An environmental control system (12) for an aircraft according to an example of the present disclosure includes a first turbine (T1) coupled to an engine (10) and a second turbine (T2) coupled to a compressor (C). One or more ducts (16) are configured to provide bleed air from the engine to the first and second turbines and the compressor such that the first and second turbines and the compressor condition the bleed air. A method of conditioning air is also disclosed.
TWO-TURBINE ENVIRONMENTAL CONTROL SYSTEM
ZWEITURBINEN-UMWELTKONTROLLSYSTEM
SYSTÈME DE COMMANDE ENVIRONNEMENTAL DOTÉ DE DEUX TURBINES
2023-06-14
Patent
Elektronische Ressource
Englisch
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
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