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不同进气方式对机载电子设备气冷冷板性能影响
引用本文:任童,彭孝天,陈维建,冯诗愚. 不同进气方式对机载电子设备气冷冷板性能影响[J]. 海军航空工程学院学报, 2019, 34(5): 443-447
作者姓名:任童  彭孝天  陈维建  冯诗愚
作者单位:南京航空航天大学航空学院飞行器环境控制与生命保障工业和信息化部重点实验室,南京210016;南京航空航天大学航空学院飞行器环境控制与生命保障工业和信息化部重点实验室,南京210016;南京航空航天大学航空学院飞行器环境控制与生命保障工业和信息化部重点实验室,南京210016;南京航空航天大学航空学院飞行器环境控制与生命保障工业和信息化部重点实验室,南京210016
基金项目:江苏省研究生科研与实践创新计划项目;中央高校基本科研业务费专项资金资助项目;江苏高校优势学科建设工程资助项目
摘    要:
电子设备的热负荷占到了航空器全机热负荷的60%以上,高温失效是电子设备失效的主要形式,采取合理的散热手段及时带走电子设备产生的热量对飞行安全和电子设备工作的稳定性有着至关重要的影响。文章利用计算流体力学方法(CFD)对某机载电子设备用气冷冷板进行了传热模拟,通过改变入口速度以及冷空气的流动方式,得到不同工况下气冷冷板各位置的温度分布和工作性能。研究结果显示,入口速度增加会使冷却效果得到提升,但同时增加了流动阻力使得设备工作的稳定性下降。另外,流动方式一(中间进两侧出)的冷却效果优于流动方式二(两侧进中间出),流动方式二的工作噪音和流动阻力优于流动方式一,可根据实际需要进行选择。

关 键 词:气冷冷板  机载电子设备  数值模拟  散热  飞机

Design and Performance Analysis of Air-Cooled Plate for Airborne Electronic Equipment
REN Tong,PENG Xiaotian,CHEN Weijian and FENG Shiyu. Design and Performance Analysis of Air-Cooled Plate for Airborne Electronic Equipment[J]. Journal of Naval Aeronautical Engineering Institute, 2019, 34(5): 443-447
Authors:REN Tong  PENG Xiaotian  CHEN Weijian  FENG Shiyu
Affiliation:Key Laboratory of Aircraft Environmental Control and Life Support Industry and Information Technology,Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China,Key Laboratory of Aircraft Environmental Control and Life Support Industry and Information Technology,Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China,Key Laboratory of Aircraft Environmental Control and Life Support Industry and Information Technology,Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China and Key Laboratory of Aircraft Environmental Control and Life Support Industry and Information Technology,Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China
Abstract:
The thermal load of electronic equipment accounts for more than 60% of the total thermal load of the aircraft.High temperature failure is the main form of failure of electronic equipment. Reasonable heat dissipation means timely tak?ing away the heat generated by electronic equipment to stabilize flight safety and electronic equipment. In this paper, thecomputational fluid dynamics (CFD) method was used to simulate the heat transfer of an air-cooled cold plate for an air?borne electronic device. By changing the inlet flow rate and the flow pattern of cold air, the temperature distribution andworking performance of each position of the air-cooled plate under different working conditions were obtained. The re?search results show that the increase of the inlet flow rate will increase the cooling effect but increase the flow resistance,which will reduce the stability of the equipment operation. In addition, the cooling effect of the flow mode one (the middleside is two sides) is better than the flow mode two (the two sides enter the middle), and the working noise and flow resis?tance of the flow mode two are better than the flow mode one, which can be carried out according to the actual situation se?lect.
Keywords:air cooled plate   airborne electronic equipment   numerical simulation   dissipate heat   aircraft
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