发明名称 Thermal stress reduction in aircraft motor controllers
摘要 A thermal stress reduction method includes ramping an electric power generator, 240, to start an aircraft engine, 280, for a time period associated with the aircraft engine start sequence toggling three-level inverter switch array, 300, to a three-level pulse width modulation mode, determining if a first time interval in the three-level pulse width modulation mode exceeded a predetermined three-level pulse width modulation mode interval, in response to the first time interval exceeding the three-level pulse width modulation mode interval, toggling the three-level inverter switch array to a two-level pulse width modulation mode, determining if a second time interval in the two-level pulse width modulation mode exceeded a predetermined two-level pulse width modulation mode interval and in response to the second time interval exceeding the two-level pulse width modulation mode interval, toggling the three-level inverter switch array to the three-level pulse width modulation mode.
申请公布号 EP2654191(A2) 申请公布日期 2013.10.23
申请号 EP20130164707 申请日期 2013.04.22
申请人 HAMILTON SUNDSTRAND CORPORATION 发明人 CHAI, HUAZHEN;WHITE, ADAM M;KHERALUWALA, MUSTANSIR
分类号 H02M7/487;F02C7/26;H02P9/08 主分类号 H02M7/487
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