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COMPARISON OF CREEP-FATIGUE EVALUATION METHODS WITH NOTCHED SPECIMENS MADE OF MOD.9CR-1MO STEEL

机译:MOD.9CR-1MO钢制缺口标本的蠕变疲劳评价方法比较

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In a component design at elevated temperature, creep-fatigue is one of the most important failure modes, and assessment of creep-fatigue life in structural discontinuity is important issue to evaluate structural integrity of the components. Therefore a lot of creep-fatigue life evaluation methods were proposed until now. To compare and assess these evaluation methods, a series of creep-fatigue tests was carried out with notched specimens. All the specimens were made of Mod.9Cr-1Mo steel, which it is a candidate material for a primary and secondary heat transport system components of JSFR (Japan Sodium-cooled Fast Reactor). Mechanical creep-fatigue tests and thermal creep-fatigue tests were performed by using conventional uni-axial push-pull fatigue test machine and thermal gradient generating system with an induction heating coil. Stress concentration levels were adjusted by varying the diameters of notch roots in the both tests. In the test, creep-fatigue lives, crack initiation and propagation processes were observed by digital micro-scope and replica method. Besides those, a series of elastic Finite Element Analysis (FEA) were carried out to predict the number of cycles to failure by several creep-fatigue life evaluation methods. Then these predictions were compared with test results. Several types of evaluation methods which are stress redistribution locus (SRL) method, simple elastic follow-up method and the methods described in JSME FR(Fast Reactor) code were applied. The applicability and conservativeness of these methods were discussed. It was appeared that SRL method gave rational prediction of creep-fatigue life with conservativeness when the factor of k=1.6 was applied for all the conditions tested in this study. Comparison of SRL method and simple elastic follow-up method indicated that SRL method applied factor of k=1.6 gave the smallest creep-fatigue life in practicable stress level. JSME FR code gave an evaluation 70~100 times conservative lives comparing with the test results.
机译:在升高温度下的组件设计中,蠕变 - 疲劳是最重要的失效模式之一,结构不连续性的蠕变疲劳寿命是重要的问题,可以评估组分的结构完整性。因此,提出了许多蠕变疲劳寿命评估方法。为了比较和评估这些评估方法,通过缺口样本进行一系列蠕变疲劳试验。所有标本都由MOD.9CR-1MO钢制成,这是JSFR(日本钠冷却快速反应器)的初级和二次热传输系统组分的候选材料。通过使用具有感应加热线圈的传统的单轴推拉疲劳试验机和热梯度产生系统来进行机械蠕变疲劳试验和热蠕变疲劳试验。通过改变两种测试中的缺口根的直径来调节应力浓度水平。在测试,蠕变 - 疲劳寿命,裂缝引发和繁殖过程中观察到数字微观和复制方法。除了那些之外,进行了一系列弹性有限元分析(FEA)以预测几种蠕变疲劳寿命评估方法的失效循环次数。然后将这些预测与测试结果进行了比较。施加了几种类型的评估方法,该评估方法是应力再分布轨迹(SRL)方法,简单的弹性随访方法和JSME FR(快速反应堆)代码中描述的方法。讨论了这些方法的适用性和保守性。似乎SRL方法在本研究中施加k = 1.6因子时,对蠕变疲劳寿命的合理预测具有保守性。 SRL方法的比较和简单的弹性随访方法表明,SRL方法施加的k = 1.6的施加因子在切实可行的应力水平下给出了最小的蠕变疲劳寿命。 JSME FR代码给出了70〜100次保守生活与测试结果相比的评估。

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