1) Turbine disk-blade
涡轮盘-叶片
2) turbine disk
涡轮机叶片盘
3) turbine blade-disc
涡轮盘-片
1.
Research on residual life prediction of turbine blade-disc under radon environment
随机环境下涡轮盘-片剩余寿命预测方法
4) turbine disc-blade
涡轮盘片
5) turbine blades
涡轮叶片
1.
Parametric design of turbine blades based on feature modeling;
基于特征造型技术的涡轮叶片参数化设计
2.
Research on Fatigue Life of Large Gas Turbine Blades;
大型燃气轮机涡轮叶片疲劳寿命研究
3.
The single crystal Ni-base superalloys were widely used for manufacturing advance gas turbine blades,but the ignored weakness of these alloys to date is that the extent of primary creep at intermediate temperature is much higher than that at high temperature.
单晶镍基高温合金已广泛用于制造先进燃气涡轮叶片,但这种合金至今仍被忽视的薄弱环节是它的中温Ⅰ阶蠕变伸长量远高于高温蠕变,而且与高温蠕变相比,中温Ⅰ阶蠕变对取向偏离、合金成分和热处理组织的变化更为敏感。
6) Turbine blade
涡轮叶片
1.
Error Analysis on Turbine Blade;
精铸涡轮叶片的误差分析技术
2.
Displacement transfer with the mesh deformation method in multidisciplinary optimization of turbine blades;
基于网格变形技术的涡轮叶片变形传递
3.
Turbine blade design and optimization based on the combination means of parametric-Bezier curve;
基于参数法和贝塞尔曲线的涡轮叶片造型及其优化
补充资料：MS6001系列燃气轮机一级空心涡轮叶片
MS6001系列燃气轮机一级空心涡轮叶片
Ms6()()l系列燃气轮机一级空心涡轮叶片 中同科学院金属研究所供稿
说明：补充资料仅用于学习参考，请勿用于其它任何用途。
参考词条