communication with an outlet of the fuel cell for receiving output products from the fuel cell, wherein the inlet line is positioned to be in thermal communication with the output products during operation of the gas turbine engine.

First claim

We claim:

1 . A gas turbine engine comprising:
a turbomachine having a compressor section, a combustor, a turbine section, and an exhaust section arranged in serial flow order, the exhaust section defining an exhaust gas flowpath through which an exhaust gas flow is directed downstream of the turbine section, the turbomachine further comprising an outer casing; a fuel cell assembly positioned within the outer casing of the turbomachine, the fuel cell assembly comprising a fuel cell, a reformer comprising a first stage and a second stage downstream from the first stage, a fuel line in fluid communication with an anode of the fuel cell, an anode output products line in fluid communication with an anode outlet of the fuel cell and a cathode output products line in fluid communication with a cathode outlet of the fuel cell for receiving output products from the anode and a cathode of the fuel cell, respectively, wherein the second stage of the reformer is configured to reduce a hydrogen gas content of the output products from the anode outlet by reaction with the output products from the cathode outlet, and wherein the fuel line is positioned to be in thermal communication with the output products from the anode and the cathode at the first stage of the reformer to accept heat from the output products from the anode and the cathode during operation of the gas turbine engine, and wherein the cathode includes a cathode inlet positioned to receive at least a portion of the exhaust gas flow, and a recirculation line extending from a location downstream of the reformer to the fuel cell for providing a flow from the reformer to the fuel cell.

2 . The gas turbine engine of claim 1 , wherein the reformer is in fluid communication with the anode output products line and the cathode output products line.

3 . The gas turbine engine of claim 2 , wherein the reformer is configured to vaporize a fuel flow through the fuel line.

4 . The gas turbine engine of claim 2 , wherein the fuel cell assembly comprises a fuel control valve in fluid communication with the fuel line at a location upstream of the reformer.

5 . The gas turbine engine of claim 2 , wherein the second stage of the reformer comprises a reactor configured as a tail gas oxidizer.

6 . The gas turbine engine of claim 1 , wherein the recirculation line extends from the location downstream of the reformer to a cathode inlet line in fluid communication with the cathode of the fuel cell.

7 . A fuel cell assembly for a gas turbine engine, the fuel cell assembly comprising:
a fuel cell defining an anode, an anode inlet, an anode outlet, a cathode, a cathode inlet, and a cathode outlet; an anode inlet line in fluid communication with the anode inlet of the fuel cell; an anode output products line in fluid communication with the anode outlet for receiving output products from the anode, and a cathode output products line in fluid communication with the cathode outlet of the fuel cell for receiving output products from the cathode; and a reformer comprising a first stage and a second stage located downstream of the first stage, wherein the anode inlet line is positioned to be in thermal communication with the anode output products line and the cathode output products line in the first stage of the reformer to accept heat from the output products of the anode and the output products of the cathode during operation of the fuel cell assembly, and wherein the second stage is configured to reduce a hydrogen gas content of the output products from the anode by reaction with the output products of the cathode.

8 . The fuel cell assembly of claim 7 , wherein the anode inlet line is a fuel line, and wherein the fuel cell assembly further comprises:
a fuel control valve in fluid communication with the fuel line at a location upstream of the reformer.

9 . The fuel cell assembly of claim 7 , further comprising:
a recirculation line extending from a location downstream of the reformer to the fuel cell for providing a flow from the reformer to the fuel cell.

Assignees

• Gen Electric

Inventors

• Wang Honggang
• Miller Brandon Wayne
• Benjamin Michael Anthony
• Hart Richard L
• Vondrell Randy M
• St Pierre Ryan

Classifications

• Y02E60/50

  Fuel cells · CPC title

• H01M2008/1293

  Fuel cells with solid oxide electrolytes · CPC title

• H01M8/0618 Primary

  Reforming processes, e.g. autothermal, partial oxidation or steam reforming · CPC title

• H01M8/04014

  Heat exchange using gaseous fluids; Heat exchange by combustion of reactants · CPC title

• H01M8/04097

  with recycling of the reactants (H01M8/04119, H01M8/04104 take precedence) · CPC title