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大尺寸燃气轮机叶片的熔模铸造工艺 被引量:11
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作者 孔胜国 《铸造》 CAS CSCD 北大核心 2012年第10期1138-1141,共4页
介绍了大尺寸燃气轮机叶片熔模铸造工艺现状,重点列举了叶片熔模铸造的几个关键过程:模具设计及制造、蜡模尺寸控制、型壳制造工艺、定向和单晶叶片技术等。并指出了大尺寸燃机叶片熔模铸造工艺的几种关键技术目前的发展方向。
关键词 大尺寸叶片 熔模铸造 关键技术
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Directional solidification casting technology of heavy-duty gas turbine blade with liquid metal cooling(LMC) process 被引量:5
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作者 Xiao-fu Liu Yan-chun Lou +5 位作者 Bo Yu Gui-qiao Su Chang-chun Li Xin-li Guo Biao Li Guo-yan Shui 《China Foundry》 SCIE 2019年第1期23-30,共8页
In this work, some important factors such as ceramic shell strength, heat preservation temperature, standing time and withdrawal rate, which influence the formability of directionally solidified large-size blades of h... In this work, some important factors such as ceramic shell strength, heat preservation temperature, standing time and withdrawal rate, which influence the formability of directionally solidified large-size blades of heavy-duty gas turbine with the liquid metal cooling(LMC) process, were studied through the method of microstructure analysis combining. The results show that the ceramic shell with medium strength(the high temperature flexural strength is 8 MPa, the flexural strength after thermal shock resistance is 12 MPa and the residual flexural strength is 20 MPa) can prevent the rupture and runout of the blade. The appropriate temperature(1,520 ℃ for upper region and 1,500 ℃ for lower region) of the heating furnace can eliminate the wide-angle grain boundary, the deviation of grain and the run-out caused by the shell crack. The holding time after pouring(3-5 min) can promote the growth of competitive grains and avoid a great deviation of columnar grains along the crystal orientation <001>, resulting in a straight and uniform grain structure. In addition, to avoid the formation of wrinkles and to ensure a smooth blade surface, the withdrawal rate should be no greater than the growth rate of grain. It is also found that the dendritic space of the blade decreases with the rise of solidification rate, and increases with the enlarging distance between the solidification position and the chill plate. 展开更多
关键词 liquid METAL COOLING (LMC) HEAVY-DUTY gas turbine large-size blade directional SOLIDIFICATION microstructure
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重型燃机大尺寸叶片定向凝固组织模拟 被引量:3
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作者 李海松 杨啊涛 +2 位作者 张琼元 杨照宏 杨功显 《特种铸造及有色合金》 CAS 北大核心 2020年第9期980-984,共5页
采用CAFE模型对某重型燃机大尺寸动叶片定向凝固组织进行了数值模拟。结果表明,叶根朝下组模时,柱状晶尺寸细小,偏离度和发散度较小,叶根晶粒尺寸细小,叶顶晶粒尺寸粗大;叶顶朝下组模时,柱状晶粗大,偏离度和发散度较大,叶顶晶粒细小,叶... 采用CAFE模型对某重型燃机大尺寸动叶片定向凝固组织进行了数值模拟。结果表明,叶根朝下组模时,柱状晶尺寸细小,偏离度和发散度较小,叶根晶粒尺寸细小,叶顶晶粒尺寸粗大;叶顶朝下组模时,柱状晶粗大,偏离度和发散度较大,叶顶晶粒细小,叶根晶粒粗大。抽拉速率对柱状晶组织的影响与组模方式相关性不大,抽拉速率越大,柱状晶尺寸越小,偏离度和发散度越小。试生产发现,数值模拟结果和试验结果符合较好。 展开更多
关键词 重型燃机 大尺寸动叶片 定向凝固 偏离度 发散度
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厚大实心双联叶片工艺研究
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作者 穆森 闵蓉 《特种铸造及有色合金》 CAS 北大核心 2019年第12期1335-1337,共3页
对某厚大实心双联叶片晶粒度超差、铸件叶型鼓胀及尺寸超差、缘板缩松等问题进行分析,通过降低浇注温度、采用复合型壳、陶瓷棉包裹及优化蜡模压制参数和防变形工艺条、应用制壳工艺筋和局部型壳增强等措施,解决了上述问题。
关键词 厚大实心双联叶片 晶粒度超差 尺寸超差 缩松
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