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论文:2016,Vol:34,Issue(3):460-466 |
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引用本文： |
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项松, 刘远强, 佟刚, 张利国, 康桂文, 吴江, 王吉, 刘百明. 某型电动飞机螺旋桨的设计与试验[J]. 西北工业大学学报 |
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Xiang Song, Liu Yuanqiang, Tong Gang, Zhang Liguo, Kang Guiwen, Wu Jiang, Wang Ji, Liu Baiming. Design and Test of an Electric Powered Aircraft Propeller[J]. Northwestern polytechnical university |
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| 某型电动飞机螺旋桨的设计与试验 |
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| 项松, 刘远强, 佟刚, 张利国, 康桂文, 吴江, 王吉, 刘百明 |
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| 沈阳航空航天大学 辽宁省通用航空重点实验室, 辽宁 沈阳 110136 |
| 摘要: |
| 某型电动飞机采用稀土永磁电动机作为动力装置,采用螺旋桨产生拉力。为了提高电动飞机的航时,螺旋桨的设计目标应为:具有较高的效率,足够的拉力,并且保证螺旋桨需用功率与电动机功率相匹配。设计了某型电动飞机的固定桨距螺旋桨,建立了螺旋桨的三维CATIA模型,制造了两叶的木质螺旋桨,进行了螺旋桨的地面试验和风洞试验。试验结果表明:该型螺旋桨在起飞状态(螺旋桨转速2 164 r/min),静态拉力达到98.2 kg,电动机轴功率为35.09 kW,电池输出功率37.08 kW;巡航状态,螺旋桨效率达86.76%,设计的螺旋桨达到了预期的设计目标。 |
| 关键词:
电动飞机
螺旋桨
高效率
地面试验
风洞试验
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| Design and Test of an Electric Powered Aircraft Propeller |
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| Xiang Song, Liu Yuanqiang, Tong Gang, Zhang Liguo, Kang Guiwen, Wu Jiang, Wang Ji, Liu Baiming |
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| Liaoning Key Laboratory of General Aviation, Shenyang Aerospace University, Shenyang 110136, China |
| Abstract: |
| The power plant of an electric powered aircraft is the rare earth permanent magnetic electric motor. The propeller is used to generate the thrust for this aircraft. In order to improve the endurance of the electric powered aircraft, the design object of propeller is to design the propeller with high efficiency and enough thrust, the required power of propeller should match with the output power of electric motor. The present paper designed a fixed pitch propeller, created the 3-D CATIA model of propeller, and manufactured the two-blade wooden propeller, carried out the ground test and wind-tunnel test of propeller. The test results show that, at take-off condition (2164r/min), static thrust is 98.2kg, shaft power of electric motor is 35.09kw, output power of battery is 37.08kw; at cruise condition, efficiency of propeller is 86.76%, the propeller meets the design requirement. |
| Key words:
electric powered aircraft
propeller
high efficiency
ground test
wind-tunnel test
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| 收稿日期: 2015-10-27
修回日期:
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| DOI: |
| 基金项目: 辽宁"百千万人才工程"项目(2014921048)、辽宁省科学技术计划面上项目(2015020167)与沈阳市科技计划项目(F16-205-1-07)资助 |
| 通讯作者:
Email： |
| 作者简介: 项松(1978—),沈阳航空航天大学高级工程师,主要从事高效率低噪声螺旋桨设计研究。
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| 相关功能 |
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| 作者相关文章 |
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| 项松 在本刊中的所有文章 |
| 刘远强 在本刊中的所有文章 |
| 佟刚 在本刊中的所有文章 |
| 张利国 在本刊中的所有文章 |
| 康桂文 在本刊中的所有文章 |
| 吴江 在本刊中的所有文章 |
| 王吉 在本刊中的所有文章 |
| 刘百明 在本刊中的所有文章 |
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参考文献: |
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[1] Larrabee E E. Practical Design of Minimum Induced Loss Propellers[C]//SAE Preprint 790585, 1979
[2] Eppler R, Hepperle M. A Procedure for Propeller Design by Inverse Methods[C]//International Conference of Inverse Design Concepts in Engineering Sciences, Austin TX,1984: 445-460
[3] Romeo G, Borrello I F, Cestino E, et al. ENFICA-FC: Environmental Friendly Inter-City Aircraft and 2-Seat Air-Craft Powered by Fuel Cells Electric Propulsion[C]//Airtec 2nd International Conference "Supply on the Wings", Frankfurt,(Germany), 2007: 24-25
