可靠性试验与环境试验的关系

介绍了可靠性试验和环境试验的定义、目的、意义、分类,并对两者之间的联系与区别以及产品研制生产过程中两者的分布与作用等方面进行分析。     

弹丸动平衡自动测试方法研究

采用 IBM- PC机为主机 ,对弹丸动不平衡量 (m1 ,m2 )及相位角α进行自动测试并做相应的数据处理。设计了弹丸左、右两标定面的平面分离电路、A/D转换电路等。     

A nonparametric approach to accelerated life testing under multiple stresses

Accelerated life testing (ALT) is concerned with subjecting items to a series of stresses at several levels higher than those experienced under normal conditions so as to obtain the lifetime distribution of items under normal levels. A parametric approach to this problem requires two assumptions. First, the lifetime of an item is assumed to have the same distribution under all stress levels, that is, a change of stress level does not change the shape of the life distribution but changes only its scale. Second, a functional relationship is assumed between the parameters of the life distribution and the accelerating stresses. A nonparametric approach, on the other hand, assumes a functional relationship between the life distribution functions at the accelerated and nonaccelerated stress levels without making any assumptions on the forms of the distribution functions. In this paper, we treat the problem nonparametrically. In particular, we extend the methods of Shaked, Zimmer, and Ball [7] and Strelec and Viertl [8] and develop a nonparametric estimation procedure for a version of the generalized Arrhenius model with two stress variables assuming a linear acceleration function. We obtain consistent estimates as well as confidence intervals of the parameters of the life distribution under normal stress level and compare our nonparametric method with parametric methods assuming exponential, Weibull and lognormal life distributions using both real life and simulated data. © 1998 John Wiley & Sons, Inc. Naval Research Logistics 45: 629–644, 1998     

Approximation algorithms for sequential batch‐testing of series systems

We introduce and study a generalization of the classic sequential testing problem, asking to identify the correct state of a given series system that consists of independent stochastic components. In this setting, costly tests are required to examine the state of individual components, which are sequentially tested until the correct system state can be uniquely identified. The goal is to propose a policy that minimizes the expected testing cost, given a‐priori probabilistic information on the stochastic nature of each individual component. Unlike the classic setting, where variables are tested one after the other, we allow multiple tests to be conducted simultaneously, at the expense of incurring an additional set‐up cost. The main contribution of this article consists in showing that the batch testing problem can be approximated in polynomial time within factor , for any fixed . In addition, we explain how, in spite of its highly nonlinear objective function, the batch testing problem can be formulated as an approximate integer program of polynomial size, while blowing up its expected cost by a factor of at most . Finally, we conduct extensive computational experiments, to demonstrate the practical effectiveness of these algorithms as well as to evaluate their limitations. © 2016 Wiley Periodicals, Inc. Naval Research Logistics 63: 275–286, 2016     

连续波强激光武器动态毁伤概率的非毁检测法

给出一种强激光武器与目标存在相对运动时的毁伤概率(动态毁伤概率)在非致毁条件下的检测方法。该方法是在已知强激光对目标的致毁时间、一次发射时间的基础上,在武器的跟瞄子系统对目标无毁的跟踪试验中,通过检测跟踪误差在射击门内外交替出现的时间间隔,给出动态毁伤概率的点估计,以及在既定置信度下,动态毁伤概率的置信区间,同时还能判断所测毁伤概率是否处于最佳状态,为进一步优化动态毁伤概率提供依据。     

基于圆柱体缺陷构件的超声探伤重构研究

圆柱体构件中非轴对称人造缺陷偏心圆孔的超声探伤一直是无损检测的难点。基于脉冲反射原理设计超声实验平台,根据检测回波信号判定偏心圆孔缺陷所呈现的特征。在实验研究基础上,针对声场在圆柱体工件内部的传播情况,根据惠更斯原理以圆柱体为发射声源,基于k-wave仿真工具箱建立仿真平台,并利用声学传感器接收声波信号,设计的仿真平台能够实现360°同时刻采集工件的发射信号,同时利用传播过程中声压强弱的变化构建声场模型。根据采集的信号采用逆时反演重构模型,直观可视化地重构了内部缺陷的位置形状信息。     

面向构件的测试研究

主要阐述了对构件测试的一种观点 ,并通过对系统测试及集成测试的裁剪 ,给出了对构件的一种测试方法     

钢弦测功仪的智能化改造研究与实现

将过去传统的钢弦式测功仪用计算机技术进行数据采集与处理 ,从而提高了其测量速度及测试精度 ,数据更为准确、稳定 ,可在 1台仪器上同时连续高速动态显示被测主轴的转速、功率、扭矩 ,并自动保存数据 .人机界面强 ,智能化程度高 ,具有很强的数据后处理及文件形成功能 .     

测试系统静电干扰的仿真实验研究

由于静电干扰的随机性和测试手段的限制 ,难以定量计算静电对测试系统的影响程度。基于人体静电模型和器件模型 ,导出用起电率表示的静电干扰对测试系统影响的仿真计算式 ,并计算出了一般静电环境下静电干扰的具体值 ,为测试系统的干扰计算和静电防护提供了依据     

航空发动机叶片的内窥涡流集成化原位检测

目前内窥检测是航空发动机叶片原位检测的唯一方法,但是内窥检测对于叶片裂纹缺陷的检测效果不理想.为此,提出内窥涡流集成化检测技术,使这两种方法的优势互补,实现对航空发动机叶片的原位检测.研制了一种可用于航空发动机叶片原位检测的内窥涡流集成化检测探头,给出了航空发动机叶片的检测实例.检测结果表明:内窥涡流集成化检测技术的缺陷检测能力高,并且可以实现对裂纹缺陷的定量评估,因此较单一的内窥检测更有优越性.具有很高的实际应用价值.