SPEC2000规范在可靠性数据共享中的应用

行业内可靠性数据采用不同的交换格式,易导致出现数据来源较多,数据共享和数据分析效率低下等问题。SPEC2000规范提供了一整套可靠性数据收集和交换的标准记录格式,用于改善可靠性数据在收集、测量和共享过程中的兼容性,提高工作效率,减少时间成本和人为差错。     

贝叶斯网络在飞控系统可靠性评估中的应用

把一种基于贝叶斯网络的故障树分析法应用于飞控系统俯仰控制功能的可靠性评估中,突破传统故障树分析法的局限性——各部件独立、状态为二值,不但可以计算系统的可靠性指标,而且可以定量给出某个事件或某几个事件在系统可靠性中所占的地位,找出系统的薄弱环节。     

应用6Sigma改进方法提高TCAS系统可靠性

在大型民用飞机中TCAS系统是重要的飞行安全运行的航电系统之一,其故障会对飞机正常营运造成很大的影响。应用6Sigma原理进行维修管理可以有效地改进TCAS系统的可靠性。结合航空公司波音737NG机队的运行中TCAS系统故障情况,介绍运用6Sienna方法的分析过程达到的实际改进效果。     

武器装备可靠性工程研究现状与最新进展

介绍国内外武器装备可靠性工程理论模型的发展现状与最新研究进展,主要包括提高系统可靠性经常应用到的冗余配置问题,系统失效分析采用的最短路径的旅行商问题,小样本数据条件下的动态故障树问题,复杂系统可靠性预测的随机约束与虚拟最短路径以及NASA对高技术项目进行评价和排序过程中采用的一种多学科群决策模型等。     

多元混合数据回归分析方法

针对加速寿命试验中经常遇到完全数据、定数截尾数据和定时截尾数据混合的情况,提出一种多元混合数据回归分析方法,建立了多元混合回归模型,给出回归系数和标准差的最佳无偏估计,以及百分位值的点估计和置信限估计.该方法不但适用于正态分布,而且还适用于Weibull分布、极值分布等其他各种位置-尺度分布,从而将传统只适用于完全数据...     

随机-有界混合不确定性下结构可靠性优化设计

在结构可靠性分析和设计中,往往无法将所有不确定性参数均作为概率随机变量,存在部分不确定性分布特征不明确而仅知其扰动界限的情况.基于概率模型与多椭球模型的混合不确定性描述,以标准U空间中扩展定义的混合可靠性指标为约束条件,建立了随机不确定性和有界不确定性并存情况下的结构可靠性优化数学模型.利用功能测度方法对原优化模型进行...     

基于名义极限因子和降维方法的涡轮盘结构可靠性优化

结合名义极限因子方法完全实现了可靠性分析与优化过程的解耦,使可靠性分析成为进行优化之前的预分析过程,而在预分析中采用的基于降维的可靠性分析技术,在一阶可靠度方法(FORM)获得的计算结果的基础上进行适晕的数值计算就能够提高可靠性分析的结果.最后,以某涡轮盘结构优化为例对提出的方法可行性和效率进行了验证,结果表明:该方法...     

New Neural Network Response Surface Methods for Reliability Analysis

This article presents two new kinds of artificial neural network (ANN) response surface methods (RSMs): the ANN RSM based on early stopping technique (ANNRSM-1), and the ANN RSM based on regularization theory (ANNRSM-2). The following improvements are made to the conventional ANN RSM (ANNRSM-0): 1) by monitoring the validation error during the training process, ANNRSM-1 determines the early stopping point and the training stopping point, and the weight vector at the early stopping point, which corresponds to the ANN model with the optimal generalization, is finally returned as the training result; 2) according to the regularization theory, ANNRSM-2 modifies the conventional training performance function by adding to it the sum of squares of the network weights, so the network weights are forced to have smaller values while the training error decreases. Tests show that the performance of ANN RSM becomes much better due to the above-mentioned improvements: first, ANNRSM-1 and ANNRSM-2 approximate to the limit state function (LSF) more accurately than ANNRSM-0; second, the estimated failure probabilities given by ANNRSM-1 and ANNRSM-2 have smaller errors than that obtained by ANNRSM-0; third, compared with ANNRSM-0, ANNRSM-1 and ANNRSM-2 require much fewer data samples to achieve stable failure probability results.     

数传控制装备可靠性预计

分析了某型数传控制装置可靠性模型,采用应力分析法对该装置进行了可靠性预计,根据设备实际状况求得其各主要部件的失效率,评估了产品的可靠性,从数据分析得出了影响可靠性的主要环节,提出了改进措施。通过可靠性试验,对可靠性预计值进行了验证。     

Fundamentals of Design and Technology of Rolling Element Bearings

This article presents an overview of fundamentals of rolling element bearing designs and technologies. The aim is to outline the complex interrelation of all fundamentals with the rolling contact fatigue and the attainable bearing life. Such fundamentals include, amongst others, bearing stressing and life capability. The article shows the different types of rolling bearing stressing and the analysis of the stress distribution (principal stresses and equivalent stresses) in the material under the rolling contact area. It becomes obvious that the contamination of the bearing with foreign particles leads to a drastic reduction in bearing life. Furthermore, it demonstrates the impact of the bearing lubrication and coating as well as the effect of additives on the attainable life and wear. Further fundamentals of rolling element bearing design are the materials, the material cleanliness and the heat treatment. The article reveals the importance of the cleanliness of bearing steels as well as different types of inclusions and their effect on rolling contact fatigue. Additionally the article describes how to optimize the material properties (strength, toughness and residual stress) by the heat treatment processes. The outcome of these investigations is that endurance life of a rolling element bearing can be achieved if specific operating conditions, an adequate lubrication, good system cleanliness and specific bearing stressing are met. The article provides a guideline for bearing engineers on how designs and technologies can be applied to optimizing a bearing for a particular industry or aerospace application.