| 摘要 |
An apparatus for supplying inlet gas 29 and fuel 17 to a gas turbine engine 10 , the apparatus comprising: a heat exchanger 28 for transferring thermal energy from the inlet gas 29 to a fuel 17 for the gas turbine engine 10 , the heat exchanger 28 comprising a first input for receiving fuel 17 , a second input for receiving inlet gas 29 , a first output for providing inlet gas 31 after heat exchange to the gas turbine engine 10 and a second output for providing fuel 33 after heat exchange to the gas turbine engine 10.
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