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HOT CRACKING OF ALLVAC 718PLUS, ALLOY 718 AND WASPALOY AT VARESTRAINT TESTING

机译:拉西雷引用的Allvac 718Plus,合金718和Waspaloy的热裂化

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Varestraint testing together with DSC and SEM-EDX analyses have been performed as means of investigating the hot cracking susceptibility of Allvac 718Plus, alloy 718 and Waspaloy. The solidification sequences in Allvac 718Plus and alloy 718 were very similar to each other starting by an initial solidification of the gamma phase, gamma/MC reaction at around 1260 C and then finally ending the sequence by gamma/Laves eutectic reaction at around 1150 C. Waspaloy had the same solidification sequence, except no Laves phase formation takes place, and solidification started at a somewhat higher temperature as compared to alloy 718 and the solidification sequence ends by a gamma/MC reaction at around 1245 C. The total amount of hot cracking in Waspaloy was shown to be much less than that in alloy 718 and in Allvac 718Plus which is believed to be related to the presence of the Laves eutectic in the latter two alloys with corresponding larger solidification ranges. Hot cracking of 718Plus is slightly less than in 718.
机译:使用DSC和SEM-EDX分析的紫杉鸟测试作为研究全瓦克718Plus,合金718和蜂马洛伊的热裂化敏感性的方法。通过伽马相的初始凝固,γ/ MC反应在约1260℃的初始凝固开始,γ/ MC反应的凝固序列在彼此非常相似,然后在1150℃下通过γ/ Laves共晶反应结束序列。沃斯帕洛尹合金具有相同的凝固顺序,除了没有Laves相的形成发生,并且凝固在稍微更高的温度下开始作为在约1245℃。热裂纹的总量相比,通过伽马/ MC反应合金718条凝固序列两端在黄蜂中被证明远低于合金718和在全vac 718Plus中,其被认为与后两种合金中的Laves共肠的存在有关,具有相应的较大凝固范围。 718plus的热裂纹略低于718。

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