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
31.10.2024
Patent
Elektronische Ressource
Englisch
MULTIPLE HEAT SOURCE CRYOGENIC BOTTOMING CYCLE SEQUENCING AND ROUTING
Europäisches Patentamt | 2024
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Online Contents | 1995
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