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
2019-03-19
Patent
Elektronische Ressource
Englisch
IPC: | F01D Strömungsmaschinen [Kraft- und Arbeitsmaschinen oder Kraftmaschinen], z.B. Dampfturbinen , NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F04D Strömungsarbeitsmaschinen , NON-POSITIVE-DISPLACEMENT PUMPS |
MIXING BLEED AND RAM AIR AT A TURBINE INLET OF A COMPRESSING DEVICE
Europäisches Patentamt | 2023
|MIXING BLEED AND RAM AIR AT A TURBINE INLET OF A COMPRESSING DEVICE
Europäisches Patentamt | 2017
|MIXING BLEED AND RAM AIR AT A TURBINE INLET OF A COMPRESSING DEVICE
Europäisches Patentamt | 2017
|