An environmental control system of an aircraft includes a plurality of inlets (22, 24, 28) for receiving a plurality of mediums including a first medium (A1), a second medium (A2), and a third medium (A3) and an outlet for delivering a conditioned flow of the second medium to one or more loads of the aircraft. A ram air circuit (30) includes a ram air shell (32) having at least one heat exchanger positioned therein. At least one compressing device (40) is arranged in fluid communication with the ram air circuit and the outlet. The at least one compressing device includes at least one compressor (42) and at least one turbine (44) operably coupled via a shaft. A heat exchanger (34) is arranged in fluid communication with the at least one compressing device. The second medium output from the at least one compressing device is cooled by the third medium. The second medium is fresh air.
AIRCRAFT ENVIRONMENTAL CONTROL SYSTEM
FLUGZEUGKLIMAREGELUNGSSYSTEM
SYSTÈME DE RÉGLAGE ENVIRONNEMENTAL D'UN AÉRONEF
2024-01-31
Patent
Electronic Resource
English
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |