共轴刚性旋翼试验自动配平技术研究 |
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引用本文: | 章贵川,彭先敏,车兵辉,尹欣繁,李雷.共轴刚性旋翼试验自动配平技术研究[J].南京航空航天大学学报,2019,51(2):226-231. |
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作者姓名: | 章贵川 彭先敏 车兵辉 尹欣繁 李雷 |
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作者单位: | 中国空气动力研究与发展中心,绵阳, 621000 |
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摘 要: | 针对共轴刚性旋翼高速直升机研究的需求,对共轴刚性旋翼试验自动配平技术展开了研究。基于现有试验平台,结合共轴刚性旋翼的配平原理,参考单旋翼自动配平技术,提出了基于模糊控制的共轴刚性旋翼试验自动配平技术,并在试验中进行了考核和验证,达到了实用阶段。
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关 键 词: | 高速直升机 共轴刚性旋翼 自动配平 |
收稿时间: | 2018/11/11 0:00:00 |
修稿时间: | 2019/3/8 0:00:00 |
Research on Automatic Trim Technology of Coaxial Rigid Rotor Test |
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Institution: | China Aerodynamics Research & Development Center, Mianyang, 621000, China |
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Abstract: | In order to meet the demand of research requirements of the coaxial rigid rotor high-speed helicopter in China, the automatic trim technology of coaxial rigid rotor test is studied. Based on the existing test platform, combined with the trim principle of the coaxial rigid rotor, and referring to the automatic trim technology of the single rotor, the automatic trim technology of the coaxial rigid rotor test based on fuzzy control is proposed. It is tested and verified in the experiment and reached the practical stage. |
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Keywords: | high speed helicopter coaxial rigid rotor automatic trim |
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