起重机二级桁架下皮带的扭转

Yu. Markina
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引用次数: 0

摘要

起重机沿其移动的起重机二级桁架下带是由薄壁箱型材制成的。起重机的最大局部集中力偏心施加在薄壁焊接箱形桁架的下带上,导致其产生约束扭转。吊车二级桁架的计算方法没有考虑下带的扭转和腹杆的水平弯曲。起重机沿其移动的下皮带的设计方案是跨度等于起重机副桁架跨度的梁。事实上,扭转时皮带的功与梁的功不同。 这项工作的目的是评估腹板和上皮带在扭转期间对下皮带运行的影响,并明确计算下皮带的方法。研究了腹板对下皮带角度延展性和扭矩的影响。考虑了皮带和整个起重机二级桁架的各种刚度比。提出了计算扭转的皮带设计方案--在腹板交界处的梁角度弹性支撑。采用了弹性支撑刚度的确定公式。根据所提出的方法确定的下皮带弯矩与整个起重机二级桁架的杆件设计方案数值计算结果的误差不超过 2%。考虑到扭转分量,下带的应力是通过分析确定的。使用壳体有限元和全尺寸试验对结果进行了数值验证。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
TORSION OF LOWER BELT OF CRANE SECONDARY TRUSS
The lower belt of the crane secondary truss, along which the crane moves, is made of a thin-walled box profile. The largest local concentrated crane forces applied with eccentricity to the lower belt of truss made of thin-walled welded box cause its restrained torsion. The calculation method of the crane secondary truss does not consider the inclusion in the work of the lower belt for torsion and horizontal bending of the webs. A beam with a span equal to the span of the crane secondary truss is taken as the design scheme of the lower belt along which the crane moves. In fact, the work of the belt during torsion is different from the work of the beam. The objectives of the work are to assess the impact on the operation of the lower belt during torsion of the webs and the upper belt and to clarify the methodology for calculating the lower belt. The study of the influence of webs on the angular malleability and torque of the lower belt has been carried out. Various ratios of the stiffness of the belt and the entire crane secondary truss are considered. The design scheme of the belt for the calculation of torsion is proposed – a beam angular elastic supports at the points of junction of the webs. The formula for determining the stiffness of elastic supports has been adopted. The error in determining the bending moments in the lower belt according to the proposed method relative to the results of numerical calculation of the rod design scheme of the entire crane secondary truss does not exceed 2%. The stresses in the lower belt, considering the torsion component, are analytically determined. The results were verified numerically using shell finite elements and a full-scale examination.
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