发明名称 AIRCRAFT ELECTRIC MOTOR SYSTEM
摘要 <p>PROBLEM TO BE SOLVED: To provide a method and apparatus for controlling an electric aircraft.SOLUTION: A method and apparatus for controlling an electric aircraft is presented. An apparatus comprises a controller. The controller is configured to identify a state for an electric aircraft. The controller is further configured to identify a group of recharging parameters for a group of electric motors in an electric propulsion system. The electric propulsion system is configured to move the electric aircraft on the basis of the state of the group of electric motors for the electric aircraft. The controller is still further configured to recharge a power source for the electric aircraft using the group of recharging parameters to control recharging of the power source with the group of electric motors when a recharge state is present for the electric aircraft.</p>
申请公布号 JP2015085934(A) 申请公布日期 2015.05.07
申请号 JP20140178857 申请日期 2014.09.03
申请人 BOEING CO 发明人 CHRISTOPHER PETE BENSON;LEONARD J QUADRACCI;DOUGLAS C CAMERON
分类号 B64F3/02;B64C39/02;B64D27/24;H02J7/00 主分类号 B64F3/02
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