考虑气动系数试验测定的钢塔法兰连接结构活力评价

V. Erofeev, I. Samokhvalov
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摘要

考虑气动系数的计算值,在达到临界载荷和其中一个设计区域存在缺陷的情况下,对法兰组件的生存能力进行了数值研究。正在进行一项试验,以确定作用在金属塔支撑腿上的风荷载值。应力应变状态的计算采用SCAD Office和IDEA StatiCa 10.0软件进行。在计算结构核心模型中的受力后,形成装配体的三维板模型并准备进行计算。根据实验结果,将气动系数绘制成图形,用于计算节点的应力-应变状态。计算结果分析表明,在结构设计(无缺陷)状态下,承载单元和构件的安全系数为35 ~ 40%(等效应力为165 MPa)。如果带的金属结构在法兰区域存在缺陷,则在解理(缺陷孔)区域等效应力增加到247.6 MPa,因此承载余量下降到0.4%。通过对法兰连接的生存能力进行评估,发现该连接具有较高的潜在生存能力,反过来,法兰本身也能够在存在某些缺陷的情况下工作,而不会使其承载能力降低到临界水平。本文所获得的气动系数将决定这种型腔的风荷载,并可用于塔结构的风荷载设计计算。
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EVALUATION OF THE VITALITY OF A FLANGED CONNECTION WITH A STEEL TOWER STRUCTURE WITH ACCOUNT OF EXPERIMENTAL DETERMINATION OF AERODYNAMIC COEFFICIENTS
A numerical study of the survivability of the flange assembly is carried out upon reaching a critical load and in the presence of a defect in one of the design areas, taking into account the calculated values of the aerodynamic coefficients. An experiment is being carried out to determine the values of the wind load acting on the supporting legs of a metal tower. The calculation of the stressstrain state is performed using software system as SCAD Office and IDEA StatiCa 10.0. After calculating the forces in the core model of the structure, a threedimensional plate model of the assembly is formed and prepared for calculation. According to the results of the experiment, a graph was compiled with the values of aerodynamic coefficients, which were used in calculating the stressstrain state of the node. The analysis of the calculation results revealed that in the design (defectfree) state of the structure, the safety factor of the bearing units and elements is 35-40% (equivalent stresses were 165 MPa). If there is a defect in the metal structures of the belt in the region of the flange, the equivalent stresses increase to 247.6 MPa in the region of the cleavage (defective hole), thus, the margin in bearing capacity drops to 0.4%. As a result of the assessment of the survivability of the flange connection, it was revealed that the connection has a high potential survivability, in turn, the flange itself is able to work in the presence of some defects without reducing its bearing capacity to a critical level. The aerodynamic coefficients obtained in this work will determine the wind load on this type of profile and can be used in design calculations of tower structures for wind loads.
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