| 某型无人机螺旋桨的设计与气动性能分析 |
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| 引用本文： | 贺军,项松,王艳冰,刘占军.某型无人机螺旋桨的设计与气动性能分析[J].航空动力学报,2021,36(5):1033-1039. |
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| 作者姓名： | 贺军 项松 王艳冰 刘占军 |
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| 作者单位： | 沈阳航空航天大学 航空宇航学院,沈阳110136;;沈阳航空航天大学 辽宁省通用航空重点实验室,沈阳 110136;辽宁通用航空研究院 科研管理办公室,沈阳 110136 |
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| 基金项目： | 辽宁省教育厅重点攻关和服务地方项目（JYT19004）； 航空科学基金项目（20173254006）； 辽宁省自然科学基金指导计划（20180550824） |
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| 摘 要： | 为了提高某型无人机(UAV)的航时,螺旋桨应该具有高的巡航效率、足够的爬升拉力。利用高效率螺旋桨设计方法设计了某型无人机的两叶木质螺旋桨,获得了螺旋桨的弦长和桨叶角分布,基于片条理论计算了螺旋桨的气动性能,进行了螺旋桨的地面静态试验。结果表明:螺旋桨性能计算结果与台架试验结果具有较好的一致性,螺旋桨性能计算的巡航效率为83.81%,巡航拉力为222.95 N。设计的两叶木质螺旋桨可以满足某型无人机的巡航效率与拉力需求。
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| 关 键 词： | 无人机(UAV) 螺旋桨 气动性能 巡航效率 片条理论 |
| 收稿时间： | 2020/7/30 0:00:00 |
Design and aerodynamic performance analysis of a type of UAV propeller |
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| HE Jun,XIANG Song,WANG Yanbing,LIU Zhanjun.Design and aerodynamic performance analysis of a type of UAV propeller[J].Journal of Aerospace Power,2021,36(5):1033-1039. |
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| Authors: | HE Jun XIANG Song WANG Yanbing LIU Zhanjun |
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| Institution: | College of Aerospace Engineering,,Shenyang Aerospace University,Shenyang 110136,China;;Liaoning Key Laboratory of General Aviation,,Shenyang Aerospace University,Shenyang 110136,China;Management Office of Science and Research,,Liaoning General Aviation Academy,Shenyang 110136,China; College of Aerospace Engineering,,Shenyang Aerospace University,Shenyang 110136,China;, |
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| Abstract: | In order to improve the endurance of a type of unmanned aerial vehicle (UAV), a propeller of high cruising efficiency and sufficient climbing thrust should be required. The two-blade wooden propeller of a type of UAV was designed by the high efficiency propeller design method. The chord length and blade angle distribution of the propeller were obtained. The aerodynamic performance of the propeller was calculated based on the strip theory. Ground static tests of propeller were carried out. The results of the performance calculation of the propeller were in good agreement with the results of the ground static tests. The calculated cruising efficiency was 83.81%, and the calculated cruising thrust was 222.95 N. The two-blade wooden propeller can meet the requirements of the cruising thrust and efficiency of a type of UAV. |
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| Keywords: | unmanned aerial vehicle(UAV) propeller aerodynamic performance cruising efficiency strip theory |
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