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风洞模型支杆系统设计及振动主动控制 被引量:2

Design of Sting and Active Control of Vibration in Wind Tunnel
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摘要 研究了悬臂梁支撑系统在强流场环境下的振动抑制问题,并且基于跨声速实验设备中的模型支杆实际振动情况,采用压电陶瓷作为执行器设计了一套抑振器系统。对模型支杆进行了设计,对抑振器的轴向及周向安装位置进行了优化,以获得最佳的抑振器输出性能。基于PD控制算法,搭建了一套实验室模拟系统,在模型自由端施加加速度振幅为0.5 g,1.3 g,2 g的激励,实验结果表明,剩余振幅比为12%,10%,26%,取得了很好的振动抑制效果。 In this paper, the vibration suppression of cantilever-beam support system under strong flow field is studied, and piezoelectric ceramic is used as actuator to design a set of vibration suppressor system, based on the actual vibration condition of the model support system in transonic facility. The model support sting is redesigned, and the axial and circumferential installation position of the active vibration damper is optimized, so that the output performance of the active vibration damper is the best.Based on the PD control algorithm, a laboratory simulation system is set up, and the excitations with acceleration amplitudes of 0.5g, 1.3g, and 2g are applied to the free end of the model. The experimental results show that the residual amplitude ratios are 12%, 10%, and 26%. A good vibration suppression effect is achieved.
作者 鲁继文 刘巍 刘昱 贾振元 刘惟肖 张家昆 姜雨丰 LU Jiwen;LIU wei;LIU Yu;JIA Zhenyuan;LIU Weixiao;ZHANG Jiakun;JIANG Yufeng(Key Laboratory for Precision and Non-Traditional Machining Technology of the Ministry of Education,Dalian University of Technology,Dalian 116024,China;AVIC Aerodynamics Research Institute,Shenyang 110034 China)
出处 《计测技术》 2018年第4期10-16,共7页 Metrology & Measurement Technology
基金 中航工业产学研专项(cxy2014DLLG23)
关键词 振动分析 支杆设计 强度校核 振动控制 vibration analysis sting design intensity check vibration control
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  • 1杨恩霞.大攻角张线-尾撑组合支撑设备的设计[J].机械工程师,2005(7):113-114. 被引量:6
  • 2陈卫东,邵敏强,杨兴华,路波,徐庆华.跨声速风洞测力模型主动减振系统的试验研究[J].振动工程学报,2007,20(1):91-96. 被引量:20
  • 3胡志强,法庆衍,洪宝林等.随机振动试验应用技术[M].北京:中国计量出版社,2003.
  • 4Tyler C. Evaluation of rapid prototyping technologies for use in wind tunnel model fabrication[R]. AIAA2005- 1301.
  • 5Christensen P F. Methods for increasing wind tunnel testing effectiveness[R]. AIAA2008-1655.
  • 6Aghanajafi C. Intesation of three- dimensional printing technology for wind- tunnel model fabrication[J]. Journal of Aircraft, 2010,47(6).
  • 7Ulrich A .Remotely controlled movable surface motorization of an industrial used wind tunnel model[R] AIAA2010-4338.
  • 8Paryz R .Recent developments at the NASA Langley research center national transonic facility[C]. The 113th Supersonic Tunnel Association, International, May 2010.
  • 9Ivanco T G .Validation of the Lockheed Martin morphing concept with wind tunnel testing[R]. AIAA 2007-2235.
  • 10梁鉴,张卫国,王勋年,杜进宏.4m×3m风洞无人机模型振动抑制系统研制[J].实验流体力学,2007,21(4):65-70. 被引量:7

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