首页> 外文期刊>Journal of Engineering for Gas Turbines and Power >Investigation on Material's Fatigue Property Variation Among Different Regions of Directional Solidification Turbine Blades: Part Ⅰ: Fatigue Tests on Full Scale Blades
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Investigation on Material's Fatigue Property Variation Among Different Regions of Directional Solidification Turbine Blades: Part Ⅰ: Fatigue Tests on Full Scale Blades

机译:定向凝固涡轮叶片不同区域材料的疲劳性能变化研究:第一部分:全尺寸叶片的疲劳试验

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At present, directional solidification (DS) made blades are commonly used in high performance turbine for their better high temperature mechanical, especially in creep properties compared with the equiaxed grain (EG) blades made by conventional casting method. To predict DS blades' fatigue life accurately, one of the practical ways is to conduct tests on full-scale blades in a laboratory I bench environment. In this investigation, two types of full scale turbine blades, which are made from DZ22B by DS method and K403 by conventional casting method, respectively, were selected to conduct high temperature combined low and high cycle fatigue (CCF) tests on a special design test rig, to evaluate the increase of fatigue life benefitted from material change. Experimental results show that different from EG blades, DS blades' fracture section is not located on the position where the maximum stress point lies. By comparing fatigue test results of the two types of blade, it can be found that the fatigue properties among different regions of the DS blade are different, and its fatigue damage is not only related to the stress field, but also affected by different parts material's fatigue properties.
机译:目前,定向凝固(DS)制成的叶片因其更好的高温机械性能,特别是在蠕变性能方面与常规铸造方法制成的等轴晶粒(EG)叶片相比,通常用于高性能涡轮机。为了准确预测DS叶片的疲劳寿命,一种实用的方法是在I型实验室环境中对满量程叶片进行测试。在这项研究中,我们选择了两种全尺寸涡轮叶片,分别由DS方法的DZ22B和常规铸造方法的K403制成,以在特殊设计测试中进行高温联合的低循环疲劳和高循环疲劳(CCF)试验装置,以评估受益于材料变化的疲劳寿命的增加。实验结果表明,与EG叶片不同,DS叶片的断裂截面不在最大应力点所在的位置。通过比较两种叶片的疲劳测试结果,可以发现DS叶片不同区域之间的疲劳性能是不同的,其疲劳损伤不仅与应力场有关,而且还受到不同零件材料的影响。疲劳性能。

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