An aircraft propulsion system includes a core engine, a first bottoming cycle and a second bottoming cycle that utilize different working fluids having different critical temperatures such that each of the bottoming cycles have different heat absorption capabilities.
STACKED CRYOGENIC BOTTOMING CYCLES
2024-10-31
Patent
Electronic Resource
English
MULTIPLE HEAT SOURCE CRYOGENIC BOTTOMING CYCLE SEQUENCING AND ROUTING
European Patent Office | 2024
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