POWER PLANT USING TWO FUELS, INCLUDING ONE FUEL WITH A HIGH GELATION TEMPERATURE
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United States of America Patent
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Issued Date -
Jun 23, 2016
app pub date -
Dec 23, 2014
filing date -
Dec 23, 2014
priority date (Note) -
Abandoned
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Abstract
The present invention relates to a fuel supply device for a heat engine intended for a rotary-wing aircraft, which feed device includes first and second reservoirs respectively containing first and second fuels suitable for feeding the heat engine. The second fuel is heated by passing through a heat exchanger, and then passes through a return valve positioned beyond the heat exchanger. The return valve is driven as a function of the temperature of the second fuel in order to direct the second fuel to the second reservoir when the temperature of the second fuel is lower than or equal to the setpoint temperature Tc, and to the heat engine when the temperature of the second fuel is higher than the setpoint temperature Tc.
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