Air-conditioning system for airplane cabins

An air-conditioning system in particular for aircraft is proposed wherein pressurized, moisture-containing air is conditioned for air-conditioning the cabin. The pressurized air is compressed further in two separate stages (C1,C2), dehumidified in a high-pressure water extraction cycle (CON,WE2) and...

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Bibliographische Detailangaben
1. Verfasser:	ALFRED SAUTERLEUTE
Format:	Patent
Sprache:	eng
Schlagworte:	AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TOTRANSPORTATION COSMONAUTICS EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS PARACHUTES PERFORMING OPERATIONS TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINSTCLIMATE CHANGE TRANSPORTING
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Beschreibung
Zusammenfassung:	An air-conditioning system in particular for aircraft is proposed wherein pressurized, moisture-containing air is conditioned for air-conditioning the cabin. The pressurized air is compressed further in two separate stages (C1,C2), dehumidified in a high-pressure water extraction cycle (CON,WE2) and subsequently expanded in one or two turbine stages (T). Depending on the design one can thereby achieve ice-free conditioned air or a high efficiency of the air-conditioning system, in particular if two turbine stages (T1,T2) are provided and the energy gained in the particular turbine stages is utilized regeneratively, distributed over the compressor stages (C1,C2).