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Estimation of the Maximum Thermionic Emission Cooling of High-Speed Aircraft
Russian Aeronautics Pub Date : 2020-12-03 , DOI: 10.3103/s1068799820030010
A. V. Kolychev , V. A. Kernozhitskii , M. V. Chernyshov

Abstract

The paper analyzes the possibilities of using the thermionic cooling methods that significantly reduce the temperature and temperature stresses in the elements and structures of aircraft, increasing the life of thermally loaded elements and flight safety. We estimate the range of altitudes and flight speeds of aircraft at which the practical implementation of thermionic cooling is possible.



中文翻译:

高速飞机的最大热电子发射冷却估算

摘要

本文分析了使用热电子冷却方法的可能性,该方法可显着降低飞机元件和结构中的温度和温度应力,从而增加热载元件的寿命和飞行安全性。我们估计可以实际实施热电子冷却的飞机的高度和飞行速度范围。

更新日期:2020-12-04
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