The invention provides a heat exchange loop and a heat exchange system of a hybrid power aircraft, relates to the technical field of aircraft heat management, and is used for transmitting cold energy to required heat dissipation equipment, realizing heat dissipation of the equipment and ensuring stable and safe operation of aircraft system equipment. The heat exchange loop comprises a cold side flow path and a hot side flow path, and the cold side flow path and the hot side flow path are connected through a shared mixed liquid heat exchanger. The cold side flow path is composed of the mixed liquid heat exchanger, a wing oil tank and a first electric drive pump which are sequentially connected end to end. The hot side flow path is composed of the mixed liquid heat exchanger, a liquid storage tank, a second electric drive pump, a DC/DC converter and a propulsion motor controller which are sequentially connected end to end. Wherein the cold side flow path is driven by the first electric drive pump to achieve cold side fuel oil circulation, and the hot side flow path is driven by the second electric drive pump to achieve hot side fuel oil circulation.
本申请提供了一种混合动力飞机换热回路及换热系统,涉及飞机热管理技术领域,用于将冷量传输至所需的散热设备,实现设备散热并保证飞机系统设备的稳定安全运行。该换热回路包括:冷边流路和热边流路,所述冷边流路和所述热边流路通过共用的混合液换热器连接;所述冷边流路由首尾依次连接的所述混合液换热器、机翼油箱以及第一电驱动泵组成;所述热边流路由首尾依次连接的所述混合液换热器、储液箱、第二电驱动泵、DC/DC变换器以及推进电机控制器组成;其中,所述冷边流路通过所述第一电驱动泵的驱动实现冷边燃油循环,所述热边流路通过所述第二电驱动泵的驱动实现热边燃油循环。
Heat exchange loop and heat exchange system of hybrid aircraft
一种混合动力飞机换热回路及换热系统
2024-03-15
Patent
Electronic Resource
Chinese
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
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