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公开(公告)号：US20240326629A1
公开(公告)日：2024-10-03
申请号：US18740189
申请日：2024-06-11
发明人： Alex CLARABUT , Paul FRIHAUF , Yalan BI , Holger TEICHGRAEBER , Mamdouh MUBARAK ALTAYEB , Jon David PETERSON
CPC分类号： B60L53/62 , B60L53/14 , B60L58/26 , B64F1/35 , H02J7/0047 , H02J7/00714 , B60L2200/10
摘要： Aspects of the present disclosure generally relate to systems and methods for the configuration and control of charging and cooling systems for aircrafts driven by electric propulsion systems and in other types of vehicles. In some embodiments, a method of charging an aircraft is disclosed comprising: receiving a mode of operation indicating whether battery packs of the aircraft are connected in parallel prior to joining a charging bus, receiving charging protocol information, and controlling charging operations of the battery packs based on the mode of operation and the charging protocol information.
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公开(公告)号：US20240326599A1
公开(公告)日：2024-10-03
申请号：US18737373
申请日：2024-06-07
申请人： Archer Aviation Inc.
IPC分类号： B60L3/04 , B60L50/60 , B64C29/00 , H01M50/583 , H02H7/20
CPC分类号： B60L3/04 , B60L50/60 , H01M50/583 , H02H7/20 , B60L2200/10 , B64C29/0008 , H01M2200/103 , H01M2220/20
摘要： An electrical system for an aircraft, comprising at least one processor configured to: receive aircraft movement information, detect that the movement information indicates a potential crash, detect a loss of continuity in at least one low voltage wire, and blow a battery pack fuse to disconnect supply of the high voltage power to the aircraft.
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