Prediction of methane adsorption content in continental coal-bearing shale reservoir using SLD model

Shale gas, as an important unconventional resource, has drawn global attention. It is mainly composed of adsorption gas and free gas. Adsorption gas content could play an important guiding role on both the selection of favorable perspective area and the exploration and exploitation of shale gas resources. In order to accurately measure adsorption gas content, a new approach was established to predict the adsorption isotherm of methane on shale. Based on the simplified local-density (SLD) method, both the adsorption isotherms of illite, illite/smectite mixed-layer, cholorite and type III kerogen and the total shale rock could be well fitted. The fitting results show good coincidences with the true experimental test data, which proves the method is reasonable and dependable and the prediction results are effective and credible. In addition, the good simulation results show that the SLD parameters can reflect the pore structure characteristics and corresponding adsorption characteristics of the shale samples, which can be used for the quantitative characterization of shale pore system.     

柔性桩沉降可靠性的简化分析公式

本文提出了结合分层的剪切位移法、摄动法和随机场理论来计算柔性桩沉降可靠度的简化方法，并用随机有限元和蒙特卡洛模拟法对此简化模型的精度进行了对比分析，分析结果表明该方法计算简便，精度较高。通过算例发现，在土的变形模量为小变异的情况下，其概率模型对桩的沉降可靠度影响不明显，因此其概率模型可近似采用正态分布；在土的变形模量为大变异的情况下，其概率模型对桩的沉降可靠度影响非常明显，在选择概率模型时要慎重。对于土的变形模量服从对数正态分布的情况，采用将其当量正态化后的中心点法即使在参数大变异的情况下也可以获得理想的计算精度。     

钢筋砼框架非线性分析的简化单元模式

介绍一种用于钢筋混凝土框架二阶弹塑性分析的简化单元模式。它考虑了轴力的二阶效应、横截面的塑化和塑性区长度等非线性因素的影响。利用杆件截面的弯矩—曲率关系,可以直接由弹性杆件的转角—位移方程建立单元的非线性刚度矩阵。经与试验结果比较,说明计算结果是正确的。     

直扩接收机基带迟早门跟踪环的简化设计

针对要求设计简化、资源有限的设备和系统 ,通过对直扩接收机基带迟早门跟踪环的性能分析 ,在扩频增益比较大时 ,提出了一种简化设计结构 ,用两个由扩频码的部分序列构成的相关器分别替代原来早门和迟门的完全序列相关器。仿真表明该结构在给定足够的相关值情况下 ,性能略有恶化 ,但资源却得到较大节约 ,设计可大大简化。     

大空间结构钢屋盖火灾下温度场计算方法研究

为了研究大空间结构屋面钢构件火灾下温度场的简化计算方法,把国内外现有用于“室内火灾”温度场的简化计算公式和方法,应用于典型尺寸的大空间结构模型,并与数值模拟结果进行比较。给出了对各种方法的计算准确性的分析结果,并从理论和原理的角度对各种方法的优劣进行了综合评价,提出了进一步修正的方向。     

轴对称正挤压的简化滑移线解

介绍了一种分析轴对称塑性成形问题的新方法———简化滑移线解法 ,并得到了光滑锥形凹模正挤压问题的简化滑移线解 ,求解所依据的近似应力场满足平衡微分方程和应力边界条件 ,并包含有应力间断面 ,但在某些局部范围内不满足屈服准则。结果表明 ,简化滑移线解高于滑移线解 ,低于上限解 ,比较接近于真实载荷 ,是求解轴对称塑性成形问题变形力的一种简便而实用的新方法     

多点多板多分型面注塑模具的简化设计

应用锁扣装置、组合拉杆结构，减少导柱数量，简化了多点多板多分型面注塑模具的设计。     

A simplified model of nitric oxide emission from a circulating fluidized bed combustor

A simplified mathematical model leading to a closed form of solution is developed for estimation of nitric oxide emission from a coal fired circulating fluidized bed (CFB) furnace. The furnace is divided into two sections: a lower section below and an upper section above the secondary air injection level. Reactions in the cyclone and the return leg are neglected. Furnace dimensions, coal feed rate, coal composition and furnace temperature are inputs to the model which was validated against several pilot scale and commercial units. Experimental results from two pilot plants and two commercial power plants agree with model predictions. A sensitivity analysis was carried out using the model to examine the effect of different operating parameters and coal properties on the overall NO emission from the furnace. It was found that excess air and furnace temperature are most important factors influencing the NO emission level. The primary to secondary air ratio influences the NO emission level reasonably. Properties of coal are other factors which affect the NO emission to a large extent. The model, though it invovles some simplification, predicts the overall emission of NO with a level of accuracy accepted in commercial operation.     

基于莱维飞行的改进简化粒子群算法

基于基本粒子群算法易陷入局部最优的不足,提出一种基于莱维飞行的改进简化粒子群算法LISPSO（An Improved and Simplified Particle Swarm Optimization algorithm based on Levy flight）。简化粒子群算法舍去更新公式中的速度项,仅由位置项控制其进化方向。在简化粒子群算法SPSO（Simplified Particle Swarm Optimization）的基础上,采用带有随机性的非线性递减惯性权重动态地更新每个粒子的位置。算法又融合了基于相似度及聚集度分析的莱维飞行。粒子与最优粒子间的相似度越高,或者粒子间的聚集度越高,则粒子利用莱维飞行来重新更新位置的概率也就越大,有效地帮助粒子逃离局部最优。利用matlab语言对11个测试函数进行算法仿真,结果表明,改进的算法在求解精度和收敛速度上有显著的改善。另外,将LISPSO算法应用于求解min-max-min问题,实验结果显示,改进算法在求解效果上明显优于其他对比算法。     

Research and Application of Dynamic Equation for Full Frontal Impact

Full frontal impact theory needs researching and exploring to satisfy the primary safety design of occupant restraint system,avoiding the increasingly "engineering"trend in order to develop and design safety vehicle. After occupant restraint system is simulated by using linear elastic stiffness k,the occupant-vehicle frontal rigid barrier impact model is established. Dynamic equation of dummy chest coupling vehicle is built for full frontal impact based on ordinary vehicle deceleration by Hooke law,and the equation is solved by comparing coefficient and satisfying boundary qualifications. While relative vehicle characteristic parameters are kept unchanging,the actual vehicle deceleration is fitted to the simplified equivalent square wave( ESW),tipped equivalent square wave( TESW) and equivalent dual trapezoids wave( EDTW). Phase angle  and amplitude A of dynamic equations based on ESW,TESW and EDTW are calculated and deduced. The results show that: the dynamic equation of dummy chest coupling vehicle can be well utilized to instruct the primary safety design of full frontal impact for objective vehicle to satisfy chest deceleration demands and the equation based on TESW is best for this design.