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结构响应主动控制系统设计与试验验证

Design and Test Validation of the Active Control of Structural Response System
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摘要 振动控制是直升机设计的关键技术之一。本文首先介绍了如何进行结构响应主动控制(ACSR)系统的设计,然后详细说明了为此开发的ACSR系统的框架和软硬件基本组成,最后通过ACSR系统装直11进行地面试验和飞行试验,验证了该系统的可行性和抑制振动的有效性。
作者 李明强 凌爱民 虞汉文 黄斌根 孙东红
机构地区 中航工业直升机所
出处 《航空科学技术》 2012年第4期33-37,共5页 Aeronautical Science & Technology
关键词 振动控制 结构响应主动控制 直11 试验验证 vibration control, ACSR Z11, test validation
分类号 V217 [航空宇航科学与技术—航空宇航推进理论与工程]
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参考文献10

  • 1Miao W, Kottapalli S B R, Frye H M.Flight demonstration of higher harmonic control(HHC) on S-76[C]. Proceedings of the 42nd Annual Forum of the American Helicopter Society, Washington, D.C., 1986-6.
  • 2Staple A E, Wells D M. Development and testing of an active control of structural response system for the EH101 helicopter [C]. Proceedings of the 16th European Rotorcraft Forum, 1990-9.
  • 3Vignal B, Krysinski T. Development and qualification of active vibration control system for the Eurocopter EC225/725[C]. Presented at the American Helicopter Society 62st Annual Forum, 2005-6.
  • 4Teal R, Mecorvey D L, Malloy D. Active vibration suppression for the CH- 47D[C]. Presented at the 53rd Annual Forum of the American Helicopter Society, 1997 -5.
  • 5Welsh W A, Von Hardenberg P C, Von Hardenberg P W.Test and evaluation of fuselage vibration utilizing active control of structure response (ACSR) optimized to ADS-27[C]. Proceedings of the 46nd Annual Forum of the American Helicopter Society, 1990.
  • 6Goodman R K, Dr. Millott T A. Design, development, and flight testirig of the active vibration control system for the Sikorsky S-92[C]. Presented at the 56rd Annual Forum of the American Helicopter Society, 2000-5.
  • 7Welsh W, Fredrickson C, Rauch C. Flight test of an active vibration control system on the UH-60 black hawk helicopter[C].Presented at the 51rd Annual Forum of the American Helicopter Society, 1995-5.
  • 8Dr. Millott T A. Risk reduction flight test of a pre production active vibration control system for the UH- 60M[ C ]. Presented at the 59rd Annual Forum of the American Helicopter Society, 2003-5.
  • 9Wong Jonathan K. Risk reduction flight test of a pre-production active vibration control system for the MH-60S [C] . Presented at the 62rd Annual Forum of the American Helicopter Society, 2006-1.
  • 10Dynamics design characteristics of the Sikorsky X2 technology demonstrator aircraft [Z].
航空科学技术
2012年 第4期

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