发明名称 Power supply system for aircraft, has electric cores having input stage with alternate current/direct current converter, switching matrix that connect power modules through inductor, and switching assembly connected to charge
摘要 <p>The system has generators supplying distinct electric cores with 230 volts. Each core has an input stage (40) with an alternate current/direct current converter (46) and insulation contactors (45) provided with a precharge system. The core has power modules arranged in a parallel manner and interconnection inductor (41) between the modules. A switching matrix (42) connects the modules through the inductor, and an output filter (43). A switching assembly (44) is connected to a charge.</p>
申请公布号 FR2907760(A1) 申请公布日期 2008.05.02
申请号 FR20060054513 申请日期 2006.10.25
申请人 AIRBUS FRANCE SOCIETE PAR ACTIONS SIMPLIFIEE 发明人 LANGLOIS OLIVIER;PRISSE LUCIEN;FOCH ETIENNE;ALEJO DOMINIQUE
分类号 B64D41/00;H02J3/38 主分类号 B64D41/00
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