Fuel cell system and aircraft having an inerting system
US-2024379984-A1 · Nov 14, 2024 · US
US10490832B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-10490832-B2 |
| Application number | US-201815935649-A |
| Country | US |
| Kind code | B2 |
| Filing date | Mar 26, 2018 |
| Priority date | Oct 31, 2012 |
| Publication date | Nov 26, 2019 |
| Grant date | Nov 26, 2019 |
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Official abstract text for this publication.
A power generation system includes a gas turbine having a compressor, a combustor, and a turbine, an inlet guide vane in an air intake port in the compressor, a first compressed air supply line for supplying compressed air compressed by the compressor to the combustor, a solid oxide fuel cell (SOFC) having an air electrode and a fuel electrode, a second compressed air supply line for supplying at least part of the compressed air compressed by the compressor to the air electrode, a control valve in the second compressed air supply line, and a control device for opening the control valve when the SOFC is activated and changing a degree of opening of the inlet guide vane from a preset reference degree of opening.
Opening claim text (preview).
The invention claimed is: 1. A power generation system, comprising: a gas turbine having a compressor and a combustor; a first compressed air supply line for supplying compressed air compressed by the compressor to the combustor; a fuel cell having an air electrode and a fuel electrode; a second compressed air supply line for supplying at least a portion of the compressed air compressed by the compressor to the air electrode; a first on-off valve provided on the second compressed air supply line; a compressed air supply unit connected to the second compressed air supply line on the fuel cell side from the first on-off valve; and a control unit for closing the first on-off valve and driving the compressed air supply unit upon the fuel cell being activated. 2. The power generation system according to claim 1 , wherein the compressed air supply unit includes a third compressed air supply line connected at one end thereof to the second compressed air supply line on the fuel cell side from the first on-off valve, an activation compressor connected to the other end of the third compressed air supply line, and a second on-off valve provided on the third compressed air supply line, and upon the fuel cell being activated, the control unit closes the first on-off valve, opens the second on-off valve, and drives the activation compressor. 3. The power generation system according to claim 1 , further comprising a first sensor that measures the pressure of the compressed air compressed by the compressor and a second sensor that measures the pressure of the second compressed air supply line on the fuel cell side from the first on-off valve, wherein upon a second pressure measured by the second sensor reaches a first pressure measured by the first sensor, the control unit stops the driving of the compressed air supply unit and opens the first on-off valve.
using a compressor turbine assembly · CPC title
Fuel cells with solid oxide electrolytes · CPC title
having a turbine driving a compressor (power transmission arrangements F02C7/36; control of working fluid flow F02C9/16) · CPC title
with simultaneous supply or evacuation of electrolyte; Humidifying or dehumidifying · CPC title
Combined cycle power plant [CCPP], or combined cycle gas turbine [CCGT] · CPC title
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