Fuel conditioning system and method configured to supply an aircraft turbine engine with fuel from a cryogenic tank
US-12162621-B2 · Dec 10, 2024 · US
US9482159B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-9482159-B2 |
| Application number | US-201414183470-A |
| Country | US |
| Kind code | B2 |
| Filing date | Feb 18, 2014 |
| Priority date | Feb 20, 2013 |
| Publication date | Nov 1, 2016 |
| Grant date | Nov 1, 2016 |
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A power generation system has a fuel cell, a gas turbine, an exhausted oxidant line, a fuel gas supply line, an exhausted fuel gas supply line, a supply amount adjustment unit, and a control system including an information acquisition unit, a calculation unit, and a fuel gas supply control unit. The information acquisition unit acquires an output command of the gas turbine, an atmospheric temperature, a temperature of the exhausted oxidant supplied to the gas turbine, and a temperature of the exhausted fuel gas supplied to the gas turbine. The calculation unit calculates a heat input of the exhausted oxidant, calculates a heat input of the exhausted fuel gas, and calculates by the output command and the atmospheric temperature to calculate a gas turbine heat input command.
Opening claim text (preview).
The invention claimed is: 1. A power generation system comprising: a fuel cell; a gas turbine including a combustor; an exhausted oxidant line that supplies exhausted oxidant from the fuel cell to the combustor; a fuel gas supply line that supplies fuel gas to the combustor; an exhausted fuel gas supply line that directly supplies exhausted fuel gas from the fuel cell to the combustor; a supply amount adjustment unit that adjust an amount of the fuel gas supplied from th…
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