A cryogenic fueled aircraft propulsion system comprises a gas turbine engine mounted to a wing by an engine pylon, and configured to receive cryogenic fuel, the gas turbine engine comprising a core compressor. The propulsion system further comprises a pre-heater configured to heat the fuel prior to delivery to the gas turbine engine. The pre-heater is located within the engine pylon, aft of the engine core compressor.
CRYOGENIC FUELLED AIRCRAFT PROPULSION SYSTEM
2025-07-10
Patent
Electronic Resource
English
Rising interest in gas-fuelled propulsion
Tema Archive | 1997
|Development of a liquid nitrogen fuelled cryogenic engine
Tema Archive | 2009
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