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A Study of Micro-cracks in Overheated Forgings of Ultra-Low Sulfur Steels for Aircraft Engine Crankshafts

机译:用于飞机发动机曲轴超低硫钢过热锻件微裂纹的研究

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Several crankshafts of aircraft engines fractured in service. Consequently, the present investigation of twenty two (22) broken and recalled crankshafts was conducted. The investigation included hundreds of metallurgical evaluations, numerous fatigue and fracture tests to determine the cause of the failures. The crankshafts were forged from AMS 6414H (AISI 4340) vacuum arc remelted steels with ultra-low sulfur content of less than 0.001%. The investigation revealed that the crankshafts broke because small cracks created in the forging process became large when the crankshafts were subjected to expected operating loads in aircraft engines. The small cracks were caused by incipient melting overheat at grain boundaries. These cracks continued to grow as the engine accumulated more operating time until they reached a critical size causing a sudden failure.
机译:几个飞机发动机的曲轴在服务中被骨折。因此,进行了对二十二(22)个破碎和召回的曲轴的本研究。调查包括数百种冶金评估,许多疲劳和断裂试验,以确定失败的原因。曲轴由AMS 6414H(AISI 4340)真空弧形熔融钢锻造,具有小于0.001%的超低硫含量。调查显示,曲轴破裂,因为当锻造过程中产生的小裂缝变大,当曲轴在飞机发动机中进行预期的运行负载时变大。小裂缝是由晶界初期熔化过热引起的。由于发动机累积了更多的操作时间,因此这些裂缝继续生长,直到它们达到突然发生故障的临界大小。

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