期刊文献+

Research of an Active Tunable Vibration Absorber for Helicopter Vibration Control 被引量:6

用于直升机振动控制的主动调谐式吸振器研究(英文)
在线阅读 下载PDF
导出
摘要 Significant structural vibration is an undesirable characteristic in helicopter flight that leads to structural fatigue, poor ride quality for passengers and high acoustic signature. Previous Individual Blade Control (IBC) techniques to reduce these effects have been hindered by electromechanical limitations of piezoelectric actuators. The Smart Spring is an active tunable vibration absorber using IBC approach to adaptively alter the 'structural impedance' at the blade root. In this paper, a mathematical model was developed to predict the response under harmonic excitations. An adaptive notch algorithm was designed and implemented on a TMS320c40 DSP platform. Reference signal synthesis techniques were used to automatically track the shifts in the fundamental vibratory frequency due to variations in flight conditions. Closed-loop tests performed on the proof-of-concept hardware achieved significant vibration suppression at harmonic peaks as well as the broadband reduction in vibration. The investigation verified the capability of the Smart Spring to suppress multiple harmonic components in blade vibration through active impedance control. Significant structural vibration is an undesirable characteristic in helicopter flight that leads to structural fatigue, poor ride quality for passengers and high acoustic signature. Previous Individual Blade Control (IBC) techniques to reduce these effects have been hindered by electromechanical limitations of piezoelectric actuators. The Smart Spring is an active tunable vibration absorber using IBC approach to adaptively alter the 'structural impedance' at the blade root. In this paper, a mathematical model was developed to predict the response under harmonic excitations. An adaptive notch algorithm was designed and implemented on a TMS320c40 DSP platform. Reference signal synthesis techniques were used to automatically track the shifts in the fundamental vibratory frequency due to variations in flight conditions. Closed-loop tests performed on the proof-of-concept hardware achieved significant vibration suppression at harmonic peaks as well as the broadband reduction in vibration. The investigation verified the capability of the Smart Spring to suppress multiple harmonic components in blade vibration through active impedance control.
出处 《Chinese Journal of Aeronautics》 SCIE EI CAS CSCD 2003年第4期203-211,共9页 中国航空学报(英文版)
关键词 helicopter vibration control active tunable vibration absorber smart structure helicopter vibration control active tunable vibration absorber smart structure
  • 相关文献

参考文献12

  • 1中国航空技术研究院.直升机动力学手册[M].北京:航空工业出版社,1991..
  • 2Kretz M, Larche M. Future of helicopter rotor control [J].Veritieal,1980, 4(1) :3-22.
  • 3Chen Y, Gu Z Q, Tao B Q, et al. Development and testing of an adaptive rotor system based on solid actuation and noncontact signal transmission technology [A]. In: 22nd Conference of International Council of Aeronautics Science[C].St Louis: Mira Digital Publishiruz,2000.
  • 4Prechtl E F, Hall S R. Closed-loop vibration control experiments on a rotor with blade mounted actuation [A]. In:41st AIAA Structures, Structural Dynamics and Materials Conference [C]. Atlanta: AIAA, 2000.
  • 5Straub F K, et al. Smart material actuated rotor technology- SMART [A]. 41st AIAA Structures, Structural Dynamics and Materials Conference[C]. Atlanta: AIAA, 2000.
  • 6Rodgers J P, Hagood N W. Hover testing of 1/6 Mach-Scale CH-47D blade with integral twist actuation [A]. In:9th International Conference on Adaptive Structures and Technology[C]. Cambridge: AIAA, 1998.
  • 7Shin S J, Cesnik C E S, Wilbur M L. Dynamic response of active twist rotor blades [A]. In: 41st AIAA Structures,Structural Dynamics and Materials Conference[C]. Atlanta:AIAA, 2000.
  • 8Wickramasinghe V K, Hagood N W. Performance characterization of active fiber composite actuators for helicopter rotor blade applications [A]. SPIE 9th Smart Structuresand Materials Symposium [C]. San Diego: SPIE, 2002.
  • 9Nitzsche F, Grewal A, Zimcik D G. Structural Component Having Means for Actively Varying its Stiffness to Control Vibrations [P]. US: 5973440, 1999.
  • 10Nitzsche F. Aeroelastie analysis of a helicopter rotor blade with active impedance control at the root [J]. Canadian Aeronautics and Space Journal, 2001, 47(1): 7-16.

同被引文献81

  • 1Sun Dongye Qin Datong Wang HongyanState Key Laboratory of Mechanical Transmission, Chongqing University, Chongqing 400044, China.CONTROL STRATEGY OF A PARALLEL HYBRID CAR WITH A METAL BELT-PLANETARY GEAR CONTINUOUSLY VARIABLE TRANSMISSION SYSTEM[J].Chinese Journal of Mechanical Engineering,2002,15(3):199-203. 被引量:5
  • 2Zhu Fumin,Li Wanli,Maropoulos P G.TOLERANCE ANALYSIS OF A PLANETARY GEAR REDUCER UNDER CAD CIRCUMSTANCE[J].Chinese Journal of Mechanical Engineering,2005,18(3):342-345. 被引量:11
  • 3刘亚民.摩擦力与摩擦系数的几点性质[J].呼伦贝尔学院学报,2006,14(4):67-68. 被引量:17
  • 4Wickramasinghe V K, Zimcik D G, Chen Y, et al. Smart Spring-An actively tunable vibration absorber designed to control aeroelastic response[J]. Structural Dynamics and Materials Conference, 2003,5: 3651-3658.
  • 5Wickramasinghe V K, Chen Y, Zimcik D G, et al. Smart spring: a novel adaptive impedance control approach for active vibration suppression applications[J]. Proceedings of the SPIE - The International Society for Optical Engineering, 2004, 5390(1): 359-69.
  • 6Chen Y, Wickramasinghe V K, Zimcik D G. A novel smart spring concept for helicopter blade vibration and noise suppression[J]. Materials Science Forum,2005,475-479(3): 2095-2098.
  • 7Chen Y, Wickramasinghe V K, Zimcik D G. Smart spring impedance control algorithm for helicopter blade harmonic vibration suppression[J]. Journal of Vibration and Control, 2005,11(4): 543-60.
  • 8Chen Y, Wickramasinghe V K, Zimcik D G. Experimental evaluation of the smart spring for helicopter vibration suppression through blade root impedance control[J]. Smart Materials and Structures, 2005,14(5): 1066-74.
  • 9Wickramasinghe V K, Chen Y, Zimzik D G. Experimental evaluation of the smart spring impedance control approach for adaptive vibration suppression[J]. Journal of Intelligent Material Systems and Structures, 2008, 19(2): 171-9.
  • 10Daley S, H?t?nen J, Owens D H. Active vibration isolation in a "Smart Spring" mount using a repetitive control approach[J]. Control Engineering Practice , 2006,14(9): 991-997.

引证文献6

二级引证文献49

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部