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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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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creator	GIORGIS VINCENT HADJIDJ DJEMOUAI CASIMIR ROLAND
description	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。
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language	chi ; eng
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subjects	CIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTINGELECTRIC POWER CONVERSION OR DISTRIBUTION OF ELECTRIC POWER ELECTRICITY GENERATION SYSTEMS FOR STORING ELECTRIC ENERGY
title	Electrical conversion and distribution system for an aircraft
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