An airplane is provided. The airplane includes a pack. The pack includes a shaft (222), a compressor (210), a turbine (220) coupled to the compressor via the shaft; and a heat exchanger (250). The compressor receives and compresses a first medium in accordance with power provided by the turbine via the shaft. The turbine receives and expands a second medium to provide the power to the compressor via the shaft. The heat exchanger is configured to cool the first medium.
HYBRID THIRD AIR CONDITION PACK
DRITTE HYBRIDKLIMAANLAGE
TROISIÈME PACK D'AIR CONDITIONNÉ HYBRIDE
2021-10-20
Patent
Electronic Resource
English
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
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