Patent ID: 11859549
Assignee: BAE SYSTEMS PLC
Field: Engines, pumps, turbines (Mechanical engineering)
Classification: CPC F  Y | IPC F

Claim 19:
20. The thermodynamic apparatus of claim 19, wherein:
the first heat exchanger is provided in flow series between the compressor module inlet and the first rotor, and the first rotor is provided in flow series between the first heat exchanger and the compressor module outlet;
the first heat exchanger is configured to transfer heat to a first heat transfer unit from working fluid passing the first heat exchanger;
the second heat exchanger is provided in flow series between the turbine module inlet and the second rotor, and the second rotor is provided in flow series between the second heat exchanger and the turbine module outlet; and
the second heat exchanger is configured to transfer heat received from a second heat transfer unit to working fluid passing the second heat exchanger.