An optimization procedure for overhead gantry crane exposed to buckling and yield criteria

A. Ahmid, V. Lê, T. Dao
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引用次数: 2

Abstract

The current study presents a general optimization procedure that could be used in designing of various structural applications. To validate the performance of the proposed procedure, a real life application of a custom welded I-Beam gantry crane is selected. The crane is composed of three rectangular plates with the same length and different thicknesses and widths welded together by full penetration welds over the span length to form an I-Beam profile. The thicknesses and widths of plates are to be optimized to have the minimum cross section area while respecting yield, buckling, deflection and fatigue criteria. A mathematical procedure based on Timoshenko beam theory and Crane Manufacturers Association of America (CMAA) in combination with the Genetic Algorithm (GA) is presented, and a Mathcad code is implemented to find the optimal I-Beam cross section dimensions. Nine examples are introduced for 8, 12 and 20 m crane span subjected to 10, 20 and 40-toncapacities. It is noticed that the optimized I-section configurations always show narrow and thick lower flange, wider and thinner upper flange and tall and very thin web. Theupper flange local buckling and the lateral buckling limits are achieved for all nine cases, 75% of cases for the web buckling limit, about 33% of cases for the fatigue and yield limits whereas the maximum deflection constraint is never critical. The obtained results were verified using ANSYS Workbench software with a 3D Solid Finite Element model and shown good agreement, which confirms that the proposed procedure is efficient.
一种桥式龙门起重机屈曲优化程序及屈服准则
本研究提出了一种通用的优化程序,可用于各种结构的设计。为了验证所提出的程序的性能,选择了一个实际应用的定制焊接工字钢门式起重机。起重机由三个相同长度和不同厚度和宽度的矩形板组成,通过跨长度的全熔接焊接在一起,形成工字钢型材。在考虑屈服、屈曲、挠曲和疲劳标准的情况下,优化板的厚度和宽度,使其具有最小的横截面面积。提出了一种基于Timoshenko梁理论和美国起重机制造商协会(CMAA)结合遗传算法(GA)的数学程序,并实现了一个Mathcad程序来求工字梁的最优截面尺寸。介绍了8、12、20米跨度起重机在10、20、40吨承载能力下的9个实例。结果表明,优化后的工字截面结构下翼缘窄而厚,上翼缘宽而薄,腹板高而薄。在所有9种情况下,上法兰局部屈曲和侧向屈曲极限都达到了,75%的情况下达到了腹板屈曲极限,约33%的情况下达到了疲劳和屈服极限,而最大挠度约束从来都不是临界的。利用ANSYS Workbench软件对三维实体有限元模型进行了验证,结果吻合较好,验证了所提方法的有效性。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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