A method of operating an environmental control system of an aircraft includes providing a first medium to the environmental control system including a compressor and a turbine. The first medium is provided to the compressor and the turbine sequentially. A second medium is provided to the environmental control system. In a first mode of operation, the first medium and the second medium mix within the turbine and in a second mode of operation the second medium bypasses the turbine such that the first medium and the second medium mix downstream from the turbine.
SHOESTRING ENVIRONMENTAL CONTROL SYSTEM FOR AN AIRCRAFT
2021-11-18
Patent
Electronic Resource
English
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
ENVIRONMENTAL CONTROL SYSTEM UTILIZING SHOESTRING CYCLE TO MAXIMIZE EFFICIENCY
European Patent Office | 2015
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