An air conditioning system for an aircraft is provided. The air conditioning system includes a first rotating component and a second rotating component. The first rotating component includes a compressor and a turbine. The compressor pressurizes a first medium. The first turbine receives a mixture of a second medium and a pressurized form of the first medium. The second rotating component includes a fan.
MIXING BLEED AND RAM AIR AT A TURBINE INLET OF A COMPRESSING DEVICE
MELANGE D'AIR DE PRELEVEMENT ET D'AIR DYNAMIQUE A L'ENTREE D'UNE TURBINE D'UN APPAREIL COMPRESSEUR
2017-11-26
Patent
Elektronische Ressource
Englisch
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