- 专利标题: Cooling architecture for hydrogen fuel cell-powered aircraft
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申请号: US17662405申请日: 2022-05-06
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公开(公告)号: US12129044B2公开(公告)日: 2024-10-29
- 发明人: Ritish Tejpal
- 申请人: ZeroAvia, Inc.
- 申请人地址: US CA Hollister
- 专利权人: ZeroAvia, Inc.
- 当前专利权人: ZeroAvia, Inc.
- 当前专利权人地址: US CA Hollister
- 代理机构: Osha Bergman Watanabe & Burton LLP
- 主分类号: B64D33/10
- IPC分类号: B64D33/10 ; B60L58/33 ; B64D27/02 ; B64D27/24 ; B64D41/00 ; G01K13/00 ; H01M8/04007 ; H01M8/04014 ; H01M8/04111 ; H01M8/0432 ; H01M8/04746
摘要:
A cooling architecture for an integrated hydrogen-electric engine having a radiator and a hydrogen fuel cell includes a t and a manifold. The turbine is disposed in fluid communication with the hydrogen fuel cell. The turbine is configured to compress a predetermined amount of air and direct a first portion of the predetermined amount of the compressed air to the fuel cell for generating electricity that powers the integrated hydrogen-electric engine. The manifold is disposed in fluid communication with the turbine and positioned to direct a second portion of the predetermined amount of compressed air to the radiator for removing heat from the radiator.
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