上海交通大学学报(自然版) ›› 2014, Vol. 48 ›› Issue (02): 234-238.

• 航空、航天 • 上一篇    下一篇

柔性飞艇主气囊干湿模态分析与影响因素

陈宇峰,陈务军,何艳丽,张大旭
  

  1. (上海交通大学 空间结构研究中心,上海 200240)
     
  • 收稿日期:2013-05-28
  • 基金资助:

    国家自然科学基金项目(51278299)资助项目

Dry and Wet Modal Analysis and Evaluation of Influencing Factors for Flexible Airship Envelop

CHEN Yufeng,CHEN Wujun,HE Yanli,ZHANG Daxu
  

  1. (Space Structures Research Centre, Shanghai Jiaotong University, Shanghai 200240, China)
  • Received:2013-05-28

摘要:

为了掌握柔性飞艇无约束状态下的模态特性,以25 m平流层验证飞艇为基本分析对象,对其自振特性进行研究.根据充气膜结构的力学特点,基于柔性飞艇主气囊初始形状,通过充气压力静力非线性分析得到充气平衡形态位形和应力,利用兰索斯法进行模态数值分析.分析表明,影响柔性飞艇模态特性的主要因素为:壳单元与膜单元模型、拼接缝、不均匀质量分布、内外压差、尺寸、飞艇周围空气附加质量,且最后三者为重要影响因素;壳单元和膜单元模型频率相近且振型一致.对柔性平流层飞艇结构设计具有参考价值.
 
 

关键词: 平流层飞艇, 主气囊, 干模态, 湿模态, 空气附加质量

Abstract:

In order to grasp the unconstrained modal characteristics of the flexible airship envelop, the natural vibration performance was investigated thoroughly for a 25 m long stratospheric demonstration airship. The flexible airship envelop features is a freefloating inflatable membrane structure. Based on the mechanical nature of pneumaticstressed membrane structures, the deformed equilibrium shape and stress were computed from the initial geometry configuration, subjected the inflated air pressure through nonlinear structural analysis. The block Lanczos method was employed for modal analysis. The main influencing factors were evaluated thoroughly for modal behavior, including shell element and membrane element, pressure, geometry size, weld seam, nonuniform distributed mass and the added atmosphere mass. The numerical models of membrane and shell element have close natural frequency and identical modal shape. The airadded mass, pressure and geometry size are the key factors to govern the modal performance. This paper can provide reference for structural engineering design of stratospheric airship.
 

Key words: stratospheric airship, airship envelop, dry mode, wet mode, air added mass

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