An environmental control system of an aircraft includes a plurality of inlets (24, 28) for receiving a plurality of mediums including a first medium (A1) and a second medium (A2) 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 (34, 36) positioned therein. A compressing device is arranged in fluid communication with the ram air circuit and the outlet. The compressing device including a first compressor (40a), a second compressor (40b), and at least one turbine (44a) operably coupled via a shaft (46). The first compressor and the second compressor are arranged in parallel with respect to a flow of the second medium and the first medium is used as a heat sink by another component within the environmental control system.
AIRCRAFT ENVIRONMENTAL CONTROL SYSTEM
FLUGZEUGKLIMAREGELUNGSSYSTEM
SYSTÈME DE RÉGLAGE ENVIRONNEMENTAL D'UN AÉRONEF
2022-02-02
Patent
Elektronische Ressource
Englisch
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |