涡轮机叶片熔覆,turbine blade cladding
1)turbine blade cladding涡轮机叶片熔覆
2)turbine vane涡轮机叶片
3)turbine blading涡轮机叶片装置
4)turbine bucket vibration涡轮机叶片振动
5)turbine disk涡轮机叶片盘
6)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。
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 vane涡轮机叶片
3)turbine blading涡轮机叶片装置
4)turbine bucket vibration涡轮机叶片振动
5)turbine disk涡轮机叶片盘
6)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。
延伸阅读
涡轮机即“透平”(643页)。
