A system for an aircraft is provided. The system includes a compressing device and at least one heat exchanger. The compressing device includes a compressor, a turbine downstream of the compressor, and an electric motor coupled to the turbine and the compressor. Further, the compressor includes a high rotor backsweep. The system can be an air conditioning system.
ENVIRONMENTAL CONTROL SYSTEM UTILIZING ENHANCED COMPRESSOR
2017-10-26
Patent
Elektronische Ressource
Englisch
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