[4] Romeo G, Moraglio I, Novarese C. ENFICA-FC: Preliminary Survey & Design of 2-Seat Aircraft Powered by Fuel Cells Electric propulsion[C]//7th AIAA Aviation Technology Integration and Operation Conference, 2007, Belfast, Northern Ireland
[5] Romeo G, Borello F. ENFICA-FC: Environmental Friendly Inter-City Aircraft Design and Realization of 2-Seater Aircraft Powered by Fuel Cells Electric Propulsion[C]//XX Associazione Italiana di Aeronautica e Astronautica Congress, Milano, Italy, 2009
[6] Romeo G, Cestino E, Borello F, et al. Engineering Method for Air-Cooling Design of Two-Seat Propeller-Driven Aircraft Powered by Fuel Cells[J]. Journal of Aerospace Engineering, 2011, 24(1): 79-88
[7] Romeo G, Cestino E, Pacino M, Borello F, Correa G. Design and Testing of a Propeller for a Two-Seater Aircraft Powered by Fuel Cells[J]. Journal of Aerospace Engineering, 2012, 226: 804-816
[8] Angelo S D, Berardi F, Minisci E. Aerodynamic Performances of Propellers with Parametric Considerations on the Optimal Design[J]. The Aeronautical Journal, 2002, 106: 313-320
[9] 潘杰元,钱惠德. 螺旋桨的数值优化设计[J]. 航空动力学报, 1991, 6(4): 300-304 Pan Jieyuan, Qian Huide. Aerodynamic Design of Propeller by Numerical Optimization[J]. Journal of Aerospace Power, 1991, 6(4): 300-304 (in Chinese)
[10] 马晓平, 宋笔锋. 提高小型无人机螺旋桨效率的工程方法[J]. 西北工业大学学报, 2004, 22(2): 209-212 Ma Xiaoping, Song Bifeng. Practical Measures for Raising Propeller Efficiency of Low Speed Mini UAV[J]. Journal of North-western Polytechnical University, 2004, 22(2): 209-212 (in Chinese)
[11] 罗东明, 昂海松. 倾转螺旋桨飞行器桨叶的气动设计研究[J]. 航空动力学报, 2002, 17(5): 513-517 Luo Dongming, Ang Haisong. Aerodynamic Design of Tilt Rotor/Propeller Blade[J]. Journal of Aerospace Power, 2002, 17(5): 513-517 (in Chinese)
[12] 罗东明, 周军, 昂海松. 微型飞行器螺旋桨的气动优化设计[J]. 南京航空航天大学学报, 2003, 35(3): 322-325 Luo Dongming, Zhou Jun, Ang Haisong. Aerodynamic Optimization Design of Micro Air Vehicle Propeller[J]. Journal of Nanjing University of Aeronautics and Astronautics, 2003, 35(3): 322-325 (in Chinese)
[13] 高永卫, 黄灿金, 魏闯. 一种涵道螺旋桨的简便设计方法[J]. 航空工程进展, 2013, 4(3): 352-357 Gao Yongwei, Huang Canjin, Wei Chuang. A Simple Approach to the Design of Ducted Propeller[J]. Advances in Aeronautical Science And Engineering, 2013, 4(3): 352-357 (in Chinese)
[14] 夏贞锋, 罗淞, 杨永. 基于激励盘理论的螺旋桨滑流数值模拟研究[J]. 空气动力学学报, 2012, 30(2): 219-222 Xia Zhenfeng, Luo Song, Yang Yong. Numerical Simulations of Propeller Slipstream Flows Using Actuator Disk Theory[J]. Acta Aerodynamica Sinica, 2012, 30(2): 219-222 (in Chinese)
[15] 左岁寒, 杨永. 螺旋桨滑流对带后缘襟翼机翼气动特性影响的数值分析[J]. 航空计算技术, 2007, 37(1): 54-57 Zuo Suihan, Yang Yong. Numercal Simulation of Propeller/High Lift System Interaction[J]. AeronauticaI Computing Technique, 2007, 37(1): 54-57 (in Chinese)
[16] 高永卫, 乔志德. 一种快速计算螺旋桨气动声学特性的数值方法[J]. 空气动力学学报, 2006, 24(2): 187-194 Gao Yongwei, Qiao Zhide. A Fast Numerical Method for Calculating Propener Aerodynamic and Acoustic Characteristics[J]. Acta Aerodynamica Sinica, 2006, 24(2): 187-194 (in Chinese)
[17] 马亮, Lohmann D, Kuntz M. 基于Kirchhoff方法的跨音速螺旋桨的气动声学计算[J]. 航空动力学报, 1999, 14(3): 285-288 Ma Liang, Lohmann D, Kuntz M. Aeroacoustic Calculation of A Transonic Propeller By Using Kirchhoff Method[J]. Journal of Aerospace Power, 1999, 14(3): 285-288 (in Chinese)
[18] 李晓东, 孙晓峰, 胡宗安. 一种螺旋桨的气动声学设计与实验验证[J]. 航空动力学报, 1991, 6(4): 317-319 Li Xiaodong, Sun Xiaofeng, Hu Zongan. Aeroacoustical Modification of A Propeller[J]. Journal of Aerospace Power, 1991, 6(4): 317-319 (in Chinese)
[19] 项松, 张利国, 佟胜喜, 等. 一种高效率螺旋桨设计方法[J]. 航空动力学报, 2015, 30(1): 136-141 Xiang Song, Zhang Liguo, Tong Shengxi, et al. A Design Method for High Efficiency Propeller[J]. Journal of Aerospace Power, 2015, 30(1): 136-141 (in Chinese)
[20] 刘远强, 郭金锁, 项松, 等. 基于片条理论的螺旋桨性能计算[J]. 沈阳航空航天大学学报, 2013, 30(1): 43-46 Liu Yuanqiang, Guo Jinsuo, Xiang Song, et al. Aerodynamic Performances Calculation of Propellers Based on Standard Strip Analysis[J]. Journal of Shenyang Aerospace University, 2013, 30(1): 43-46 (in Chinese) |
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