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首页> 外文期刊>Journal of Multiscale Modelling >High-Temperature Combined Fatigue Tests on Full-Scale Turbine Blades
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High-Temperature Combined Fatigue Tests on Full-Scale Turbine Blades

机译:全规模涡轮叶片的高温联合疲劳试验

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摘要

Compared with standard specimens, fatigue tests on full-scale turbine blades can take factors such as geometry and manufacturing process into consideration of life assessment. However, for combined fatigue tests of full-scale turbine blades, there exist two challenges. The first one is that it is difficult to apply combined loads of centrifugal force (low cycle fatigue, LCF) and vibration force (high cycle fatigue, HCF) properly because of the interaction between these loads. The second one is that it is hard to determine the range of HCF load/stress which the blade experiences at service conditions. To address these two challenges, firstly, a set of two-path fixture is designed to apply combined loads on the test blade, which can transfer LCF and HCF load separately by different paths. And secondly, two methods, i.e. the inverse method and the contrast method are proposed to estimate the HCF stress level for turbine blades at service conditions. The inverse method infers the HCF stress level by comparing blade failure data between field (in service) and bench tests conditions, while the contrast method obtains HCF stress level by comparing blade failure data between new and used blades under bench tests conditions. Detailed procedures of high temperature combined fatigue tests on full-scale blade are presented, and experimental life data is also included and analyzed.
机译:与标准标本相比,全级涡轮机叶片上的疲劳试验可以考虑到寿命评估的几何和制造过程等因素。然而,对于满量型涡轮叶片的组合疲劳试验,存在两个挑战。第一个是由于这些负载之间的相互作用,难以适当地施加离心力(低循环疲劳,LCF)和振动力(高循环疲劳,HCF)的组合负载。第二个是,很难确定叶片在服务条件下经历的HCF负载/应力的范围。为了解决这两个挑战,首先,一组两条路径夹具设计用于在测试刀片上施加组合负载,这可以通过不同的路径分别传输LCF和HCF负载。其次,提出了两种方法,即反向方法和对比度方法,以估计在服务条件下涡轮机叶片的HCF应力水平。逆方法通过比较现场(在服务)和台式测试条件之间的刀片故障数据来缩小HCF应力水平,而通过比较在台面测试条件下的新和二手刀片之间的叶片故障数据来获得HCF应力水平。提出了在全尺度叶片上的高温疲劳试验的详细程序,还包括实验生活数据并分析。

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