发明名称 AIRCRAFT POWER MANAGEMENT
摘要 An electric power management system of a vehicle may interconnect a power plant, a propeller drive unit, and a battery via a bus. A command limiting controller may direct the operation of the power plant and the propeller drive unit in fast and slow modes of operation, the fast mode of operation operating at a higher bus voltage than at a slow mode of operation. The command limiting controller may generate a bus current to drive the propeller drive unit according to a command limiting, voltage-versus-current curve that adjusts the bus current depending on an amount of voltage on the power bus; where the command limiting curve includes a minimum voltage portion, a maximum voltage portion and a control range therebetween having upper and lower voltage limits and upper and lower current limits for enhanced reliability and stable control of the propeller drive unit.
申请公布号 US2013066485(A1) 申请公布日期 2013.03.14
申请号 US201213657515 申请日期 2012.10.22
申请人 AEROVIRONMENT, INC.;AEROVIRONMENT, INC. 发明人 MATUSZESKI THADDEUS BENJAMIN;KOCH ROLLAND MITCHELL;BERMAN SCOTT GARRET;ABDULRAHIM MUJAHID
分类号 B64C19/00;B60L15/20 主分类号 B64C19/00
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