螺旋桨重叠对大型串联无人机性能的影响

A. Weishäupl, S. Prior
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引用次数: 3

摘要

研究了无人机在悬停飞行过程中螺旋桨重叠产生的干扰问题。使用定制支架和RCBenchmark系列1780测力仪对超轻型碳纤维螺旋桨进行了不同程度的重叠[公式:见文本]和垂直分离[公式:见文本]的测试。文献中报道了大量与同轴配置安装螺旋桨相关的损失的混淆,并对历史上的串联直升机进行了总结。结果突出了一个有利的重叠区域(0-20%),该区域具有对大范围无人机有利的潜力。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Influence of Propeller Overlap on Large-Scale Tandem UAV Performance
This paper investigates the interference that arises from overlapping Unmanned Aerial Vehicle (UAV) propellers during hovering flight. The tests have been conducted on [Formula: see text] ultralight carbon fiber propellers using a bespoke mount and the RCBenchmark Series 1780 dynamometer at various degrees of overlap [Formula: see text] and vertical separation [Formula: see text]. A great deal of confusion regarding the losses that are associated with mounting propellers in a co-axial configuration is reported in the literature, with a summary of historical tandem helicopters having been conducted. The results highlight a region of beneficial overlap (0–20%), which has the potential to be advantageous to a wide range of UAVs.
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