土木建筑工程

大型复杂钢结构球型铰支座的力学性能——轴压荷载下的转动性能

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  • 1. 华南理工大学 土木与交通学院,广东 广州 510640; 2. 华南理工大学 亚热带建筑科学国家重点实验室, 广东 广州 510640; 3. 东南大学 土木工程学院,江苏 南京 210096
石开荣(1978-),男,博士,副教授,主要从事预应力钢结构、大跨度空间结构研究. E-mail:krshi@ scut. edu. cn

收稿日期: 2019-01-02

  修回日期: 2019-03-30

  网络出版日期: 2019-08-01

基金资助

国家自然科学基金资助项目(11673039);华南理工大学亚热带建筑科学国家重点实验室开放课题(2019ZB27)

Mechanical Behaviors of Large-tonnage Complex Steel Spherical Hinged Support: Rotation Behavior Subjected to Axial Compressive Load

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  • 1. School of Civil Engineering and Transportation,South China University of Technology,Guangzhou 510640,Guangdong,China; 2. State Key Laboratory of Subtropical Building Science,South China University of Technology,Guangzhou 510640, Guangdong,China; 3. School of Civil Engineering,Southeast University,Nanjing 210096,Jiangsu,China
石开荣(1978-),男,博士,副教授,主要从事预应力钢结构、大跨度空间结构研究. E-mail:krshi@ scut. edu. cn

Received date: 2019-01-02

  Revised date: 2019-03-30

  Online published: 2019-08-01

Supported by

Supported by the National Natural Science Foundation of China(11673039)

摘要

钢结构球型铰支座具有承载能力高、传力可靠、转动灵活(万向铰)、适应节点大 位移大转角需要等优点,但在各种荷载组合作用下,支座节点受力较为复杂,且对整体结 构的受力安全有着非常重要的影响. 文中以广州白云国际机场扩建工程二号航站楼的大 吨位复杂钢结构球型铰支座为例,进行足尺原型试验及有限元模拟分析,研究其在轴压荷 载下的转动性能,并根据试验及有限元模拟结果提出了在轴压荷载下的支座转动刚度模 型,用于整体结构的精细化分析. 结果表明:试验数据与有限元模拟结果基本吻合,应力及 变形曲线的发展趋势一致;支座的实测转动力矩小于规范规定值,其转动性能满足规范和 设计要求.

本文引用格式

石开荣 潘文智 姜正荣 吕俊锋 罗斌 . 大型复杂钢结构球型铰支座的力学性能——轴压荷载下的转动性能[J]. 华南理工大学学报(自然科学版), 2019 , 47(8) : 9 -15 . DOI: 10.12141/j.issn.1000-565X.180650

Abstract

The steel spherical hinged support has the advantages of high loading capacity,reliable transfer of loads, flexible rotation with universal hinge,and allowance of large displacement and rotation angle. However,supports are in complex forced states subjected to various load combinations,which leads to the significant influence on inte- gral structural safety. Taking the large-tonnage complex steel spherical hinged support of T2 of Guangzhou Baiyun International Airport for example,the full-scale experiments and finite element simulation analysis were carried out and the rotation behavior of the support subjected to axial compressive load was studied. The rotation stiffness model of support subjected to axial compressive load was proposed for the refinement analysis of integral structure. The results show that the results of experiments and finite element simulations are similar,and the development tendency of stress and deformation of them is coincident. In addition,the actual rotational moment is less than that prescrip- tive by code and the rotation behavior is satisfied for the requirements of code and design.

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