A conditioning system for an aircraft including a fuel conduit which receives a liquid fuel, an evaporator and a heater which heat the liquid fuel to convert the fuel to a gas fuel supplied to an engine on the aircraft, the evaporator transfers heat from a hot working fluid to the liquid fuel and the heater converts energy into heat applied to the liquid fuel, and a heat recovery circuit which circulates the working fluid through the evaporator and a heat exchanger in a hot exhaust gas stream generated by the engine.
FUEL CONDITIONING SYSTEM
2024-07-04
Patent
Electronic Resource
English
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