公开(公告)号：US20240326599A1

公开(公告)日：2024-10-03

申请号：US18737373

申请日：2024-06-07

Applicant: Archer Aviation Inc.

Inventor： Saienath POOPALARAJAH ,  Pedro Roberto Paterson CARLEIAL ,  Paul FRIHAUF

IPC: B60L3/04 ,  B60L50/60 ,  B64C29/00 ,  H01M50/583 ,  H02H7/20

CPC classification number: B60L3/04 ,  B60L50/60 ,  H01M50/583 ,  H02H7/20 ,  B60L2200/10 ,  B64C29/0008 ,  H01M2200/103 ,  H01M2220/20

Abstract: 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.