View source for 20250215828. I (Rolls-Royce North American Technologies .)

= INTEGRATED POWER AND COOLING SYSTEM =

'''Abstract''':
a system includes a hydrogen fuel delivery system for an engine that pumps hydrogen from a tank in a liquid state and an evaporator configured to convert at least some of the hydrogen to a gaseous state. the system includes a heat source thermally coupled with the system and fluidly uncoupled from the system. the system is configured to supply the hydrogen to the engine for combustion and cool the heat source using the hydrogen. the system further includes a coolant loop that circulates coolant between the heat source and the evaporator. the coolant loops includes a valve that splits the coolant flowing from the evaporator into a first portion that flows to a heater and a second portion that flows to the heat source. the first and second portions are directed to the evaporator after having passed through the heater and the heat source.

'''Inventor(s)''': [[:Category:Patrick Gore of Indianapolis IN US|Patrick Gore]]

'''CPC Classification''': [[:Category:CPC_F02C7/18|F02C7/18]] (GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS  (construction of turbines ; jet-propulsion plants ; construction of compressors or fans ; generating combustion products of high pressure or high velocity ; using gas turbines in compression refrigeration plants ))


[[Category:Patent Applications]]
[[Category:Rolls-Royce North American Technologies Inc.]]
[[Category:CPC_F02C7/18]]
[[Category:Patrick Gore of Indianapolis IN US]]

[https://wikipatents.org/index.php?search=20250215828+rejection&title=Special%3ASearch&wprov=acrw1_-1 Search for rejections for patent application number 20250215828]


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