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Investigation on the microstructure and tensile behavior of a Ni-based IN792 superalloy:

机译:镍基IN792高温合金的显微组织和拉伸行为的研究:

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The Ni-based IN792 superalloy is widely used in aeroengine components because of its low manufacturing cost and good mid-temperature (600°C–900°C) properties. However, its mechanical properties exhibit fluctuation with temperature, so a comprehensive understanding on the tensile behavior of IN792 superalloy at different temperatures is necessary. In this article, IN792 superalloy was fabricated and heat treated with the standard heat treatment of 1120°C/2?h air cooling?+?1080°C/4?h air cooling?+?845°C/24?h air cooling, and its tensile behavior at 550°C, 600°C, 650°C, 700°C, 760°C, 850°C, and 900°C was investigated. The results showed that IN792 superalloy exhibited obvious anomalous yield and intermediate temperature brittleness behaviors. The yield strength and ultimate strength of IN792 superalloy changed little below 760°C, but decreased significantly as the temperature increases to above 760°C. The ductility of IN792 superalloy had a little increase between 550°C and 600°C and then decreased significa...
机译:镍基IN792超级合金由于其较低的制造成本和良好的中温(600°C–900°C)性能而被广泛用于航空发动机部件。但是,其机械性能会随温度而变化,因此有必要全面了解IN792高温合金在不同温度下的拉伸性能。在本文中,制造了IN792超级合金,并通过1120°C / 2?h空冷?+?1080°C / 4?h空冷?+?845°C / 24?h空冷的标准热处理进行了热处理。研究了其在550℃,600℃,650℃,700℃,760℃,850℃和900℃下的拉伸性能。结果表明,IN792高温合金具有明显的异常屈服和中间温度脆性​​行为。在温度低于760°C时,IN792高温合金的屈服强度和极限强度几乎没有变化,但随着温度升高至760°C以上,其屈服强度和极限强度却显着下降。在550°C至600°C之间,IN792高温合金的延展性略有增加,然后显着降低。

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