An environmental control system (20) of an aircraft includes a ram air circuit (30) including a ram air shell (32) having at least one heat exchanger positioned therein. A dehumidification system (42) is arranged in fluid communication with the ram air circuit (30) and at least one compressing device (60) is arranged in fluid communication with the ram air circuit (30) and the dehumidification system (42). The at least one compressing device (60) includes a turbine (64) and a compressor (62) operably coupled via a shaft (68). A fan is operably coupled to the ram air circuit (30). At least one compressing device (60) is arranged non-linearly with the ram air circuit (30) such that an axis of rotation of the fan is offset from the axis of the shaft (68).
ADVANCED ENVIRONMENTAL CONTROL SYSTEM IN AN INTEGRATED SPLIT PACK ARRANGEMENT WITH ONE BLEED/OUTFLOW HEAT EXCHANGER
FORTSCHRITTLICHES UMWELTKONTROLLSYSTEM IN EINER INTEGRIERTEN GETEILTEN ANORDNUNG MIT EINEM ZAPFLUFT WÄRMEÜBERTRAGER
SYSTÈME AVANCÉ DE COMMANDE ENVIRONNEMENTAL
2021-03-10
Patent
Electronic Resource
English
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
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