期刊检索

  • 2024年第56卷
  • 2023年第55卷
  • 2022年第54卷
  • 2021年第53卷
  • 2020年第52卷
  • 2019年第51卷
  • 2018年第50卷
  • 2017年第49卷
  • 2016年第48卷
  • 2015年第47卷
  • 2014年第46卷
  • 2013年第45卷
  • 2012年第44卷
  • 2011年第43卷
  • 2010年第42卷
  • 第1期
  • 第2期

主管单位 中华人民共和国
工业和信息化部
主办单位 哈尔滨工业大学 主编 李隆球 国际刊号ISSN 0367-6234 国内刊号CN 23-1235/T

期刊网站二维码
微信公众号二维码
引用本文:武岳,远芳,薛龙瑞,李清朋.零弯矩型自由曲面结构找形方法[J].哈尔滨工业大学学报,2018,50(6):177.DOI:10.11918/j.issn.0367-6234.201707122
WU Yue,YUAN Fang,XUE Longrui,LI Qingpeng.Form-finding method for free-form shell structures with zero bending moment[J].Journal of Harbin Institute of Technology,2018,50(6):177.DOI:10.11918/j.issn.0367-6234.201707122
【打印本页】   【HTML】   【下载PDF全文】   查看/发表评论  下载PDF阅读器  关闭
过刊浏览    高级检索
本文已被:浏览 1889次   下载 1294 本文二维码信息
码上扫一扫!
分享到: 微信 更多
零弯矩型自由曲面结构找形方法
武岳1,远芳2,薛龙瑞3,李清朋1
(1.哈尔滨工业大学 土木工程学院,哈尔滨 150090;2.哈尔滨工业大学 建筑设计研究院,哈尔滨 150090; 3.太原万科房地产有限公司,太原030006)
摘要:
为获得受力合理且形式丰富的自由曲面结构,借鉴传统模型试验找形法的原理,提出基于动力松弛法和局部线性化法的零弯矩型自由曲面结构数值找形方法.该方法利用了零弯矩型薄壳结构与相同荷载与边界条件下的柔性膜结构具有相同形状的性质,通过膜结构来实现自由曲面结构的找形.首先采用动力松弛法确定柔性结构在不同驱动力作用下的平衡构形;然后利用局部线性化方法调整结构初始参数,实现对结构形状的精确调控,以满足建筑设计对控制点坐标的要求.利用所提方法分别对逆吊型、充气型和张拉型自由曲面进行了数值模拟分析.通过对Isler逆吊试验模型的模拟,并与实际模型的3D扫描结果进行比较,验证了方法的精确性;通过对一充气型自由曲面的模拟,证明通过多区域分步控制可实现复杂造型结构的多点精确控制;通过对一找形后的张拉型自由曲面结构进行受力分析,证明采用本文方法可获得受力合理的纯压结构.研究表明,本文方法的计算效率更高,适用范围更广,有助于实现建筑与结构设计的协调统一.
关键词:  自由曲面结构  模型实验  数值找形  动力松弛法  形状调控
DOI:10.11918/j.issn.0367-6234.201707122
分类号:TU33
文献标识码:A
基金项目:国家自然科学基金(6,2)
Form-finding method for free-form shell structures with zero bending moment
WU Yue1,YUAN Fang2,XUE Longrui3,LI Qingpeng1
(1.School of Civil Engineering, Harbin Institute of Technology, Harbin 150090, China; 2.Architecture Design and Research Institute of HIT, Harbin 150090, China; 3.Taiyuan Vanke Real Estate Limited Company, Taiyuan 030006, China)
Abstract:
To design free-form structures with reasonable mechanical behaviors and rich geometrical shapes, the principles of traditional form-finding methods by physical experiments were referred, and a numerical form-finding method for free-form structures was proposed based on the combination of the Dynamic Relaxation method and the Local Linearization method. As the zero bending moment type free-form structure has the same form with the flexible membrane structure which has the same loading distributions and boundary conditions, the form-finding of free-form shell structures can be realized by membrane structures. In the proposed method, equilibrium forms under different driving forces, such as the gravity, pneumatic pressure, pretension force, were generated by Dynamic Relaxation method, and the form-control problem aiming to meet the requirements of architectural design was explored by adjusting the initial parameters of the model using the Local Linearization method. The poposed form-finding method was applied to the inverse-hanging type shells, the pneumatic type shells and the tension type shells separately. For the inverse-hanging type shells, a model made by Isler was simulated, and the results were compared with the data by 3D scanning to verify the accuracy of the proposed method. For the pneumatic type shells, the multi-region controlling strategy was used to realize the form-finding of complicated shapes. For the tension type shells, the behaviors of a shell genertated by the form-finding method were analized to illustrate the zero bending moment feature. It can be concluded that the proposed method is more effective and applicable, which is helpful to realize the harmonious design of architecture and structure.
Key words:  free-form structures  physical experiments  form-finding  dynamic relaxation method  form-control

友情链接LINKS