留言板

尊敬的读者、作者、审稿人, 关于本刊的投稿、审稿、编辑和出版的任何问题, 您可以本页添加留言。我们将尽快给您答复。谢谢您的支持!

姓名
邮箱
手机号码
标题
留言内容
验证码

直升机减振的旋翼桨叶优化设计研究综述

向锦武 郭俊贤 张晓谷

向锦武, 郭俊贤, 张晓谷等 . 直升机减振的旋翼桨叶优化设计研究综述[J]. 北京航空航天大学学报, 2001, 27(1): 32-35.
引用本文: 向锦武, 郭俊贤, 张晓谷等 . 直升机减振的旋翼桨叶优化设计研究综述[J]. 北京航空航天大学学报, 2001, 27(1): 32-35.
XIANG Jin-wu, GUO Jun-xian, ZHANG Xiao-guet al. An Overview of Rotor Blades Optimum Design for Helicopter Vibration Reduction[J]. Journal of Beijing University of Aeronautics and Astronautics, 2001, 27(1): 32-35. (in Chinese)
Citation: XIANG Jin-wu, GUO Jun-xian, ZHANG Xiao-guet al. An Overview of Rotor Blades Optimum Design for Helicopter Vibration Reduction[J]. Journal of Beijing University of Aeronautics and Astronautics, 2001, 27(1): 32-35. (in Chinese)

直升机减振的旋翼桨叶优化设计研究综述

详细信息
    作者简介:

    向锦武(1964-),男,湖南岳阳人,教授,100083,北京.

  • 中图分类号: V 214.3+3

An Overview of Rotor Blades Optimum Design for Helicopter Vibration Reduction

  • 摘要: 围绕降低直升机振动水平的旋翼桨叶减振优化设计,对国内外这方面研究进展情况作了综述;着重讨论了降低旋翼激振力减振优化设计分析中的几个主要问题,包括桨叶减振优化设计途径与目标,桨叶优化设计中的分析模型,优化设计方法及灵敏度分析技术,以及桨叶优化减振设计研究的最新发展方向和需进一步研究的问题等.

     

  • [1] 张晓谷. 直升机动力学设计[M]. 北京:航空工业出版社,1995.1~6. [2] Gabel R.When helicopter smooth surpasses jet smooth-keynote address. In:Specialists Meeting on Helicopter Vibration. Hartford:American Helicopter Society,1981. 1~10. [3] Friedman P P.Application of modern structural optimization methods to vibration reduction in rotorcraft[J]. Vertica,1985, 9(4):363~376. [4] Peters D A,Rossow M P,Korn A,et al. Design of helicopter rotor blades for optimum dynamic characteristics[J]. Journal of Compt & Math with Appl, 1986,12(1):85~109. [5] 程耿东,顾元宪,候汝良,等.旋翼桨叶的频率敏度分析与调频及优化设计[J].直升机技术, 1983,3(3):21~39. [6] 向锦武,张呈林,王适存.低振动旋翼桨叶的动力学优化设计[J].航空动力学报,1996,11(2):125~128. [7] Taylor R B. Helicopter vibration reduction by rotor blade modal shaping. In: Proceedings of the 38th Annual Forum. Maryland:American Helicopter Society, 1982. 223~229. [8] Pritchard J I, Adelman H M. Optimal placement of tuning masses for vibration reduction in helicopter rotor blades[J]. AIAA Journal,1990, 28(2):233~239. [9] Bennett R L. Optimum structural design. In:Proceedings of the 38th Annual Forum. Maryland:American Helicopter Society,1982. 121~129. [10] Straub F K,Callahan C B,Culp J D.Rotor design optimization using a multidisciplinary approach[J].Journal of Structural Optimization, 1992, 5(1-2):70~75. [11] Hodges D H,Dowell E H. Nonlinear equations of motion for elastic bending and torsion of twisted non-uniform blades. NASA-TN-D-7818,1974. [12] Rosen A,Friedmann P P. Nonlinear equations of equilibrium for elastic helicopter or wind turbine blades undergoing moderate deformation. UCLA-ENG-7718,1977. [13] Refield L W. Design analysis methodology for composite rotor blades. AFWAL-TR-85-3094, 1985. [14] Giavotto V,Borri M. Anisotropic beam theory and applications[J]. Computer & Structure, 1983,16(1-4):403~413. [15] 向锦武,张晓谷,赵 翔. 直升机旋翼桨叶剖面刚度的有限元计算[J].航空动力学报,1998,13(2):206~208. [16] Hodges D H. A mixed variational formulation based on exact intrinsic equations for dynamics of moving beam[J]. International Journal of Solids and Structures, 1990,26(11):1253~1273. [17] Friedmann P P, Shanthakumaran P. Optimum design of rotor blades for vibration reduction in forward flight[J]. Journal of American Helicopter Society,1984, 29(4):334~342. [18] Kim K C, Chopra I. Aeroelastic analysis of helicopter rotor blades with advanced tip shapes. AIAA-No-1118, 1990. [19] Ganguli R, Chopra I. Aeroelastic optimization of a helicopter rotor to reduce vibration and dynamic stresses[J].Journal of Aircraft, 1996, 12(4):334~342. [20] Bielawa R L. Techniques for stability analysis and design optimization with dynamic constraints on non-conservative linear systems. In:Proceedings of the 12th AIAA/ASME/ SSDM Conference. Maryland:AIAA/ASM, 1971.334~327. [21] Miura H. Application of numerical optimization methods to helicopter design problems-a survey[J]. Vertica, 1985,9(2):141~154. [22] Davis M W, Weller W H. Applications of design optimization techniques to rotor dynamics problems[J]. Journal of American Helicopter Society,1988,33(3):42~50. [23] Adelman H M, Mantay W R. Integrated multidisciplinary design optimization of rotorcraft[J]. Journal of Aircraft,1991, 28(1):67~77. [24] Lim J W, Chopra I. Aeroelastic optimization of helicopter rotor using an efficient sensitivity analysis[J]. Journal of Aircraft,1991, 28(1):123~129. [25] Straub F K, Ealey M A, Schelky L McD. Application of smart material to helicopter rotor active control. A97-3160508-31,1997. [26] Nagashima T. The state of the art of active control technology for helicopter vibration reduction (survey). A96-3287508-31,1995.
  • 加载中
计量
  • 文章访问数:  2982
  • HTML全文浏览量:  196
  • PDF下载量:  1633
  • 被引次数: 0
出版历程
  • 收稿日期:  1999-12-21
  • 网络出版日期:  2001-01-31

目录

    /

    返回文章
    返回
    常见问答