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Buckling of insulated irregular transition flue gas ducts under axial loading

机译:绝缘不规则过渡烟气管道在轴向载荷下的屈曲

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摘要

Finite element buckling analysis of insulated transition flue ducts is carried out to determine the critical buckling load multipliers when subjected to axial compression for design process. Through this investigation, the results of numerical computations to examine the buckling strength for different possible duct shapes (cylinder, and circular-to-square) are presented. The load multipliers are determined through detailed buckling analysis taking into account the effects of geometrical construction and duct plate thickness which have great influence on the buckling load. Enhancement in the buckling capacity of such ducts by the addition of horizontal and vertical stiffeners is also investigated. Several models with varying dimensions and plate thicknesses are examined to obtain the linear buckling capacities against duct dimensions. The percentage improvement in the buckling capacity due to the addition of vertical stiffeners and horizontal Stiffeners is shown to be as high as three times for some cases. The study suggests that the best location of the horizontal stiffener is at 0.25 of duct depth from the bottom to achieve the maximum buckling capacity. A design equation estimating the buckling strength of geometrically perfect cylindrical-to-square shell is developed by using regression analysis accurately with approximately 4% errors.
机译:进行了隔热过渡烟道的有限元屈曲分析,以确定在设计过程中受到轴向压缩时的临界屈曲载荷倍数。通过这项调查,提出了数值计算的结果,以检查不同可能的管道形状(圆柱和圆形至正方形)的屈曲强度。通过详细的屈曲分析来确定载荷乘数,其中要考虑几何结构和风管板厚度对屈曲载荷有很大影响的影响。还研究了通过增加水平和垂直加劲肋来增强此类管道的屈曲能力。研究了具有不同尺寸和板厚的几种模型,以获得相对于管道尺寸的线性屈曲能力。在某些情况下,由于添加了垂直加劲肋和水平加劲肋,导致屈曲能力的提高百分比高达三倍。研究表明,水平加劲肋的最佳位置是从底部到导管深度的0.25,以实现最大屈曲能力。通过使用具有大约4%的误差的精确回归分析,开发了估算几何完美圆柱体到方形壳体屈曲强度的设计方程。

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