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为实现仓储的自动化,研究了巷道堆垛机对通用托盘的自动存取。对仓储作业中的巷道堆垛机进行方案设计,并利用单片机来控制巷道堆垛机的行走、升降、上架和下架、取货和放货等作业。通过试验验证了单片机能够对巷道堆垛机进行有效控制,实现了巷道堆垛机对通用托盘的自动存取。单片机控制所需设备简单,易于维护,为后续研究仓储作业自动化提供了依据。 相似文献
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旋转关节型堆垛机的运动轨迹分析 总被引:2,自引:0,他引:2
堆垛机是物流设备之一,在物流工程中占有重要地位.文章介绍了4自由度堆垛机的结构特点,通过示教再现作业和运动轨迹规划,对堆垛机的动作进行了分析研究. 相似文献
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双立柱巷道堆垛机水平行走加速度达到1.5m/s2时,堆垛机在启动和停止时产生很大的惯性力,需要研究分析堆垛机结构受力以验证其是否符合强度要求.文章以某型号双立柱堆垛机为基础,建立高速高加速堆垛机金属结构模型并对其进行合理简化,运用经验公式和应用Ansys软件对堆垛机高速运行时的堆垛机结构强度进行计算和有限元分析,并分析比较其结果.合理简化了高加速堆垛机结构模型,得到了堆垛机结构的应力及变形云图,得到堆垛机立柱最大变形量和最大应力值;验证了堆垛机立柱根部受到不对称交变应力,堆垛机运行时立柱危险截面在发生运行方向前立柱和下横梁的交界处.文章所研究堆垛机结构满足高速高加速运动时的结构强度要求,为研究高速高加速堆垛机提供重要依据. 相似文献
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《热加工工艺》2016,(15)
建立了55钢铸坯堆垛过程热-力耦合数学模型,并对计算结果进行了验证。分析了不同堆垛条件(堆垛初始温度、堆垛高度和铸坯宽度)对铸坯温度和应力的影响。研究表明,堆垛顶部铸坯冷却速度最快。堆垛铸坯温度高于55钢相变温度(Ar_3、Ar_1温度分别为755℃和690℃)时,中间铸坯温度出现一平台,堆垛有利于缓解铸坯内部热应力和相变应力。随堆垛高度和铸坯宽度增加铸坯冷却速度先是降低较快,而后变化不大。堆垛顶部和底部铸坯在堆垛过程中受到的是拉应力,中间铸坯为压应力。堆垛铸坯表面应力大,应力不均匀是铸坯产生裂纹、变形等质量问题的原因。根据以上研究结果,建议在堆垛铸坯表面覆盖一层保温罩,以减小表面热损失和55钢铸坯表面应力;不在55钢相变温度范围进行堆垛和拆垛操作;另外,铸坯堆垛高度应与铸坯宽度相匹配。 相似文献
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针对单立柱堆垛机结构受力复杂,刚度要求高等特点,文章运用有限元分析方法对单立柱堆垛机进行建模及静力学分析,并对单立柱堆垛机截面尺寸进行优化设计,使优化后立柱刚度提高40%左右,达到了在安全范围内降低了制造成本,提高了堆垛机的工作性能和使用寿命。 相似文献
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This article describes the initial analysis underlying the design of a core module consisting of a 1 to 3 kW solid oxide fuel
cell (SOFC) stack and a radiant air preheater (RAP) module. The design and testing of three SOFC stack/RAP modules was part
of a California Energy Commission-sponsored project with the Gas Technology Institute. The objective of the design was to
improve the thermal management of an SOFC system through radiant heat transfer from the stack walls to adjacent air preheater
panels. The testing of this and subsequent modules has suggested that use of the radiation-based approach significantly improved
the management of stack-generated heat.
This paper was presented at the ASM Materials Solutions Conference & Show held October 18–21, 2004 in Columbus, OH. 相似文献
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Interlayer gap formation during through-hole drilling in stacked structures is a common problem in large assembly operations. The resulting interfacial burrs and non-coaxial stacked holes deteriorate the machining quality and increase the overall assembly time and costs. This study presents both experimental work and theoretical analysis to understand the interlayer gap formations and non-coaxiality occurrences in the drilling of stacked structures of broad skins and narrow stringers, which imitate typical structures of large assemblies. First, some stack drilling experiments are specially designed and are performed to observe that the stacked holes are non-coaxial in a regular fashion by measuring the hole diameters of the upper layer, lower layer and interface. Then, a simplified mechanical model of the stacks is built in 2-D to study how the interlayer gaps and non-coaxiality are formed during stack drilling. Through quantitative analysis based on the simplified model, it is noted that the stack stiffness, drilling thrust force and pressing force have important impact on the interlayer gaps and non-coaxiality. Finally, finite element methods are adopted to present the deformations in 3-D. The calculation results agree with the theoretical explanations for non-coaxiality given by the analytical simplified model. In addition, the beneficial effects of the fasteners and ribs are discussed based on the calculation results, and thus, they could contribute to proposals for better designs for stack drilling. 相似文献
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M. Yu. Belomyttsev A. I. Laptev I. P. Ezhov S. S. Chertov 《The Physics of Metals and Metallography》2006,101(4):397-403
The effect of thin tungsten and molybdenum layers, which were applied onto powder particles of intermetallic compound NiAl or its alloys with Hf and Nb before their pressing, on the hot strength and short-time creep strength of compact samples obtained from such granules has been studied. Such materials are proposed to be called composite materials (CM) with a honeycomb structure. Miniature samples in the form of small cylinders 5 mm in diameter and 5–8 mm in height were tested for compression at 1000–1300°C in air and for creep upon compression at 1050, 1110 and 1210°C in a vacuum. Alloying NiAl with hafnium or niobium increases the hot strength of the alloys by a factor of 1.4–3.7; the formation of honeycomb structure increases this characteristic by a factor of 1.6–3.6 at 1000°C; with increasing test temperature to 1300°C, the effect of solid-solution strengthening decreases to values typical of pure NiAl (σy = 7–12 MPa), and the effect of the honeycomb structures increases to σ y CM / σ y NiAl 6–7 at σ y CM = 50–80 MPa. The creep strength characteristics of the CM σ 1% h/y and σ 10% h/y at all test temperatures are higher by a factor of 1.5–2.4 than those of NiAl and its alloy with Hf; they are as high as σ 1% h/1210 = 40.4 MPa and σ 10% h/1210 = 61.3 MPa for the NiAl + W(1 μm) CM and σ 1% h/1210 = 17.7 MPa and σ 10% h/1210 = 26.3 MPa for NiAl. For the composite material with a honeycomb structure, the attained gain in the working temperature relative that of the nonstrengthened NiAl is ~ 160 K. 相似文献