TWO-TURBINE ENVIRONMENTAL CONTROL SYSTEM

An environmental control system for an aircraft according to an example of the present disclosure includes a first turbine coupled to an engine and a second turbine coupled to a compressor. One or more ducts are configured to provide bleed air from the engine to the first and second turbines and the...

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Bibliographische Detailangaben
Hauptverfasser:	Pess, Matthew, Retersdorf, Alan, DeFrancesco, Gregory L
Format:	Patent
Sprache:	eng
Schlagworte:	AIR INTAKES FOR JET-PROPULSION PLANTS AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION BLASTING COMBUSTION ENGINES CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS COSMONAUTICS EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS GAS-TURBINE PLANTS HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS LIGHTING MECHANICAL ENGINEERING PARACHUTES PERFORMING OPERATIONS TRANSPORTING WEAPONS
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Beschreibung
Zusammenfassung:	An environmental control system for an aircraft according to an example of the present disclosure includes a first turbine coupled to an engine and a second turbine coupled to a compressor. One or more ducts 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.