航空发动机帽罩热气膜防冰的加热特性  

Heating characteristics of aero-engine nose cone with film-heating anti-icing system

作　　者：柯鹏[1] 杨慧赟 王俊凯 杨春信[2] KE Peng;YANG Huiyun;WANG Junkai;YANG Chunxin(Aircraft/Engine Integrated System Safety Beijing Key Laboratory, School of Transportation Science and Engineering, Beijing University of Aeronautics and Astronautics, Beijing 100191, China;School of Aeronautics Science and Engineering, Beijing University of Aeronautics and Astronautics, Beijing 100191, China)

机构地区：[1]北京航空航天大学交通科学与工程学院飞机/发动机综合系统安全性北京市重点实验室,北京100191 [2]北京航空航天大学航空科学与工程学院,北京100191

出　　处：《航空动力学报》2018年第3期530-539,共10页Journal of Aerospace Power

基　　金：中央高校基本科研业务费(YWF-14-JTXY-009)

摘　　要：针对复合材料帽罩采用的一种热气膜防冰系统,采用计算流体力学方法研究了其内部冲击换热和外部气膜加热效果。发展了二维轴对称计算方法并与全三维计算结果进行了对比,搭建了热气吹风实验台,利用红外测温仪和热电偶测量帽罩温度,验证了数值计算方法。全面研究了不同射流雷诺数、相对冲击距和气膜缝结构参数对热气加热特性的影响,结果表明:增大射流雷诺数有利于提高内部冲击换热效果和外部气膜加热效果;最佳相对冲击距随射流雷诺数的增大而增大,射流雷诺数为10 000~40 000范围内最佳相对冲击距在5~8内取得;气膜射流能大幅提高缝后外壁面温度,加热效率与气膜缝宽和位置有关,前缘开设的气膜缝还会提升前缘冲击换热效果。For the film heating anti-icing system used in composite aero-engine nose cone,a computational fluid dynamics method was adopted to study the internal jet impingement heat transfer and external film heating efficiency.Two-dimensional axisymmetric algorithm was developed and compared with the results calculated by three-dimensional algorithm.A hot-air blowing experimental apparatus was built up and the infrared thermometer and thermocouple were used to verify the numerical simulation method.The effects of Reynolds number,relative impingement distance and structure parameters of film slot on heat transfer characteristics were comprehensively investigated.Results show that increasing Reynolds number is conducive to improving the internal jet impingement heat transfer andexternal film heating efficiency.The optimal value of relative impingement distance increases with the increasing Reynolds number,and the optimal value is between 5 and 8 when Reynolds number is between 10 000 and 40 000.Opening film slot can significantly increase the temperature of exterior surface,and heating efficiency is related to the width and location of film slot.Opening film slot at leading edge can also enhance jet impingement heat transfer.

关 键 词：防冰 帽罩 计算流体力学 测温实验 冲击换热 气膜加热 

分 类 号：V228.71[航空宇航科学与技术—飞行器设计]