航空学报 > 1992, Vol. 13 Issue (9): 516-521

复合材料桨叶振动特性分析的一种新方法

王荇卫1, 蔡慧莲1, 王寿梅2   

  1. 1. 江西省景德镇市825信箱22分箱 景德镇 333001;2. 北京航空航天大学固体力学所 北京 100083
  • 收稿日期:1991-11-24 修回日期:1992-02-20 出版日期:1992-09-25 发布日期:1992-09-25

A NEW APPROACH TO ANALYSING THE VIBRATION CHARACTERISTICS OF COMPOSITE BLADES

Wang Xing-wei1, Cai Hui-lian1, Wang Shou-mei2   

  1. 1. Box825-22 Jingdechen, Jiangxi, 333001;2. Research Center of Solid Mechanics, Beijing Universily of Aeronautics and Astronautics, Beijing, 100083
  • Received:1991-11-24 Revised:1992-02-20 Online:1992-09-25 Published:1992-09-25

摘要: 本文研究了复合材料桨叶振动特性的分析方法。基于连续介质力学理论,提出了一个新的等参曲梁单元,详细推导了梁上任意一点的形状函数,讨论了复杂翼型剖面的积分技术。算例表明,本文的计算结果与实验结果非常吻合。

关键词: 桨叶, 复合材料, 振动, 曲梁

Abstract: The method for analysing the vibration characteristics of composite blades is presented. Based on the continuum mechanics theory, a new isoparametric curve beam element is set up. The shape functions of every point on the beam are derived in detail and the integral techniques of complex aerofoil are discussed. The new element can model the cross section and the plyment of composite. The calculation time will be widely reduced if this element is used to analyse the vibration characteristics and response of blades. Certainly the new element is fit for the analysis of the other thin-walled structures. Numeral examples show that the results are coincident with the test.

Key words: blade, composite, vibration, curve beam