An environmental control system includes a cooling circuit (30) having at least one heat exchanger (32, 34) for cooling a first medium therein. At least one compressing device is operably coupled to the cooling circuit. The at least one compressing device includes a first compressor (42a) and a second compressor (42b), wherein the first medium is provided to the first compressor and the second compressor in series, and a temperature of the first medium provided to an inlet of the second compressor is less than the temperature of the first medium at an outlet of the first compressor.
ENVIRONMENTAL CONTROL SYSTEM FOR SUPERSONIC COMMERCIAL AIRCRAFT
KLIMATISIERUNGSANLAGE FÜR ÜBERSCHALLVERKEHRSFLUGZEUGE
SYSTÈME DE CLIMATISATION POUR AVION COMMERCIAL SUPERSONIQUE
2022-07-20
Patent
Electronic Resource
English
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
ENVIRONMENTAL CONTROL SYSTEM FOR SUPERSONIC COMMERCIAL AIRCRAFT
European Patent Office | 2022
|Environmental control system considerations for supersonic cruising aircraft
Engineering Index Backfile | 1965
|Environmental Control System Considerations for Supersonic Cruising Aircraft
SAE Technical Papers | 1965
|Control and flight characteristics of commercial supersonic transport aircraft
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|Control and Flight Characteristics of Commercial Supersonic Transport Aircraft
SAE Technical Papers | 1964
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