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COMBINED LOW AND HIGH CYCLE FATIGUE TESTS ON FULL SCALE TURBINE BLADES

机译:满量程涡轮叶片的低周和高周疲劳综合测试

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Since the unavoidable vibrations wildly exist in the operating environment of turbine blades, the assessment of the combined low and high cycle fatigue (CCF) properties are of paramount importance for turbine blades. To study turbine blades' CCF properties accurately, one important and useful way is to carry out the CCF tests on full scale turbine blades. When conducting the CCF tests of turbine blades, there are two challenges. One is finding ways/paths to transfer the low cycle load and the high cycle load properly, and the other is the determination of high cycle vibration stress level in the working condition. In this investigation, a new experimental method, in which full scale turbine blades are loaded by a special design test system providing high cycle loads and low cycle loads without interference, is proposed to conduct CCF life tests, while an analysis method (reverse method) based on the CCF tests was developed to estimate the high cycle vibration stress level. The design of the test system and the principle of the reverse method are fully explained in this paper. Test results show that the test system can apply HCF/LCF combined loading on the key section of the full scale turbine blade, and successfully simulated the working state. Meanwhile, the working condition vibration stress range of the blade is obtained through the reverse method.
机译:由于不可避免的振动在涡轮机叶片的工作环境中普遍存在,因此评估组合的低和高周疲劳(CCF)特性对于涡轮机叶片至关重要。为了准确地研究涡轮叶片的CCF特性,一种重要且有用的方法是在满量程涡轮叶片上进行CCF测试。在进行涡轮叶片的CCF测试时,存在两个挑战。一种是寻找适当地传递低周向载荷和高周向载荷的方法/路径,另一种是确定工作条件下的高周向振动应力水平。在这项研究中,提出了一种新的实验方法,其中通过特殊设计的测试系统对满量程的涡轮叶片进行加载,该系统可以提供高循环负载和低循环负载而不会产生干扰,该方法可以进行CCF寿命测试,而分析方法(反向方法)基于CCF测试的结果被开发出来,以估计高周振动应力水平。本文详细说明了测试系统的设计和反向方法的原理。测试结果表明,该测试系统可以在全尺寸涡轮叶片关键部位施加HCF / LCF组合载荷,并成功模拟了工作状态。同时,通过反向方法获得叶片的工作条件振动应力范围。

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