An aircraft thermal management system includes a high temperature circuit and a low temperature circuit. The high temperature loop is configured to manage a temperature of a fuel cell stack in the engine compartment using the engine compartment heat exchanger. The cryogenic circuit is configured to cool a plurality of thermal loads in the engine compartment using the thermal capacity of the liquid hydrogen.
一种飞机热管理系统,包括高温回路和低温回路。高温回路配置为使用发动机舱热交换器来管理发动机舱中的燃料电池堆的温度。低温回路配置为使用液氢的热容量来冷却发动机舱中的多个热负荷。
Fuel cell aircraft thermal management system
燃料电池飞机热管理系统
2025-02-21
Patent
Electronic Resource
Chinese
Improving Aircraft Fuel-Thermal Management
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