UNITE D'ALIMENTATION EN AIR SOUS PRESSION POUR AERONEF

Pressurised-air supply unit (1A; 1B; 1C; 1D) for an aircraft, comprising: a load compressor (30) configured to supply pressurised air (3) to the aircraft; a driving part (10) that can drive the load compressor (30); an electric motor (60) that can drive the load compressor (30); an electrical supply...

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Bibliographische Detailangaben
Hauptverfasser:	RENOTTE, ALEXIS, TUNZINI, MARC DANIEL
Format:	Patent
Sprache:	fre
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:	Pressurised-air supply unit (1A; 1B; 1C; 1D) for an aircraft, comprising: a load compressor (30) configured to supply pressurised air (3) to the aircraft; a driving part (10) that can drive the load compressor (30); an electric motor (60) that can drive the load compressor (30); an electrical supply connector (61) configured to transmit electrical power (60) supplied by an electrical power source outside of the aircraft; and an electrical conversion unit (UC) positioned between the electrical motor (60) and the electrical supply connector (61), the electrical conversion unit being capable of supplying, without conversion, the electrical power (60) supplied by the electrical power source outside of the aircraft to the electrical motor (60), and of converting the electrical power (60) supplied by the electrical power source outside of the aircraft and of supplying the electrical motor (60) with the converted electrical power (6).