TWO-TURBINE ENVIRONMENTAL CONTROL SYSTEM

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 firs...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser: PESS, Matthew, RETERSDORF, Alan, DeFrancesco, Gregory L
Format: Patent
Sprache:eng ; fre ; ger
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Beschreibung
Zusammenfassung: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.