涡轮叶片,Turbine blade
1)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
英文短句/例句
1.conduction-cooled turbine blade(导热)冷却式涡轮叶片
2.Check no damage for fan blades and turbine blades.检查风扇叶片和涡轮叶片无损坏迹象。
3.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
4.This steam is used to turn turbine blades of electric generators.这蒸汽被用来推动发电机的涡轮叶片。
5.Investigation of Turbine Blade Modeling Technique Based on NURBS;基于NURBS的涡轮叶片造型技术研究
6.Study on Temperature and Displacement Detection Technique for Turbine Blades;涡轮叶片温度和位移的检测技术研究
7.Study of Creep Grinding on Superalloy for Turbine Blade高温合金涡轮叶片缓进磨削工艺研究
8.Research of multiaxial fatigue-creep life prediction for turbine blade涡轮叶片多轴低周疲劳/蠕变寿命研究
9.Research on Infrared Thermal Wave Non-destructive Inspection Technology of Turbine Blades涡轮叶片红外热波无损检测技术研究
10.Hierarchical B-spline Surface Fitting of Turbine Blades涡轮叶片叶面B-spline曲面层次化拟合方法
11.Overheating Damage Analysis on Turbo-disk and Turbo-blades Used in Locomotive Turbocharger Heated by High-temperature and Short-time一种增压器涡轮盘和涡轮叶片短时超温损伤分析
12.NUMERICAL SIMULATION OF INFLUENCE OF UNSTEADY WAKE ON HEAT TRANSFER OF TURBINE BLADE非定常尾迹对涡轮叶片换热影响的数值模拟
13.Application study of new mould-parting technology of ceramic core mould to turbine blade涡轮叶片陶瓷型芯模具分模技术应用研究
14.DZ4 Alloy Direction Detection Coagulation Turbine Blade Recrystallization Experimental Study;DZ4合金定向凝固涡轮叶片再结晶试验研究
15.Experimental Study and Analysis of the Endurance Properties of Directionally Solidified Turbine Blade;定向凝固涡轮叶片持久性能试验研究与分析
16.Primary Development of High Strength and Hot Corrosion Resistance Aero-Engine Turbine Blade Material DZ68 Alloy;高强抗热腐蚀航空涡轮叶片材料（DZ68）的初步研制
17.The Research of the Accuracy Control of Turbine Blade Based on Displacement Field from Precise Cast;基于位移场的精铸涡轮叶片误差分析系统研究
18.Heat Transfer Investigation of Film Cooling on the Leading Edge of Turbine Blade;涡轮叶片前缘气膜冷却的传热实验研究
相关短句/例句
turbine blades涡轮叶片
1.Parametric design ofturbine 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 gasturbine 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。
3)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-engineturbo 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。
4)turbine vane涡轮叶片
1.Precise reconstruction technology of curved surface ofturbine vane;涡轮叶片曲面的精确重构技术
2.The third classturbine vanes of some engine have fractured three times successively.某发动机Ⅲ级涡轮叶片连续发生三起断裂失效,对这三个叶片的设计强度、材质进行了综合分析,并对三叶片的断口源区及源区附近的断裂细节特征进行了研究,对断口裂纹扩展区进行了定量分析,计算出了叶片的疲劳扩展寿命,并据此给出了叶片的定期检查周期。
3.Therefore, eliminating these grain boundries can improve the resistance ofturbine vane cracks, based on which directly solidification was developed.但是，在高性能的航空发动机的研制中，仅靠先进的冷却技术、发展新型耐高温合金和改进涡轮叶片的制造工艺(定向、单晶)，难以满足安全可靠工作所需的高温蠕变强度，抗高温氧化和热腐蚀能力。
5)Turbine disk-blade涡轮盘-叶片
6)turbine vane涡轮机叶片
延伸阅读
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
