三峡库区秭归县卡子湾大桥设计与施工

卡子湾大桥为预应力混凝土斜拉式桁架连续刚构桥,跨径79.45 m 140 m 79.45 m,桥梁全长344.3 m,采用悬臂拼装法施工。介绍该桥的总体布置、结构设计、施工及施工监控要点。     

大跨度连续刚构桥施工期截面应力测试与分析

广西布柳河大桥主桥为主跨235m、墩高97米、桥宽仅8.3米的特柔预应力混凝土连续刚构桥。文章结合主桥施工监控实践,介绍大跨高墩连续刚构桥施工期截面应力测试及数据分析的方法,为同类桥型施工提供参考。     

矮墩宽箱连续刚构桥设计

文章结合广西八尺江大桥建设的工程实例,介绍如何利用二三维有限元电算程序对矮墩宽箱连续刚构桥进行施工和成桥阶段的计算分析,从而达到满足宽箱(18·5m)、矮墩(12·5m)的设计要求。     

粘性地层地铁盾构隧道管片结构力学特征研究

以南京地铁一号线为工程背景,采用现场试验的研究手段对穿越粘性地层的盾构隧道管片结构在施工全过程和稳定期的力学行为进行了系统研究,同时采用考虑结构与地层相互作用的梁-弹簧模型对其进行了有限元数值模拟分析,并将结果进行比较和综合,提出了粘性地层条件下地铁盾构隧道管片结构的设计原则与方法。     

济南经十路SMA混合料的质量控制

SMA属于间断级配沥青混合料,它依靠大量粗集料形成嵌挤并通过沥青玛蹄脂填充而形成高性能沥青路面,其设计与验证依然沿用马歇尔试验方法,另附加了其他试验方法以弥补马歇尔法的不足。SMA设计必须对其混合料是否形成嵌挤进行验证。     

国内外沥青路面铣刨机的发展概况

概述了国内外沥青路面铣刨机的发展状况及结构特点，介绍了沥青路面铣刨机的有关标准及国产沥青路面铣刨目前存在的差距，同时认为国产沥青路面铣刨机具有广阔的市场前景。     

BC131变速器阻尼降噪结构设计

本文说明了对BC131汽车变速器取力孔盖板做阻尼处理后,可降低噪声声功率级3.2dB,本文分三部分:(1) 阻尼结构的减振降噪机理;(2) 实验装置;(3) 声压级及声功率级的测量和计算。     

一种基于跟踪变结构控制的鱼雷制导律设计方法

利用变结构控制对干扰和参数摄动的“完全自适应性”,设计出了一种基于运动跟踪变结构控制的鱼地律,并将其于被动方式的水下目标跟踪问题中,结果表明,该制导律可以令相对视线角速度按照给定的运动规律变化,从而大大增强了被动跟踪问题的可观性评估的 且对干扰和参数摄动具有较强的鲁棒性,易于工程化问题的处理     

任意多面体消隐系统的研究

本文在相交凸多面体隐藏线消除方法研究的基础上.运用体素构形的方法.进一步探讨了凹多面体的数据结构以及凹多面体在不同情况下隐藏线消除的可能性,从而建立了一个任意平面体的消隐系统.     

Transient responses of a VLFS during landing and take-off of an airplane

The transient elastic deformation of a pontoon-type very large floating structure (VLFS) caused by the landing and take-off of an airplane is computed by the time-domain mode-expansion method. The memory effects in hydrodynamic forces are taken into account, and great care is paid to numerical accuracy in evaluating all the coefficients appearing in the simultaneous differential equations for the elastic motion of a VLFS. The time-histories of the imparted force and the position and velocity of an airplane during landing and take-off are modeled with data from a Boeing 747-400 jumbo jet. Simulation results are shown of 3-D structural waves on a VLFS and the associated unsteady drag force on an airplane, which is of engineering importance, particularly during take-off. The results for landing show that the airplane moves faster than the structural waves generated in the early stage, and the waves overtake the airplane as its speed decreases to zero. The results for take-off are essentially the same as those for landing, except that the structural waves develop slowly in the early stage, and no obstacle exists on the runway after the take-off of airplane. The additional drag force on an airplane due to the elastic responses of the runway considered in this work was found to be small in magnitude.