期刊文献+

2 MW风机叶片的结构设计及静力学分析 被引量:4

Structural designs and statics analysis of 2 MW wind turbine blade
下载PDF
导出
摘要 以2 MW风力发电机叶片为研究对象,通过Matlab中的优化函数fmincon对风机叶片的关键参数(弦长、扭角、轴向和周向因子)进行优化.采用UG建模,导入ABAQUS分析软件,将叶片分为叶片根部、主梁、前缘、后缘、腹板5个部分分区域铺层后,对其施加载荷进行静力学分析,分析不同部位应力和应变规律,同时对叶根部位的复合材料层间力进行分析.结果表明:叶片根部为应力最大部位,最大变形部位为叶片端部;-45°铺层的层间应力最大,而且应力随铺设角度的不同呈现出周期性变化.通过对叶片进行静力学分析和层间力分析,能够对叶片铺层设计提供可靠的依据. Here 2 MW wind turbine blade is selected as the research object. The optimization function of fmincon in Matlab is used to optimize the fan blade key parameters, including the chord length, torsion angle, axial and circumferential factors. Imported UG Modeling to ABAQUS, The blade is divided into five parts:the blade root, the main beam, the leading edge, the trailing edge, and the web. After laminated, statics analysis is performed by applying the loading. The stress and strain analysis of different parts of turbine blade suggested that blade root possesses the maximum stress and blade end possesses the maximum deformation degree. Composite interlaminar stress analysis of the blade root found that -45° layer of interlaminar stress is the largest, and stress showed cyclical changes with the laying Angle. Through the static analysis and interlaminar stress analysis of the blade, a solid basis for the blade design can be established.
出处 《材料科学与工艺》 EI CAS CSCD 北大核心 2017年第3期69-76,共8页 Materials Science and Technology
基金 机械制造系统工程国家重点实验室开放课题研究基金资助项目(sklms2014006)
关键词 风力发电机叶片 Matlab 铺层设计 静力学分析 层间力 blade Matlab laminate statics analysis force between the layers
  • 相关文献

参考文献3

二级参考文献30

  • 1杜善义.先进复合材料与航空航天[J].复合材料学报,2007,24(1):1-12. 被引量:1022
  • 2I. G NIKOLAOU, E S POLITIS, P K CHAVIAROPOU- LOS. Modeling the flow Around Airfoils Equipped with Vortex Generators Using a Modified 2D Navier - Stokes solver[ J ]. Journal of Solar Energy Engineering, 2005, 127:223-233. [9 [1.
  • 3陈丁刚,屈本宁,赵燕萍.一新型立轴风力机直叶片翼型气动特性数值模拟[J].科学技术与程,2011,2(11):423-425.
  • 4Nathan Logsdon. A procedure for numerically analy- zing airfoils and wing sections [ D ]. The Faculty of the Department of Mechanical & Aerospace Engineering U- niversity of Missouri - Columbia,2006.
  • 5N. Zehnder, P. Ermanni. A methodology for the global optimization of laminated composite structures [ J ]. Composite Structures, 2006, (72) :311-320.
  • 6LIU Bo yanga, T. Haftka, A. Akgtin, Mehmeta. Permutation genetic algorithm for stacking sequence design of composite laminates [ J ]. Computer Methods in Applied Mechanics and Engineering, 2000, 186:357-372.
  • 7Ching-Chieh, Lin. Ya-Jung Lee. Stacking sequence optimization of laminated composite structures using genetic algorithm with local im- provement[ J ]. Composite Stmctures ,2004, ( 63 ) :339-345.
  • 8Soremekun G, Gurdal Z, Haftka RT. Watson LT. Composite laminate design optimization by genetic algorithm with generalized elitist selec- tion[ J ]. Computer Structure ,2001,79 : 131-143.
  • 9Sargent PM, Ige DO, Ball RN. Design of laminate composite lay ups using genetic algorithm [ J ]. Engineer Computer, 1995,11:59-69.
  • 10Lin CC, Lee YJ. Stacking sequence optimization of laminated compos- ite structures using genetic algorithm with local improvement [ J ]. Computer Structure,2004,63 : 339 -345.

共引文献36

同被引文献42

引证文献4

二级引证文献8

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