1) turbine blade with air cooling
气冷涡轮叶片
1.
Numerical study of 3D heat transfer for turbine blade with air cooling;
气冷涡轮叶片三维换热问题计算
2) directional solidification turbine blade
定向凝固气冷涡轮叶片
1.
This model and algorithm were applied to the analyses of anisothermal visco-plastic creep and damage of an air-cooled directional solidification turbine blade taking into consideration of the.
采用一种考虑损伤的单晶体热—粘塑性变形本构模型和迭代求解数值方法,可以描述单晶在变温过程中的应力应变关系,还可以描述单晶在晶体滑移机制控制下的蠕变变形和孔洞型损伤;考虑定向凝固高温涡轮叶片的柱晶结构,应用本文模型和算法对包含若干个柱晶晶粒的定向凝固气冷涡轮叶片进行不均匀温度场下的变温热粘塑性蠕变和损伤分析。
4) Cooling Turbine blade
涡轮冷却叶片
5) gas-turbine blade
燃气涡轮叶片
6) 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。
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