1) turbine blade design
涡轮叶片设计
1.
Research of Multidisciplinary Design Optimization(MDO) technology applied to the aeroengine turbine blade design was presented.
叙及了多学科设计优化技术在航空发动机涡轮叶片设计中的应用研究,对涡轮叶片多学科设计优化方法进行设计的具体实施过程进行了介绍,讨论了结构、气动、传热、强度、振动和寿命以及优化算法等跨学科之间进行耦合优化设计的理论和方法。
2) turbine blade cooling design technologies
涡轮冷却叶片设计技术
3) Turbine Blade Process Design
涡轮叶片流程设计
4) 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。
5) 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
6) turbo blade
涡轮叶片
1.
Research and Application of Parting Design for Turbo Blade Mould with the Case- based Reasoning (CBR);
基于事例推理技术的涡轮叶片精铸模分模设计研究与应用
2.
An integration system is set up to meet the need for information integration in the process of mold design and manufacture and detection of aero-engine turbo blade by investment casting.
为满足航空发动机涡轮叶片精铸模具设计、制造、叶片铸件检测流程对信息集成的需求,提出构建精铸模具集成设计系统平台。
3.
Seven stageⅠturbo blades fractured during working time of an engine.
某发动机在服役过程中,有7片Ⅰ级涡轮叶片连续发生断裂或开裂。
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