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 controller may direct the operation of the power plant and the propeller drive unit. In a slow control mode, the propeller drive unit may react slowly to small throttle change requests. In the slow control mode, the propeller drive unit may draw power completely or substantially from the power plant. Upon a throttle request to rapidly change propeller drive unit speed more than a threshold amount, the controller may direct that the propeller drive unit quickly obtain the requested speed by drawing power required from the battery in excess of that being generated from the power plant. Subsequently, the controller may direct that the power plant increase power generation to maintain the propeller drive unit at the new speed, and recharge or float the battery.
申请公布号 AU2010298512(A1) 申请公布日期 2012.05.10
申请号 AU20100298512 申请日期 2010.09.20
申请人 AEROVIRONMENT, INC. 发明人 MATUSZESKI, THADDEUS BENJAMIN;KOCH, ROLLAND MITCHELL;BERMAN, SCOTT GARRET;ABDULRAHIM, MUJAHID
分类号 B64C11/00 主分类号 B64C11/00
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