The invention relates to the technical field of cooling, and provides a skin structure, a cooling adjusting system and a cooling adjusting method. The skin structure comprises an annular heat exchanger, a first pipeline and a second pipeline, and the annular heat exchanger is used for being arranged outside the aircraft in a sleeving mode; the first end of the first pipeline communicates with a heat source of the aircraft, and the second end of the first pipeline communicates with the annular heat exchanger; the first end of the second pipeline communicates with the annular heat exchanger, and the second end of the second pipeline communicates with a heat source; wherein the heat source, the first pipeline, the annular heat exchanger and the second pipeline form a circulation loop, and the annular heat exchanger is used for exchanging heat with liquid in the heat source. According to the skin structure, the annular heat exchanger is arranged outside the aircraft in a sleeving mode, the annular heat exchanger is designed to be the skin of the aircraft through integrated design, the space occupied by the interior of the aircraft is reduced, meanwhile, the annular heat exchanger does not need to be provided with special refrigeration equipment for cooling a cooling medium, and energy consumption of the aircraft is reduced.
本发明涉及冷却技术领域,提供一种蒙皮结构、冷却调节系统及冷却调节方法。上述的蒙皮结构,包括:环形换热器、第一管路和第二管路,环形换热器用于套设于航行器的外部;第一管路的第一端用于与航行器的热源连通,第一管路的第二端与环形换热器连通;第二管路的第一端与环形换热器连通,第二管路的第二端用于与热源连通;其中,热源、第一管路、环形换热器以及第二管路形成循环回路,环形换热器用于与热源内的液体进行热交换。上述的蒙皮结构,通过在航行器的外部套设环形换热器,通过一体设计将环形换热器设计为航行器的蒙皮,减少了对航行器内部的空间占有,同时环形换热器不需要设置专门的制冷设备对冷却介质进行降温,降低了航行器的能耗。
Skin structure, cooling adjusting system and cooling adjusting method
蒙皮结构、冷却调节系统及冷却调节方法
2023-09-29
Patent
Electronic Resource
Chinese
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
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