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A review on design and optimization of forced air-cooled cold plate for avionic application

机译:防空航空应用强制风冷冷板的设计与优化综述

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Now a day's electronic machinery and components are reducing in magnitude as a result difficulty keeps on increasing at an remarkable level. As well as the energy is increased, and volume is decreased. Which results in a remarkable raise of power density, which causes rise in temperatures and failures of the system? Guarded temperatures in components are to be ensured for a dependable electronic system. Elevated temperatures results in electronic malfunctions. For a minor temperature raise an out of tolerance condition might occur, if the temperature raise is huge a disastrous failure might take place. The fundamental problem that is faced during heat transfer is to eliminate of heat generated internally by providing a flow path from heat sources to the final sink (surrounding ambient air). Current day avionics are responsive and compact designed to be free from structural and thermal instability. A distinctive avionic gear for flying will be designed with miniaturized power amplifier components, high pace processors and power supply. The vast amount of heat generated must be dissipated efficiently so that the system will work without any interruption. Due to size and weight limitations design of custom heat sink cannot be produced. By taking all these points into consideration thermal administration is to be designed in such a way that cooling is done by using external fans. In this review paper a lot of research on management of cooling system and thermal analysis of electronic systems has been done.
机译:现在,一天的电子机械和组件幅度幅度幅度幅度难以保持在越来越多的水平。以及能量增加,并且体积减少。这导致功率密度显着提高,导致系统的温度和故障升高?为了可靠的电子系统,将确保部件中的保护温度。升高的温度导致电子故障。如果温度提高是巨大的灾难性失败,可能会出现轻微温度升高,可能会发生超出耐受性。传热期间面临的根本问题是通过提供从热源到最终水槽(周围环境空气)的流动路径来消除内部产生的热量。目前的日航空电子响应性和紧凑型设计,不源于结构性和热不稳定。用于飞行的独特航空齿轮将设计采用小型化功率放大器组件,高速度处理器和电源。产生的大量热量必须有效地耗散,使得系统将在没有任何中断的情况下工作。由于尺寸和重量限制定制散热器的设计无法生产。通过考虑所有这些点来考虑热量给药,以这种方式设计,使得通过使用外部风扇进行冷却。在本文中,已经完成了许多关于电子系统的冷却系统管理和热分析的研究。

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