我国实施国际海上人命安全公约的不足及改进建议

《1974年国际海上人命安全公约》于1980年5月25日对我国生效以来,经过政府、各级海事管理部门、港口行政管理部门、船公司等有关部门和人员的共同努力,较好地实施了公约及其修正案的履约工作。但是,我国在执行SOLAS 1974中也存在一些不足之处。探讨我国履约工作存在的问题和不足,并提出改进建议。     

用现有疲劳试验数据确定疲劳裂纹扩展率

疲劳寿命的预报在船舶与海洋工程领域中相当重要，但其关键问题是要找到一种较科学的疲劳寿命预报方法。最近，本文第二作者提出了一种海洋结构物疲劳寿命预报的统一方法。该方法是基于疲劳裂纹扩展理论而发展起来的，在其九个参数模型的假设之下，能够较好地解释一些其它方法所不能解释的现象。采用该方法的主要障碍在于需要确定疲劳裂纹扩展率。作者通过对不同的疲劳裂纹扩展率的比较研究，并推广McEvily模型后，提出了一个具有较宽适用范围的九个参数疲劳裂纹扩展率模型(从门槛域一直到不稳定断裂域)。本文的主要目的是解决如何根据一些现有的疲劳试验数据来确定这九个模型参数的问题。文中给出了通过实验数据确定裂纹扩展率模型中各个参数的方法，并进行了模型参数的灵敏度分析。通过对文献中一些试验数据的收集，给出了几种常用金属材料的裂纹扩展率模型参数。     

A probabilistic damage tolerance concept for welded joints Part 2: a supplement to the rule based S–N approach

The first part of this paper presented the required statistics and stochastic models for reliability analysis of the fatigue fracture of welded plate joints. This present Part 2 suggests a probabilistic damage tolerance supplement to the design S–N curves for welded joints. The goal is to provide the practising engineer with simple tools that predict the reliability against fatigue fracture during service life. The impact of the chosen fatigue design factors (FDF) and the uncertainty in the applied stresses is revealed. The effect of an in-service inspection programme is also predicted. The results are presented as dimensionless matrices and suggested for use in support of decision-making at the design stage, without any advanced fracture mechanics modelling and stochastic simulation. One important advantage of this format is that the probability levels are presented regardless of actual weld class and target service life (TSL). This is obtained by introducing the FDF as a key parameter to the results. This parameter is defined as the ratio of predicted fatigue life over TSL. FDF is always calculated in the S–N approach which is mandatory in fatigue life prediction. Various welded details (classes) will have the same reliability level for the same FDF. This is true at the end of TSL and at earlier stages, i.e. fractions of TSL. The absolute value of TSL is immaterial for a given FDF. In the case of in-service inspection, the inspection interval is also given without dimensions as a fraction of TSL.

Only the influence of future scheduled inspections is treated. Updating based on actual inspection results is not included as the scope of work is inspection planning at the design stage. Results for some frequent cases occurring in practice are readily derived and presented.     

船体结构腐蚀疲劳问题以及数值计算方法

船体或者内部高强脆性材料在腐蚀环境中的破坏问题已受广泛关注,其中涉及破坏机理的研究屡见报道,但相关的数值计算研究方法目前还屈指可数,文章在介绍各种破坏机理的基础上,从数值计算方法研究的角度阐述了最近几十年中的研究进展以及作者在该领域所取得的前沿性的成果,并指出了无网格有限元计算方法将在这个研究领域扮演重要角色.     

大型集装箱船舱口盖疲劳寿命研究

提出大型集装箱船舱口盖的疲劳问题,基于S-N曲线提出分析方法,对某8530TEU集装箱船上的典型舱口盖结构进行疲劳寿命分析,并将计算结果与船级社规范推荐方法计算的结果相比较,得到有益结论.     

装备项目风险管理体系的研究

首先对装备项目全寿命周期内各阶段风险管理的工作内容、相互关系进行了分析,参考系统工程三维结构概念和国内学者提出的风险管理体系的论述,提出了新的三维风险管理体系概念模型,对结构、要素进行了定义和阐述,对其理论指导作用和实际使用意义做了初步探讨,提出了进一步研究的方向,以期对装备项目的风险管理工作和理论研究起到参考和促进作用.     

Prediction of fatigue life and estimation of its reliability on the parts of an air suspension system

Air suspension systems have been implemented in various commercial vehicles, such as buses and special purpose trucks, because of the comfortable ride and easy height control. An evaluation of the durability of vehicle parts has been required for service life and safety starting in the early stages of design. The cyclic load applied to the vehicle can cause fatigue failure of parts, such as the suspension frame. This paper presents a method to predict the fatigue life of the suspension frame at the design stage of the air suspension system used in a heavy-duty vehicle. To estimate the fatigue life using the SN method, the Dynamic Stress Time History (DSTH) is necessary for the part of interest. DSTH can be obtained from the results of the flexible body dynamic analysis using the Belgian road simulation and the Modal Stress Recovery (MSR) method. Furthermore, the reliability of the predicted fatigue life can be evaluated by considering the variations in material properties. The probability and distribution of the expected life cycle can be obtained using experimental design with a minimum number of simulations. The advantage of using statistical methods to evaluate the life cycle is the ability to predict replacement time and the probability of failure of mass-produced parts. This paper proposes a rapid and simple method that can be effectively applied to the design of vehicle parts.     

基于灰色马尔可夫理论的油气管道腐蚀剩余寿命预测

以灰色理论的标准GM（1,1）模型和马尔可夫TPM理论为基础,提出了基于灰色马尔可夫理论的油气管道腐蚀剩余寿命预测方法。利用灰色马尔可夫理论预测腐蚀油气管道剩余寿命的步骤主要包括：最大允许腐蚀深度的确定,腐蚀速率的预测以及剩余寿命预测。并基于该方法,采用VB系统开发了实用软件,简便可靠。该方法可以在腐蚀速率波动比较大的情况下预测油气管道的剩余寿命,为油气管道腐蚀检测周期的确定提供了科学依据。     

简易机场道面结构的疲劳特性试验

为了分析简易机场的合理道面结构,依托陕西西安、湖南耒阳的室内外试验段,利用直径30cm刚性承载板模拟机轮荷载圆,使用反力架、千斤顶及疲劳试验机,通过人工和机械定点重复加载模拟飞机通行,研究了薄层沥青混凝土面层 水泥稳定细粒土基(垫)层道面结构在重复荷载作用下的疲劳特性。试验结果表明:推荐道面结构早期承载能力较高,在60d龄期内,整体回弹模量为200～300MPa,弯沉小于1mm;此时道面可承受飞机荷载几万至十几万次的起降通行而不破坏,并保持良好的使用性能;推荐道面结构的疲劳特性可以满足简易机场的应急使用需求。     

基于Digatron电池测试系统的锂电池温度寿命试验技术研究

本文主要论述了利用目前国际主流的Digatron电池测试分析系统,选取温度作为表征锂电池组寿命特性的参数,设计了电池组性能试验,通过实验数据分析得到了锂电池组寿命特性趋势,对于改善车辆电池控制管理策略具有指导意义。