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首页> 外文期刊>Journal of Intelligent & Robotic Systems: Theory & Application >Experimental Analysis of Variable Collective-pitch Rotor Systems for Multirotor Helicopter Applications
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Experimental Analysis of Variable Collective-pitch Rotor Systems for Multirotor Helicopter Applications

机译:多旋翼直升机应用可变变桨距旋翼系统的实验分析

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This paper presents an experimental study of variable collective-pitch rotor systems for multirotor helicopter applications. An experimental research facility has been established to conduct this research. The facility enables the high-resolution measurement of forces and torques produced by rotor systems. The power consumption of the rotor system during experimentation can also be recorded. The experimental research facility also allows for the characterisation of the effect of rotor systems on multirotor helicopter performance. It is shown that the variable collective-pitch rotors have a significant performance advantage over fixed-pitch rotors when comparing thrust response, and multirotor helicopter step input response performance. Further, it is observed that variable collective-pitch rotors are more efficient in terms of energy consumption than comparable fixed-pitch rotors under similar operating conditions.
机译:本文提出了用于多旋翼直升机应用的可变集合螺距旋翼系统的实验研究。已经建立了实验研究机构来进行这项研究。该设备可以对转子系统产生的力和扭矩进行高分辨率测量。还可以记录实验过程中转子系统的功耗。实验研究设施还可以表征旋翼系统对多旋翼直升机性能的影响。结果表明,在比较推力响应和多旋翼直升机阶跃输入响应性能时,可变集合螺距旋翼比固定螺距旋翼具有明显的性能优势。此外,可以观察到,在相似的工作条件下,可变的集体螺距转子在能量消耗方面比类似的固定螺距转子更有效。

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