发明名称 ELECTRICAL SYSTEM FOR STARTING UP AIRCRAFT ENGINES
摘要 <p>An electrical system for starting an engine is provided. The system includes: an AC/DC rectifier powered by an AC power network to deliver a first DC voltage Vdc, a DC/AC converter module for delivering an AC voltage for starting the engine from said first DC voltage Vdc, and k n-phase inverters arranged in parallel (k>1) and each delivering power no greater than half a maximum power Pmax required for starting the engine, and the two power supply lines of each of the inverters are connected to an electronic protection device receiving the first DC voltage Vdc, and the n outputs of each of the inverters delivering the AC voltage for starting the engine via n respective series inductors.</p>
申请公布号 EP2377235(B1) 申请公布日期 2015.09.02
申请号 EP20100706013 申请日期 2010.01.08
申请人 HISPANO SUIZA 发明人 DE WERGIFOSSE, ERIC
分类号 H02M7/493;B64D31/02;H02H7/122;H02P1/00 主分类号 H02M7/493
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