Developments of cast superalloys and technology for gas turbine blades in BIAM

被引：29

作者：

Chen, RZ ^{[1
]}

机构：

[1] INST AERONAUT MAT,BEIJING 100095,PEOPLES R CHINA

来源：

ADVANCED PERFORMANCE MATERIALS | 1995年 / 2卷 / 03期

关键词：

turbine blade; cast superalloy; crystal orientation control; ceramic core; shell mould;

D O I：

10.1007/BF00705447

中图分类号：

T [工业技术];

学科分类号：

08 ;

摘要：

Since 1960's many important subjects relating to cast turbine blades including alloy developments, directional solidification (DS) and single crystal (SC) technique and casting technology for blades have been performed with great successes in Beijing institute of Aeronautical Materials (BIAM) in order to meet the requirements for developing new aero-engines in China.

引用

页码：249 / 257

页数：9

共 11 条

[1] CHEN RZ, 1993, AVIATION PRODUCTION, P11
[2] Strengthening in a DS casting Ni3Al base alloy IC6
Han, YF
Wang, YM
Chaturvedi, MC
[J]. ADVANCED PERFORMANCE MATERIALS, 1995, 2 (03): : 259 - 268
[3] MA DW, 1984, AVIATION PRODUCTION, P71
[4] SUN CQ, 1987, J AERONAUTICAL MATER, V7, P1
[5] TANG DZ, IN PRESS INVESTIGATI
[6] WANG LB, 1986, CHIN J MET SCI TECHN, V2, P359
[7] Wu Zhongtang, 1987, Acta Metallurgica Sinica, V23, pB171
[8] XIA MY, IN PRESS INVESTIGATI
[9] ZHENG YR, 1992, 7TH P INT S SUP 7 SP, P475
[10] ZHENG YR, 1983, J AERONAUTICAL MATER, V3, P14

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