- 专利标题: BATTERY MODULE FOR AN ELECTRICALLY-DRIVEN AIRCRAFT, METHOD FOR MANUFACTURING A BATTERY MODULE AND ELECTRICALLY-DRIVEN AIRCRAFT POWERED BY A BATTERY MODULE
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申请号: US18579299申请日: 2022-03-17
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公开(公告)号: US20240317109A1公开(公告)日: 2024-09-26
- 发明人: Sébastien Demont , Franco Summermatter , Sébastien Luisier , Eduardo Guzman Roca , Daniel Diaz , Gianmichele Bertini
- 申请人: H55 SA
- 申请人地址: CH Sion
- 专利权人: H55 SA
- 当前专利权人: H55 SA
- 当前专利权人地址: CH Sion
- 国际申请: PCT/IB2022/052444 2022.03.17
- 进入国家日期: 2024-01-12
- 主分类号: B60L58/18
- IPC分类号: B60L58/18 ; B60L3/00 ; B60L50/40 ; B60L53/00 ; B64D27/24 ; B64D45/00 ; B64F5/60 ; H02J7/14 ; H02J7/34 ; H02P5/00
摘要:
A battery module for an electrically-driven aircraft is disclosed. The battery module can house multiple battery cells and prevent a battery cell fire or explosion from one battery cell from damaging neighboring battery cells. The battery module includes: a housing; a plurality of cell tubes housing a plurality of battery cells, each cell tube having an elongated surface and being positioned in the housing spaced apart from each other; a heat absorbing member comprising a heat absorbing material, wherein the heat absorbing member is arranged between at least two neighboring cell tubes; and the heat absorbing material being configured to undergo a phase transition from an initial state of matter into a final state of matter when at least one of the plurality of cell tubes exceeds a predetermined temperature in case of explosion or fire of at least one of the plurality of battery cells.
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