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THE EFFECT OF COLD ROLLING ON THE CREEP BEHAVIOR OF INCONEL ALLOY 718

机译:冷轧对Inconel合金蠕变行为的影响718

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The creep behavior of INCONEL alloy 718 (IN 718) was investigated to identify processing-creep property relationships. The alloy was cold rolled (CR) to 0, 10, 20, 30, 40, 60, and 80% followed by annealing and aging. In addition, this alloy can be superplastically formed (IN 718SPF) to a significantly finer grain size and the corresponding microstructure and creep behavior were evaluated. The creep behavior was evaluated in the applied stress range of 300-758MPa and the temperature range of 638-670°C. Constant-load tensile-creep experiments were used to measure the values of the steady-state creep rate and the consecutive load reduction method was used to determine the values of backstress (σ{sub}0). Creep-rupture time (T{sub}r) and elongation-to-failure (ε{sub}f) were also evaluated at 649°C and 758MPa, The lowest σ{sub}0 values (300MPa<σ{sub}0<310MPa) were exhibited for the most severely CR microstructures (60%, 80%, and IN 718SPF), while the baseline 0%CR microstructure exhibited a significantly greater σ{sub}0 value (540MPa). The greatest σ{sub}0 values, 645 and 630MPa, were exhibited by the 20% and 30%CR conditions, respectively. The σ{sub}0 values were related to the overall creep resistance as the 20%CR condition exhibited the lowest secondary creep rates for a given applied stress (σ{sub}a), while the samples CR to more than 40% exhibited the greatest creep rates. The values for the effective stress exponent suggested that the transition between the rate-controlling creep mechanisms was dependent on effective stresses (σ{sub}e=σ{sub}a-σ{sub}0) and the transition occurred at σ{sub}e=135MPa for a temperature of 638°C. Increased CR tended to increase T{sub}r and ε{sub}f, and the 30%CR condition exhibited the greatest creep rupture properties. Overall, the 20%CR and 30%CR microstructures exhibited the greatest creep strength, while the most severely CR materials exhibited the poorest creep strength.
机译:研究了Inconel合金718(718年)的蠕变行为以鉴定加工蠕变性质关系。合金冷轧(Cr)至0,10,20,30,40,60和80%,然后进行退火和老化。此外,该合金可以使(在718粒中)超复位形成,以显着更细的粒度和相应的微观结构和蠕变行为进行评估。在300-758MPa的施加应力范围内评价蠕变行为,温度范围为638-670℃。恒定负载拉伸蠕变实验用于测量稳态蠕变率的值,并且使用连续的负载减少方法来确定逆信符的值(σ{sub} 0)。还在649°C和758MPa下评估蠕变破裂时间(T {Sub} R)和延伸到失败(ε{Sub} F),最低σ{sub} 0值(300mpa <σ{sub} 0为最严重的Cr微观结构(60%,80%和718粒)表现出<310MPa,而基线0%Cr微观结构表现出明显更大的σ{uS} 0值(540MPa)。最大的σ{sub} 0值,645和630MPa分别由20%和30%Cr条件表现出来。 σ{sub} 0值与整体蠕变电阻有关,因为20%Cr条件表现出给定施加的应力(σ{sub} a)的最低二次蠕变速率,而样品Cr达到超过40%最大的蠕变率。有效应力指数的值表明,速率控制蠕变机制之间的转换取决于有效应力(σ{sub} e =Σ{sub} a-Σ{sub} 0),并且在σ{sub处发生转换} E = 135MPa温度为638°C。增加CR倾向于增加T {u} R和ε{} F,30%CR条件表现出最大的蠕变破裂性能。总的来说,20%Cr和30%Cr微观结构表现出最大的蠕变力量,而最严重的CR材料表现出最贫困的蠕变力量。

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