Effect of sintering temperature on ceramic cores performances of SiO2-ZrO2 system

被引:2
|
作者
Liu X.-G. [1 ]
Qi C.-J. [1 ]
He L.-L. [2 ]
Tang D.-Z. [1 ]
Xiao C.-B. [1 ]
Yao J.-S. [1 ]
Gu G.-H. [1 ]
Li X. [3 ]
机构
[1] Beijing Institute of Aeronautic Materials
[2] Avic South Aviation Industry Limited Corporation
[3] Tianjin University
关键词
Ceramic cores; Engine; Hollow blades; Hot-pressure casting; Superalloy;
D O I
10.3969/j.issn.1005-5053.2011.5.012
中图分类号
学科分类号
摘要
The easy leachable SiO2-ZrO2 ceramic cores used in directional solidification and single crystal hollow blades were prepared by traditional hot-pressure casting. The results show that the a sintering shrinkage increased with the increasing sintering temperature from 1150°C to 1250°C, and sintering shrinkage is increased markedly above 1200°C. Well-grown crystalline grains were shown, and main compositions are composed with non-crystal silica, cristobalite and zirconia. The material properties sintering at 1200°C are optimized, and bending strengths reach 42.9MPa, and best anti-deformation and bending strengths are also obtained at 1550°C. High temperature anti-deformation is 0.1mm, and the high temperature bending strength, pore, density and sintering shrinkage are 27.9MPa, 30.4%, 1.92g/cm3 and 0.4% respectively. The formations of cristobalite is about 20%. It meets the pouring requirement for superallay hollow turbine blades of the aero-engine.
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页码:62 / 65
页数:3
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