发明名称 INTEGRATED AIRCRAFT POWER CONDITIONING UNIT
摘要 An integrated power conditioning unit includes a DC bus, a first terminal for connection to first AC equipment, a second terminal for connection to second AC equipment, a first inverter circuit providing bi-directional AC-DC conversion between a first AC power signal and a first DC power signal, and a converter assembly providing bi-directional AC-DC conversion between a second AC power signal and a second DC power signal. A control module controls the first inverter circuit such that the first DC power signal may flow from/to the DC bus and the first AC power signal may flow from/to the first terminal. The control module also controls the converter assembly such that the second AC signal power signal may flow from/to the second terminal and the second DC power signal may flow from/to the DC bus.
申请公布号 US2010080027(A1) 申请公布日期 2010.04.01
申请号 US20080238905 申请日期 2008.09.26
申请人 GENERAL ELECTRIC COMPANY 发明人 WIEGMAN HERMAN LUCAS NORBERT;CARLSON WILLIAM EUGENE
分类号 H02M7/06 主分类号 H02M7/06
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