Fuel cell system and aircraft having an inerting system
US-2024379984-A1 · Nov 14, 2024 · US
US10355292B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-10355292-B2 |
| Application number | US-201715638370-A |
| Country | US |
| Kind code | B2 |
| Filing date | Jun 30, 2017 |
| Priority date | Jul 28, 2016 |
| Publication date | Jul 16, 2019 |
| Grant date | Jul 16, 2019 |
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A method of controlling a fuel cell system includes supplying a fuel gas from a fuel-gas storage container to a fuel cell via a drive valve provided in a fuel-gas path. A first pressure is detected in the fuel-gas path between a first decompression mechanism and a second decompression mechanism. A second pressure is detected in the fuel-gas path between the second decompression mechanism and the drive valve. An on-off valve is opened. The on-off valve is provided in a bypass path. The first pressure and the second pressure are compared after the on-off valve has been opened. The fuel cell system is controlled to decrease electric power generated by the fuel cell or to stop generating electric power in the fuel cell when the first pressure is not substantially equal to the second pressure.
Opening claim text (preview).
What is claimed is: 1. A method of controlling a fuel cell system that includes a fuel cell, comprising: supplying an oxidant gas to a cathode electrode of the fuel cell; supplying a fuel gas from a fuel-gas storage container to an anode electrode of the fuel cell via a drive valve provided in a fuel-gas path to generate electric power in the fuel cell via an electrochemical reaction between the fuel gas and the oxidant gas; detecting a first pressure in the fuel-gas path between a first decompression mechanism and a second decompression mechanism, the first decompression mechanism being provided in the fuel-gas path between the drive valve and the fuel-gas storage container, the second decompression mechanism being provided in the fuel-gas path between the first decompression mechanism and the drive valve; detecting a second pressure in the fuel-gas path between the second decompression mechanism and the drive valve; opening an on-off valve provided in a bypass path that bypasses the second decompression mechanism; comparing the first pressure and the second pressure after the on-off valve has been opened; and controlling the fuel cell system to decrease the electric power generated by the fuel cell as the first pressure is not substantially equal to the second pressure and to stop generating the electric power in the fuel cell as the first pressure is substantially equal to the second pressure. 2. The method according to claim 1 , wherein the on-off valve is opened as the first pressure reaches an upper limit. 3. The method according to claim 1 , wherein the first pressure and the second pressure are compared as a certain period of time has passed after the on-off valve has been opened. 4. The method according to claim 1 , wherein as the fuel cell system is controlled to stop generating the electric power in the fuel cell, the drive valve that is disposed downstream the fuel-gas storage container in the fuel-gas path is closed, and supply of the fuel-gas to the fuel cell is stopped. 5. The method according to claim 1 , wherein during generating of the electric power by the fuel cell, the fuel cell system is controlled to decrease the electric power generated by the fuel cell as the second pressure is out of a pressure range adjustable by the first decompression mechanism. 6. The method according to claim 1 , wherein the fuel cell is mounted on a vehicle body together with a sound generation mechanism, and as an output of the fuel cell is equal to or lower than a threshold, the on-off valve is opened during a period as the sound generation mechanism is generating a sound. 7. The method according to claim 1 , further comprising: closing the on-off valve as the first pressure is substantially equal to the second pressure; and detecting the second pressure after the on-off valve has been closed or as an accumulated power generation amount of the fuel cell reaches a value, wherein as the first pressure is within a pressure range adjustable by the first decompression mechanism, and the second pressure is out of a pressure range adjustable by the second decompression mechanism, the fuel cell system is controlled to decrease the electric power or to stop generating the electric power. 8. The method according to claim 7 , wherein the second pressure is detected as a certain period of time has passed after the on-off valve has been closed or as the accumulated power generation amount of the fuel cell reaches the value.
of fuel cell stacks · CPC title
Pressure differences, e.g. between anode and cathode · CPC title
of auxiliary devices, e.g. batteries, capacitors · CPC title
by purging or increasing flow or pressure of reactants · CPC title
of anode reactants at the inlet or inside the fuel cell · CPC title
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