关键参数对无轴导管转子气动特性的影响研究

IF 0.7 4区 工程技术 Q4 ENGINEERING, AEROSPACE Transactions of the Japan Society for Aeronautical and Space Sciences Pub Date : 2021-01-01 DOI:10.2322/tjsass.64.40
Suiyuan Shen, Qing-Hua Zhu, Jinfa Xu
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引用次数: 2

摘要

无轴风管转子是采用风管-转子-电机一体化设计而成的一种新型风管转子系统。基于非结构化滑动网格技术,研究了旋翼盘高度、叶片数、中心孔半径和叶根安装角等4个关键参数对SDR气动特性的影响。计算结果表明,随着转速的增加,推力性能逐渐改善。与传统风道转子安装在靠近风道唇处以获得最佳气动性能不同,SDR转子安装在远离风道入口处以获得最佳气动性能。此外,增加叶片数量以提高峰值推力和导管推力性能;然而,这导致了功率负载的降低。特别提款权的中心孔半径不能太小,否则会导致中央气流通过桨叶时产生过大的阻塞效应。最后,在转速一定的情况下,增大叶根安装角,推力会有较大的增加,但同时也会降低功率负荷。
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Research on the Influence of Key Parameters on the Aerodynamic Characteristics of Shaftless Ducted Rotors
The shaftless ducted rotor (SDR) is a new type of ducted rotor system built using a ducted-rotor-motor integration design. Based on unstructured sliding grid technology, the e ff ects of four key parameters, such as rotor disk height, number of blades, the center hole radius and the blade root mounting angle, on the aerodynamic characteristics of the SDR were investigated. The calculation results show that the thrust performance gradually improves as the rotational speed increases. It is di ff erent from traditional ducted rotors where the rotor is installed near the lip of the duct to obtain the optimal aerodynamic performance, the rotor of the SDR is installed away from the duct entrance to obtain the best aerodynamic performance. Additionally, the number of blades is increased to improve peak thrust and ducted thrust performance; however, this results in decreasing the power load. The central hole radius of the SDR should not be too small, as this can result in an excessive blocking e ff ect when the central air fl ow passes through the paddle. Finally, when the rotational speed is con-stant, increasing the blade root mounting angle results in a large increase in thrust, but this decreases the power load as well.
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来源期刊
CiteScore
1.80
自引率
0.00%
发文量
18
审稿时长
>12 weeks
期刊介绍: Information not localized
期刊最新文献
Acknowledgments to Associate Editors Abstracts of the Papers Published in Journal of the Japan Society for Aeronautical and Space Sciences (Vol. 71, No. 6, Dec. 2023) Abstracts of the Papers Published in Journal of the Japan Society for Aeronautical and Space Sciences (Vol. 70, No. 6, Dec. 2022) Analysis of Rotorcraft Vibration Reduction Using a Center-of-Gravity Offset Investigation on Applying an InGaN Photocathode with Negative Electron Affinity for Electric Propulsion
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