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作 者:齐麟[1] 张文博 孙荣来 胡雪瀛[2] 黄信 Qi Lin;Zhang Wenbo;Sun Ronglai;Hu Xueying;Huang Xin(Airport College,Civil Aviation University of C hina,Tianjin 300300,China;Tianjin Architecture Design Institute,Tianjin 300074,China)
机构地区:[1]中国民航大学机场学院,天津300300 [2]天津市建筑设计院,天津300074
出 处:《建筑结构》2019年第23期39-43,38,共6页Building Structure
基 金:天津市教委科研计划项目(2018KJ244)
摘 要:介绍了天津滨海国际机场T 2航站楼钢屋盖的基本概况、结构特点与设计参数。计算了屋盖各分区结构的自振周期与杆件最大应力比,计算结果表明,结构设计在满足控制应力比的基础上最大程度地提高了材料的利用率。结构上、下弦杆截面的控制因素为稳定应力,而腹杆截面的控制因素为长细比,腹杆对结构的刚度贡献较大。验算了结构跨中与悬挑端的最大挠度,计算结果均满足规范要求。以1~10阶屈曲模态作为结构初始几何缺陷分布形式,计算了结构各分区的极限承载力。计算结果表明,网壳结构的最低阶屈曲模态不一定为最不利初始几何缺陷模态,应以多阶屈曲模态作为结构初始几何缺陷分布状态计算承载力,以最小值作为结构的极限承载力。The general situation,structural characteristics and the design param eters of T2 terminal building steel roof of Tianjin Binhai International Airport were introduced.The natural vibration periods of the structure and the maximum stress ratios of the members were calculated.The calculation results indicate that the materials are used most profitably on the base of the satisfaction of the controlling stress ratio in the structural design.The control factor of the upper and lower chord sections of the structure is the stable stre ss,while the control factor of the web section is the slenderness ratio,and the web contributes a lot to the rigidity of the structure.The maximum deflection of the mid span and the cantilevered end of the structure was checked,and the results met the requirements of the code.The ultimate bearing capacity of each section of the structure was calculated by taking the first to tenth order buckling modes as the initial geometric defect distribution.The results show that the lowest order buckling mode is not necessarily the most disadvantageous initial geometric imperfection mode,and the multiple buckling mode should be taken as the initial geometric imperfection distribution state to calculate the bearing capacity,and the minimum value should be taken as the ultim ate bearing capacity of the structure.
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