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

Claim 6:
7. The thermodynamic apparatus of claim 6, wherein:
the first sub-passage extends through the first heat exchanger, and the first heat exchanger is in flow series between a first inlet to the first sub-passage and a first outlet from the first sub-passage, the first inlet configured to receive the first heat transfer medium from the inlet plenum of the compressor module, and the first outlet being configured to exhaust into the outlet plenum of the compressor module; and
the second sub-passage extends through the second heat exchanger, and the second heat exchanger is in flow series between a second inlet to the second sub-passage and a second outlet from the second sub-passage, the second inlet configured to receive the second heat transfer medium from the inlet plenum of the turbine module, and the second outlet being configured to exhaust into the outlet plenum of the turbine module.