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1.发明授权公开(公告)号：US11738875B2
公开(公告)日：2023-08-29
申请号：US17209900
申请日：2021-03-23
IPC分类号： H02P1/00 , B64D27/24 , B64D31/14 , B64D31/06 , B64C29/00 , B60L50/61 , B60L50/51 , B60L50/13 , H02P9/04 , H02P21/24 , B64D27/02
CPC分类号： B64D27/24 , B60L50/13 , B60L50/51 , B60L50/61 , B64C29/0033 , B64D31/06 , B64D31/14 , H02P9/04 , H02P21/24 , B60L2200/10 , B60L2220/14 , B60L2220/42 , B60L2240/421 , B60L2240/427 , B64D2027/026 , B64D2221/00
摘要： Lightweight, energy-dense, high-efficiency, hybrid power systems for electric aircraft including a prime mover internal combustion engine or gas turbine coupled to a self-cooling polyphase axial-flux dual-Halbach-array motor/alternator where the number of phases Nphase is greater than or equal to three. The motor/alternator is connected to a regenerative power converter drive also having Nphase phases, which, in turn, is connected to a DC power bus, a battery, a battery management system, and a system controller. In some embodiments, the motor/alternator and regenerative power converter drive have a neutral connection.
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2.发明申请公开(公告)号：US20220185490A1
公开(公告)日：2022-06-16
申请号：US17209900
申请日：2021-03-23
摘要： Lightweight, energy-dense, high-efficiency, hybrid power systems for electric aircraft including a prime mover internal combustion engine or gas turbine coupled to a self-cooling polyphase axial-flux dual-Halbach-array motor/alternator where the number of phases Nphase is greater than or equal to three. The motor/alternator is connected to a regenerative power converter drive also having Nphase phases, which, in turn, is connected to a DC power bus, a battery, a battery management system, and a system controller. In some embodiments, the motor/alternator and regenerative power converter drive have a neutral connection.
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