Electrical conversion and distribution system for an aircraft

The invention relates to an electrical conversion and distribution system for an aircraft, the system comprising at least one synchronous starter-generator (S/G1, S/G2) intended to be coupled to an engine (Engine1) of the aircraft, at least one conversion path comprising a plurality of power convert...

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Bibliographische Detailangaben
Hauptverfasser:	GIORGIS VINCENT, HADJIDJ DJEMOUAI, CASIMIR ROLAND
Format:	Patent
Sprache:	chi ; eng
Schlagworte:	CIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTINGELECTRIC POWER CONVERSION OR DISTRIBUTION OF ELECTRIC POWER ELECTRICITY GENERATION SYSTEMS FOR STORING ELECTRIC ENERGY
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Beschreibung
Zusammenfassung:	The invention relates to an electrical conversion and distribution system for an aircraft, the system comprising at least one synchronous starter-generator (S/G1, S/G2) intended to be coupled to an engine (Engine1) of the aircraft, at least one conversion path comprising a plurality of power converters (CVn, CV'n) associated with switching means suitable for supplying at least one charge (CAC1, CAC2, CAC3, CAC4, P1, P2) from at least one source (S/G1, S/G2, AUX S/G1, AUX S/G2, GPU1, GPU2), and at least one distribution path suitable for supplying electrical charges (CT1n, SW1n, CT2n, SW2n). 本发明涉及种适于航空器的电气转换与分布系统，所述系统包括用来连接到航空器的发动机(Engine 1)上的至少个同步起动发电机(S/G1，S/G2)，至少个转换路径，其包括多个与切换装置相连的功率转换器(CVn，CV'n)，适于从至少个电源(S/G1,S/G2,AUX S/G1,AUX S/G2,GPU1,GPU2)向至少个负载(CAC1，CAC 2，CAC 3，CAC 4，P1，P2)供电，以及至少个分布路径，适于向电气负载(CT1n，SW1n，CT2n，SW2n)供电。