Fuel cell system and aircraft having an inerting system
US-2024379984-A1 · Nov 14, 2024 · US
US9979033B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-9979033-B2 |
| Application number | US-201314436666-A |
| Country | US |
| Kind code | B2 |
| Filing date | Oct 28, 2013 |
| Priority date | Oct 31, 2012 |
| Publication date | May 22, 2018 |
| Grant date | May 22, 2018 |
A practical reading order for non-experts. Skip the full description unless you need deep technical detail.
What the patent document calls the invention.
A short plain-language summary of the technical disclosure.
Who owns or filed the patent and who is credited as inventor.
Filing, priority, publication, and grant dates set the timeline.
The legal scope of protection — read this for what is actually claimed.
Technology tags used to group this patent with similar filings.
Prior art links and similar publications in this corpus.
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 fuel cell; a gas turbine having a compressor and a combustor; an inlet guide vane on an air intake port of the compressor; a first compressed air supply line for supplying compressed air compressed by the compressor to the combustor; a second compressed air supply line for supplying at least a portion of the compressed air compressed by the compressor to the fuel cell; a compressed air circulation line that fluidically connects between the fuel cell and the combustor to supply an exhaust air from the fuel cell to the combustor; an on-off valve on the second compressed air supply line; and a control unit for opening the on-off valve and controlling a degree of opening of the inlet guide vane, wherein the control unit is configured to control the inlet guide vane so as to make the degree of opening of the inlet guide vane equal to a preset reference degree of opening of the inlet guide vane in accordance with an operating state of the gas turbine when the gas turbine is activated, to increase the degree of opening of the inlet guide vane from the preset reference degree of opening of the inlet guide vane to a predetermined degree of opening of the inlet guide vane that is greater than a degree of opening of the inlet guide vane during steady-state operation of the gas turbine when the fuel cell is activated, to reduce the degree of opening of the inlet guide vane to the preset reference degree of opening of the inlet guide vane when a second pressure which is a pressure of the second compressed air supply line approaches a first pressure which is an outlet pressure of the compressor, and to make the degree of opening of the inlet guide vane equal to the preset reference degree of opening of the inlet guide vane when the second pressure reaches the first pressure. 2. The power generation system according to claim 1 , wherein the on-off valve is a control valve that can adjust a flow rate, and upon the fuel cell being activated, the control unit opens the on-off valve to an initial degree of opening that is smaller than a fully opened state. 3. The power generation system according to claim 1 , wherein the on-off valve includes, in parallel, a first on-off valve that passes a first flow rate upon being open and a second on-off valve that passes a second flow rate upon being open, and upon the fuel cell being activated, the control unit closes the first on-off valve and opens the second on-off valve, wherein the first flow rate is larger than the second flow rate. 4. The power generation system according to claim 1 , further comprising a first sensor that measures the first pressure, and a second sensor that measures the second pressure on a fuel cell side from the on-off valve, wherein, upon the second pressure reaching the first pressure, the control unit increases a degree of opening of the on-off valve.
of cathode reactants at the inlet or inside the fuel cell · CPC title
Combined cycle power plant [CCPP], or combined cycle gas turbine [CCGT] · CPC title
Pressure; Ambient pressure; Flow · CPC title
having a turbine driving a compressor (power transmission arrangements F02C7/36; control of working fluid flow F02C9/16) · CPC title
using a compressor turbine assembly · CPC title
Related publications grouped by family.
Answers are generated from the same data shown on this page.