An aircraft propulsion system includes at least two gas turbine engines and a bottoming cycle system where a working fluid is circulated within a closed circuit that includes a bottoming compressor section and a bottoming turbine section. Each of the at least two gas turbine engines include a primary heat exchanger for communicating thermal energy into the working fluid of the bottoming cycle.
SHARED CRYOGENIC BOTTOMING CYCLE
2024-10-31
Patent
Electronic Resource
English
MULTIPLE HEAT SOURCE CRYOGENIC BOTTOMING CYCLE SEQUENCING AND ROUTING
European Patent Office | 2024
|Organic Rankine Bottoming Cycle
Automotive engineering | 1976
|Bottoming-Cycle fuer Nutzfahrzeuge
Tema Archive | 1985
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