Temperature and Load Interaction Effects on the Fatigue Crack Growth Rate and Fracture Surface Morphology of IN100 Superalloy

B. S. Adair, W. S. Johnson, S. Antolovich, A. Staroselsky
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引用次数: 7

Abstract

A study was conducted to explore some of the load and temperature interaction effects on the fatigue crack growth rate (FCGR) of polycrystalline superalloy IN100. Load interaction testing in the form of single overloads was performed at 316°C and 649°C. Temperature interaction testing was performed by cycling between 316°C and 649°C in blocks of 1, 10, and 100 cycles. After compiling a database of constant temperature, constant amplitude FCGR for IN100, fatigue crack growth predictions assuming no load or temperature interactions were made. Experimental fatigue crack propagation data were then compared with these predictions to assess interaction effects. The fracture mechanisms observed during interaction testing using a scanning electron microscope were compared with the mechanisms present during constant temperature, constant amplitude testing. Overload interaction testing led to full crack retardation at 2.0 × overloads for both 316°C and 649°C testing. Overloading by 1.6 × at both temperatures led to retarded crack growth, whereas 1.3 × overloads at 649°C created accelerated crack growth and at 316°C the crack growth was retarded. One block alternating temperature interaction testing grew significantly faster than the non-interaction prediction, while 10 block alternating temperature interaction testing also grew faster but not to the same extent. One hundred block alternating testing grew slower than non-interaction predictions. Possible explanations for the interaction effects responsible for the observed crack growth acceleration and retardation are discussed.
温度和载荷交互作用对IN100高温合金疲劳裂纹扩展速率和断口形貌的影响
研究了载荷和温度相互作用对多晶高温合金IN100疲劳裂纹扩展速率的影响。在316°C和649°C下进行单过载形式的载荷相互作用测试。通过在316°C和649°C之间循环1、10和100个循环来进行温度相互作用测试。在编制了IN100的恒温恒幅FCGR数据库后,对无载荷和温度相互作用下的疲劳裂纹扩展进行了预测。然后将实验疲劳裂纹扩展数据与这些预测进行比较,以评估相互作用的影响。用扫描电子显微镜观察到的相互作用试验的断裂机制与恒温、恒振幅试验的断裂机制进行了比较。在316°C和649°C测试中,过载相互作用测试在2.0倍过载下导致完全裂纹延迟。在这两种温度下,1.6倍的过载导致裂纹扩展延迟,而在649℃下,1.3倍的过载导致裂纹加速扩展,在316℃时,裂纹扩展延迟。1块交变温度交互作用测试的增长速度明显快于非交互作用预测,10块交变温度交互作用测试的增长速度也快于非交互作用预测,但程度不同。100块交替测试的增长速度比非交互预测慢。讨论了相互作用对裂纹扩展加速和延迟的可能解释。
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