Microstructure and susceptibility to hot tearing of K424 nickel-based superalloys for turbocharger turbine wheels
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摘要: 針對K424精密鑄造增壓渦輪葉片出現的熱裂問題,采用組織觀察和計算模擬的方法,分析增壓渦輪用K424合金特性以及渦輪葉片鑄造中出現熱裂的原因,并對比K418合金提出合金熱裂傾向性的影響因素以及減少熱裂的建議.結果表明,鑄造增壓渦輪熱裂傾向性與合金特性及鑄件特性等有關.K424合金中Al和Ti元素含量較高,導致合金中共晶組織含量多且尺寸大,與K418合金相比,熱裂傾向性較大;另一方面,由于鑄件葉片位置厚度小且曲率變化大,易形成應力集中,導致熱裂.為減小熱裂傾向性,需控制K424合金中Al和Ti元素含量并選擇合理的工藝參數.Abstract: Hot tearing tends to occur when K424 superalloy is used for a turbocharger turbine wheel. To solve this problem,the alloy characteristics of K424 and K418 superalloys and the factors impacting the susceptibility to hot tearing were studied by microstructure observations and casting simulations. The research proposed the main factors which affected the susceptibility to hot tearing and also the method to reduce hot tearing in the turbine wheel. It is found that the susceptibility to hot tearing of the turbine wheel is influenced by both the alloy characteristics and casting characteristics. K424 superalloy shows a higher susceptibility to hot tearing when compared with K418. Because of high amount of aluminum and titanium in K424 superalloy,the size and the amount of γ + γ' eutectics increase,resulting in more prior forming and propagating areas of hot tearing. On the other hand,due to a smaller thickness and a larger curvature change in the blade margin of the turbine wheel,the uneven distribution of the thermal stress is induced in the end of the solidification process,which leads to hot tearing in this paper. In order to decrease the susceptibility to hot tearing of the turbine wheel,the contents of aluminum and titanium should be controlled,and the reasonable technological parameters of casting should be set to ensure the final effect.
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