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1.
采样时间序列的故障数据检测与滑动容错滤波   总被引:1,自引:0,他引:1  
在导出采样时间序列数据滑动LS滤波的基础上,本文建立了了组简洁的故障数据检测与修复算法,地故障数据修复与滤波估计相结合,构造了对突发性故障数据有良好容错能力的滑动容错滤波算法。仿计算证实,该方法有效、可靠。  相似文献   

2.
DME设备频繁出现遇天气炎热就双机双监控器“输出功率”告警,导致设备自动切换及以次告警维持工作,严重地影响了设备的正常运行。经导航技术人员的努力最终确定故障部位在造价昂贵的天线上。DME天线结构复杂且在检修上无任何经验可借鉴,技术人员在做了认真的技术准备后,一步一步地检查出天线存在的各种故障,并逐一予以排除,最终将天线系统修复。本文详细介绍了DME天线故障引起的设备告警,并对如何确定天线故障及修复天线提供了检测、检修方法。  相似文献   

3.
为弥补战争损耗,保持飞机的持续战斗力,必须对战伤飞机进行速修复,而决定战伤修复效率的关键因素是飞机本身所具有的固有属性-战伤修复性,本文分析了战伤修复的特点,给出了评估方法,战伤修复性设计要求和措施。  相似文献   

4.
针对某型发动机金属屑信号器壳体腐蚀情况,分析了传统修复方法的缺陷,提出了机加胶接复合修复技术的新思路,确定了修复中所选用的金属和非金属材料,并介绍了修复工艺。  相似文献   

5.
为了解决军机备件配置不合理的问题,通过对飞机预防性维修和修复性维修备件的需求分析,提出了一种较为科学的备件确定方法,开发了确地件项目和数量的计算软件。  相似文献   

6.
《民航科技》2006,(4):36-37
本文通过对精达稳压器使用的调制解调器远程监控系统故障的分析,和对其通信系统的研究,并结合调制解调器通信的原理,提出了在其远程通信中通过更改调制解调器指令,应用普通的现有调制解调器的解决方案,从而降低了系统的维护难度和调制解调器的购买成本,极大地缩短了故障修复时间,更好地保障了飞行安全。  相似文献   

7.
复合材料微波胶接修补技术的研究及应用   总被引:1,自引:0,他引:1  
根据微波快速固化、均匀制热的机理,研制开发了全新的复合材料微波快速胶接修复设备,并进行了修补试验.试验结果证明,该技术完全满足飞机结构件的修复要求,且显著地缩短了修复时间.  相似文献   

8.
着重从修复机理出发分别介绍了金属基、陶瓷基和聚合物基自修复材料的研究进展,分析了达到良好自修复功能对材料结构、组成和性能等方面的要求,综述了自修复材料的研究进展、存在的问题及其发展方向。  相似文献   

9.
介绍了一种存储器自修复电路的仿真设计,其中内建自测试模块中的地址生成器采用LFSR设计,它面积开销相当小,从而大大降低了整个测试电路的硬件开销。而内建自修复模块采用基于一维冗余(冗余行块)结构的修复策略设计。通过16×32比特SRAM自修复电路设计实验验证了此方法的可行性。  相似文献   

10.
定子片粗密冲模阴阳模发生断裂。确定应用环氧型结构胶和粘接工艺技术,完好地修复冲模,冲制的定子片性能完全达到技术要求。  相似文献   

11.
E 级计算给 CFD 带来的机遇与挑战   总被引:4,自引:0,他引:4  
E 级(Exascale)计算机有望在2020年前后投入使用,E 级计算将给计算科学和科学研究带来革命性的变化。计算流体力学(CFD)作为超大规模计算机应用的重要领域之一,将迎来前所未有的发展机遇,同时也将面临极其严峻的技术挑战。本文对当前国内外超大规模 CFD 计算的现状进行了概述,探讨了未来 CFD 的发展趋势,并对 E 级计算给 CFD 带来的机遇与挑战进行了分析,最后提出了适应未来 E 级计算的 CFD 发展思路与建议。为了实现 E 级计算的宏伟目标,CFD 与计算机科学、应用数学等学科的“协同设计”势在必行。我们期待本文的分析能对我国的高性能计算应用、CFD 发展有一定的启示作用。  相似文献   

12.
本文试图说明在喷气发动机上或燃气轮机的进气道内建立聚氧滞氮的流场,增加燃烧室氧的浓度,组织富氧燃烧.提高涡轮前的温度和整机热效率.加大喷气发动机的推力,降低航空煤油耗量,减少喷气尾气对大气的污染.对各种可能的聚氧滞氮的方案进行了初步探索.  相似文献   

13.
党的“十八大”提出“到2020年要实现城乡居民人均收入比2010年翻一番”,为了实现这个目标,进一步深化收入分配改革就成为关键手段,而收入分配的重点领域就是城镇职工的收入分配。文章采用泰尔指数作为比较城镇职工收入分配差异性现状的指标,分析发现:总体上看,不管是在企业内部,还是在企业之间,在不同性质企业就业的城镇职工收入分配差距在逐步缩小,但是在不同性质企业就业的职工收入分配缩小比例并不一致,部分企业甚至有扩大收入分配差距的趋势。因此,在深化收入分配改革时,要综合考虑不同性质企业城镇职工收入分配的现状,在坚持既有的收入分配改革政策之外,还应当采取一些措施向某类企业倾斜。  相似文献   

