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针对燃气轮机各类故障的诊断问题,将条件规则与故障树法相综合的诊断技术应用到燃气轮机的故障诊断研究中.在建立燃气轮机失效故障树的基础上,通过归纳总结典型的故障案例和维修经验,构建了基于条件规则的逻辑推理模型,利用基于信号处理技术的燃气轮机故障分析原理,在故障树的中间事件和底端事件上,增加了具体故障分析的条件规则,并进行了物理和逻辑判断,以确定故障树每个分支的诊断选择,从而明确了每一步的故障诊断分析,最终得出了精确的故障原因和故障部位.结合某海上石油作业区燃气轮机发电机组的转子振动故障实例,在进行燃气轮机发电机组在线监测的基础上,运用基于条件规则的故障树法快速而准确地分析出了故障的根本原因.研究结果表明,该诊断方法简单易行,便于维修技术人员掌握,可广泛运用于燃气轮机发电机组的可靠性维护. 相似文献
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燃气轮机作为一种多功能供能机械,被广泛地应用于我国海上平台的生产作业,直接为平台的各个系统输送电能,其正常工作对整个平台的正常生产起到关键的保障作用;但是,近年来我国沿海钻井平台使用的不同型号发电机组时有发生叶片断裂的事故,造成严重的生产损失,所以研究故障叶片的诊断具有重要意义。本文运用一种将模糊综合评判与故障树分析法有机结合的诊断方案,克服了传统故障树诊断技术中难以解决的随机不确定性和复杂模糊性问题,并且以某作业区海上平台燃气轮机故障叶片为例,阐述了运用该方法对叶片故障原因进行的精确诊断。 相似文献
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《机电工程》2021,38(8)
针对燃气轮机动叶片典型故障模式断裂故障的诊断问题,对动叶片断裂激励下的敏感振动特征及识别方法进行了研究。首先,以机匣-静叶为研究对象,基于动叶片断裂故障机理,并结合燃机叶片结构特点和载荷特征,建立了其断裂激励下的动力学模型及运动方程;通过对其振动响应进行求解及响应分析,研究了便于工程中监测分析的叶片断裂故障的机理特征。然后,提出了一种基于小波变换的叶片断裂故障识别方法。最后,利用某型燃气轮机叶片断裂故障实际案例,对所提出的振动特征及故障识别方法进行了可行性验证。研究结果表明:作为系统主要激振频率,在动叶片断裂后,叶片通过频率的幅值具有阶跃式突降特性,结合小波变换算法可实现对叶片断裂故障的有效识别;该研究成果可为燃气轮机动叶片断裂故障的诊断提供一定的参考。 相似文献
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针对我国井工煤矿常用的典型掘进机液压系统故障的诊断及排除难题,基于故障树分析法及逻辑分析判断法,建立起掘进机截割部升降失效故障树及掘进机行走部马达驱动失效故障树,并依据故障树对事件发生的类别、概率、实际工况等依次进行分析判断,结合使用排除法对故障进行准确定位及处理,并对掘进机液压系统的日常维护工作进行了分析。 相似文献
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针对风力发电机变流器故障中数量较多的风扇损坏故障,进行拆解检查,并进行故障树分析。在分析中,确定了故障树中的顶事件和最小割集重要底事件,对重要底事件进行评分,进而制订相应的改进方案。实施改进方案后,取得了良好的改进效果。 相似文献
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利用故障树分析法对火力发电厂制粉系统的常见故障进行了分析研究,建立了制粉系统的故障树,涵盖了球磨机、给煤机、排粉机、粗细粉分离器的常见故障,求出了其最小割集,给出了制粉系统发生故障的原因及导致故障各种原因组合的可能性。并且以球磨机为例给出了故障树分析的具体应用,通过球磨机振动信号的采集与分析,对球磨机的机械部件故障进行诊断。故障树分析法给制粉系统的故障智能诊断提供了一种有效的方法,为故障维修及故障预防提供了指导。 相似文献
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Ali Jahangiri Seyed Ebrahim Moussavi Torshizi Seyed Majid Yadavar Nikravesh 《Journal of Mechanical Science and Technology》2013,27(4):993-999
In gas turbine power plants, a fan is used as a cooling system to dissipate generated heat in coils (copper conductors) and generator electric circuits at the end sides of its rotor. In some cases, fracture of blades causes short circuit between rotor and stator and consequently generator explosion and made lot of financial problems. The fracture of cooling fan blades has been occurred five times at the turbine side of the generator in our case of study, just 100 hr after resuming operation after overhaul. Using numerical analysis as well as laboratory investigation — includes visual inspections, metallography and SEM — can help better finding failure problems that cause blade failures. A series of numerical analysis was performed to diagnose the cause of failure possibility. CFD analysis is used to study the airflow distribution in order to observe probable separation phenomenon and pressure forces that they are imposed to fan blades due to operation. A finite element method was utilized to determine the stresses and dynamic characteristics of the fan blade (natural frequencies, stresses and vibrations). 相似文献
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High-cycle fatigue (HCF) has been identified as one of the primary causes of gas turbine engine failure. The modal characteristics and endurance strength of a 5 MW gas turbine engine blade developed by Doosan Heavy Industries & Construction Co., Ltd. in HCF fracture were verified through analysis and tests to determine the reliability of the compressor blade. A compressor blade design procedure that considers HCF life was performed in the following order: airfoil and blade profile design, modal analysis, stress distribution test, stress endurance limit test, and fatigue life verification. This study analyzed the Campbell diagram and estimated resonance risk on the basis of the natural frequency analysis and modal test of the compressor blade to guarantee safe and operational reliability. In addition, the maximum stress point of the compressor blade was determined through stress distribution analysis and test. The bonding point of the strain gage was determined by using fatigue test. Stress endurance limit test was performed based on the results of these tests. This research compared and verified the modal characteristics and endurance strengths of the compressor blades to prevent HCF fracture, which is among the major causes of gas turbine engine damage. A fatigue life design procedure of compressor blades was established. The 5 MW class gas turbine compressor blade is well designed in terms of resonance stability and fatigue endurance limit. 相似文献
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To determine the reliability of a 5 MW gas turbine engine blade in high cycle fatigue (HFC) fracture being developed by Doosan Heavy Industries & Construction Co., Ltd., resonance characteristics are verified based on the turbine blade tip shape and assembly condition. In this study, the modal characteristics of compressor and turbine blades are investigated, and a Campbell diagram is established. During the preliminary study, modal analysis and holographic modal test of the first-, fifth-, and tenth-stage compressor blades were performed. Based on the preliminary study result, the natural frequency and Campbell diagram analysis for the turbine blades were performed. This research compared and verified the modal characteristic and resonance stability according to the tip shape and assembly condition of the blade to prevent any HCF fracture. In conclusion, the resonance stability of the shrouded blade is far superior to that of the squealer blade. Suitable assembly conditions must be applied. 相似文献