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
31.10.2024
Patent
Elektronische Ressource
Englisch
MULTIPLE HEAT SOURCE CRYOGENIC BOTTOMING CYCLE SEQUENCING AND ROUTING
Europäisches Patentamt | 2024
|Organic Rankine Bottoming Cycle
Kraftfahrwesen | 1976
|Bottoming-Cycle fuer Nutzfahrzeuge
Tema Archiv | 1985
|