The invention provides an electric aircraft which comprises an environment control system, a battery and at least one heat pipe. The battery is arranged in the electric aircraft and provides electric energy support for the electric aircraft; the heat pipe comprises a first pipe section and a second pipe section, and the first pipe section is configured to perform heat transfer with the battery; the environmental control system comprises a refrigerating system, and the refrigerating system cools the second pipe section when the temperature of the battery is larger than the set first temperature. According to the electric aircraft and the control method of the battery of the electric aircraft, the heat pipe and the battery are used for heat exchange, the battery is cooled through the characteristic that the heat pipe conducts high-efficiency heat transfer, meanwhile, the environment control system is coupled with the heat pipe, and the refrigerating system of the environment control system is used for cooling the second pipe section of the heat pipe; and the heat dissipation efficiency and the heat dissipation speed of the heat pipe for heat dissipation of the battery are improved.
本发明提供一种电动飞行器,包括环控系统,还包括:电池和至少一个热管。电池设置在电动飞行器内,并为电动飞行器提供电能支持;热管包括第一管段和第二管段,第一管段被配置为与电池进行热传递;其中,环控系统包括制冷系统,制冷系统在电池的温度大于设定的第一温度时对第二管段进行冷却。本发明提供一种电动飞行器和电动飞行器电池的控制方法,使用热管和电池进行换热,利用热管进行高效率传热的特点对电池散热,同时还将环控系统与热管相耦合,利用环控系统的制冷系统对热管的第二管段进行降温,增大热管对电池散热时的散热效率和散热速度。
Electric aircraft and control method of electric aircraft battery
一种电动飞行器和电动飞行器电池的控制方法
2023-10-31
Patent
Electronic Resource
Chinese
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