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公开(公告)号：EP4363252A1
公开(公告)日：2024-05-08
申请号：EP22758580.9
申请日：2022-06-29
申请人： Skybridge U.K. Ltd
发明人： SUCIC, Zvonimir , PAVILAINEN, Maxim
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公开(公告)号：EP4357179A1
公开(公告)日：2024-04-24
申请号：EP22202270.9
申请日：2022-10-18
申请人： Volocopter GmbH
发明人： Georgiadis, Kyriakos
IPC分类号： B60K1/04 , H01M10/625 , B60L50/64 , B64D27/24 , B64D45/00 , H01M10/6556 , H01M50/143 , H01M50/24 , H01M50/249
CPC分类号： H01M10/625 , H01M10/613 , H01M50/143 , H01M50/249 , H01M50/24 , B60K1/04 , B60L50/64 , B64D27/24 , B64D45/00 , H01M10/6556 , H01M2220/2020130101 , H01M50/213 , H01M50/278 , H01M50/227 , B60L2240/54520130101 , B60L58/26 , B60L58/21 , B60L3/0046 , B64U50/19 , B64U50/30 , B60K1/00 , B60Y2200/5020130101
摘要： We describe a battery cell arrangement (1) for use in an aircraft, comprising: a plurality of battery cells (2); at least one battery housing (3) enclosing said plurality of battery cells (2), said housing (3) having an opening (3a); and
a number of separating elements (4) that are located inside said battery housing (3), for separating individual battery cells (2) from each other; wherein each battery cell (2) is associated with a respective vent channel (5), which vent channels (5) open to said opening (3a); said vent channels (5) define a number of battery cell compartments, each of said compartments holding a subset of said plurality of battery cells (2) and each of said compartments being closed by a cover element (6), which cover element (6) is devised to open if a battery cell (2) in a corresponding compartment goes into thermal runaway and produces gaseous venting products (GP). Further described is an aircraft having such a battery cell arrangement.-
公开(公告)号：EP4185528B1
公开(公告)日：2024-07-17
申请号：EP21740591.9
申请日：2021-07-20
IPC分类号： B64C25/42 , B60B27/00 , B60T5/00 , F16D65/847 , F16D65/78
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公开(公告)号：EP4063265B1
公开(公告)日：2024-07-10
申请号：EP22161611.3
申请日：2022-03-11
CPC分类号： B64C25/36 , B60B35/004 , B60B35/04 , B60B27/0078 , B60Y2200/5020130101
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