Measurement system for small propeller propulsion

J. Pieniążek, Piotr Cieciński
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引用次数: 5

Abstract

The propeller propulsion is mainly used kind of propulsion in small unmanned flying vehicles. In this propulsion an engine, in the most cases electric motor, powers the propeller which produces thrust. The efficiency of the use of engine energy by propeller depends on the proper propeller design or selection taking into account operating conditions. The whole propulsion characteristics are important for the numerical model development and advanced control systems. The optimized propeller increases the flight time of the particular vehicle. The test stand and testing method are main subjects of the paper. The tests of the motor with propeller or propeller only using some motor needs measurement devices of important variables, which are specified by theoretical analysis. Besides the measured system structure, main parts and user interface the sample results of raw data, computed propeller parameters, and pressure distribution along propeller blade are presented. The last data gives possibility for further analysis of the influence of a propeller geometry on propulsion parameters.
小型螺旋桨推进力测量系统
螺旋桨推进是小型无人飞行器主要采用的一种推进方式。在这种推进中,发动机,在大多数情况下是电动机,为产生推力的螺旋桨提供动力。螺旋桨利用发动机能量的效率取决于考虑到运行条件的适当的螺旋桨设计或选择。整体推进特性对数值模型的建立和先进的控制系统具有重要意义。优化后的螺旋桨增加了特定飞行器的飞行时间。试验台和试验方法是本文的主要研究内容。电机配螺旋桨或螺旋桨只配部分电机的试验需要重要变量的测量装置,这些测量装置由理论分析规定。除了实测的系统结构、主要部件和用户界面外,还给出了原始数据的采样结果、计算的螺旋桨参数和沿桨叶的压力分布。最后的数据为进一步分析螺旋桨几何形状对推进参数的影响提供了可能。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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