14.
管路系统计算机辅助设计方法研究   总被引:4,自引:0,他引:4  
陈志英  唐文哲 《航空动力学报》2001,16(2):182-184,188
为进行计算机辅助管路系统敷设,本文归纳出9条管路CAD规则,探讨了3种管路敷设方法。为满足管路设计规则,根据管路系统的复杂性和计算机辅助敷设的特点,本文提出了先敷设粗管再分区敷设最后解决跨区域管路的WRS法。它按照先重后轻、先短后长、先难后易的敷管原则,体现了局部最优从而达到全局最佳的原理。文中着重介绍了该方法的思路,并结合在电子模型样机上的敷管实例及过程,分析了该方法的特点。   相似文献   

15.
Numerous attempts have been made over the years to link various aspects of solar variability to changes in the Earth's climate. There has been growing interest in this possible connection in recent years, spurred largely by the need to understand the natural causes of climate change, against which the expected global warming due to man's activities will have to be detected. The time scale of concern here is that of decades to centuries, and excludes the longer millennial scale in which orbital variations play a dominant role. The field has long been plagued by the lack of an acceptable physical mechanism by which solar variability can affect climate, but the discovery of variability in the Sun's total irradiance (the solar ``constant' of meteorology) by spacecraft instruments has pointed to a direct mechanism. Other less direct mechanisms that have been suggested involve variations in the Sun's ultraviolet flux and in the plasma outflow of the solar wind. The purpose of this paper is to summarize the current state of the field, emphasizing the proposed mechanisms as an introduction to the more detailed papers that follow. The particular case of sea-surface temperature data will be used as an illustration.  相似文献   

16.
用隐式多重网格法计算三维粘性流动   总被引:1,自引:0,他引:1  
唐智礼 《航空学报》1998,19(3):327-331
求解高雷诺湍流流动时,边界层法向网格间距较流向和展向相比非常小,因此边界层中存在高度伸缩的网络,这将大大降低多重网格的求解效率。通过谐调的处理多重网格过程的各个细节,既提高了解的精度,又克服了网格展弦比的影响,使得计算效率提高了6~7倍。  相似文献   

17.
WAVES: The radio and plasma wave investigation on the wind spacecraft   总被引:3,自引:0,他引:3  
The WAVES investigation on the WIND spacecraft will provide comprehensive measurements of the radio and plasma wave phenomena which occur in Geospace. Analyses of these measurements, in coordination with the other onboard plasma, energetic particles, and field measurements will help us understand the kinetic processes that are important in the solar wind and in key boundary regions of the Geospace. These processes are then to be interpreted in conjunction with results from the other ISTP spacecraft in order to discern the measurements and parameters for mass, momentum, and energy flow throughout geospace. This investigation will also contribute to observations of radio waves emitted in regions where the solar wind is accelerated. The WAVES investigation comprises several innovations in this kind of instrumentation: among which the first use, to our knowledge, of neural networks in real-time on board a scientific spacecraft to analyze data and command observation modes, and the first use of a wavelet transform-like analysis in real time to perform a spectral analysis of a broad band signal.  相似文献   

18.
This paper deals with the problem of quickest detection of a signal in discrete-time observations where the noise is not necessarily additive. By introducing a new cost function, penalizing the decision delay, in addition to penalizing wrong decisions as in the classical case, a global risk function is derived for use in a Bayesian framework. The minimization of the average risk leads to the optimum Bayesian decision regions, giving the structure of the optimum receiver. Some simplifications for elementary costs and some applications are investigated. The optimum receiver is shown to be a parallel bank of classical optimum filters, each one matched to a particular delay of the signal to be detected. Our approach is shown to apply to the detection of certain changes in a stochastic process.  相似文献   

19.
目前,还没有实验数据和理论分析可以得出在微细管道内流体的黏性对流体流动及换热的影响,而在微细管道(微米级)内流体高速流动中黏性耗散是不能够忽略的,但是没有合理的计算公式进行理论计算。因此,这里对粘性耗散在微细管道流中的影响进行了分析和理论验证。根据已有的分析给定了一个粘性耗散在微细管道流中造成明显影响的最小标准值。  相似文献   

20.
Review of aerospace engineering cost modelling: The genetic causal approach   总被引:1,自引:0,他引:1  
The primary intention of this paper is to review the current state of the art in engineering cost modelling as applied to aerospace. This is a topic of current interest and in addressing the literature, the presented work also sets out some of the recognised definitions of cost that relate to the engineering domain. The paper does not attempt to address the higher-level financial sector but rather focuses on the costing issues directly relevant to the engineering process, primarily those of design and manufacture. This is of more contemporary interest as there is now a shift towards the analysis of the influence of cost, as defined in more engineering related terms; in an attempt to link into integrated product and process development (IPPD) within a concurrent engineering environment. Consequently, the cost definitions are reviewed in the context of the nature of cost as applicable to the engineering process stages: from bidding through to design, to manufacture, to procurement and ultimately, to operation. The linkage and integration of design and manufacture is addressed in some detail. This leads naturally to the concept of engineers influencing and controlling cost within their own domain rather than trusting this to financers who have little control over the cause of cost. In terms of influence, the engineer creates the potential for cost and in a concurrent environment this requires models that integrate cost into the decision making process.  相似文献   

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