飞行器舵机摆线减速器输出装置传热分析

为探究飞行器舵机在高温下的工作情况针对飞行器舵机摆线减速器利用Unigraphics NXHypermesh和ANSYS等软件基于有限元方法对减速器输出机构进行传热分析。采用高阶四面体单元对减速器销轴输出机构进行有限元离散并在与舵翼直接相连的输出机构凸台采用等温加载经数值计算得到飞行器输出机构温度分布及变化状况。结果表明：有限元方法可以有效地分析飞行器输出机构传热情况舵翼温度和摆线轮定位位置是影响减速器正常工作时间的重要因素降低舵翼温度以及将摆线轮靠销轴远热端定位可提高飞行器舵机寿命。

Heat transfer analysis of the output unit of cycloidal reducers for aircraft actuator

To investigate the work condition of the aircraft actuators in high temperatureheat transfer process of the output unit of a cycloidal reducer of the actuator is taken into account by Unigraphics NXHypermesh and ANSYS softwares based on finite element analysis(FEA).The temperature distribution of the output unit is obtained by meshing modelapplying loads and solving discrete problems.Thenthe temperature variation of the output unit is gotten by sampling and processing the data of FEA results.In the endthree main conclusions are drawn.Firstthe heat transfer process of the output units of cycloidal reducers of actuators can be analyzed by FEA efficiently.Secondthe temperature of the rudder and the design position of cycloid gears are two major factors in the operating life of reducers.Thirdthe operating life can be improved by lowering the rudder temperature and installing the cycloidal gear as far as possible away from the heat source.