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Experimental study of UAV propeller Thrust generation for various Propeller Blade-Span and the relation with mouth-ring

机译:不同螺旋桨叶片跨度的无人机推力生成的实验研究及与嘴环的关系

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In this study, the main focus is to investigate the thrust generation of various propeller blade width-spans with the relation of mouth-ring application. By using the parameter, the thrust was calculated based on the value of velocity, voltage and rpm. The testing was performed in two condition that is with mouth-ring and without mouth-ring and 2 size of propeller been tested in this experiment. The application of mouth-ring is based on the gap between the wall of mouth-ring and the blade tip. There are 3 size of gap; 10mm, 8mm and 5mm. The result shows that 10mm mouth-ring have better thrust generation other than two gap. In addition, if compare to with and without mouth-ring, the application of mouth-ring also has proved it has a better thrust. Furthermore, the application of mouth-ring is evaluating to be good base on this study.
机译:在这项研究中,主要重点是研究各种螺旋桨叶片宽度跨越的推力产生与口圈应用的关系。通过使用该参数,基于速度,电压和RPM的值计算推力。在两个条件下进行测试,该条件是口圈,没有嘴环,在该实验中测试了2尺寸的螺旋桨。口环的施加基于口圈壁和叶片尖端之间的间隙。有3个差距; 10mm,8mm和5mm。结果表明,除了两个间隙之外,10mm嘴环具有更好的推力生成。另外,如果与嘴环进行比较,嘴环的应用也证明它具有更好的推力。此外,嘴环的应用正在评估本研究的良好基础。

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