空心涡轮叶片,hollow turbine blade
1)hollow turbine blade空心涡轮叶片
1.Numerical simulation of solidification process ofhollow turbine blade of the second generation single crystal superalloy;第二代单晶高温合金空心涡轮叶片凝固过程数值模拟研究
英文短句/例句
1.Research of Detection Extraction of Vane Defects Based on ICT Images;基于锥束CT的空心涡轮叶片缺陷检测技术研究
2.HOLLOW TURBINE BLADE 3D WALL-THICKNESS ANALYSIS BASED ON ITS ICT MEASUREMENT DATA基于工业CT测量数据的空心涡轮叶片三维壁厚分析
3.Surface Grain Refinement Process for Hollow Turbine Blade with Complicated Shape复杂空心涡轮工作叶片表面细晶工艺研究
4.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
5.Research on Aero-engine Blade Containment Test and Computational Simulation;航空发动机涡轮叶片的包容试验和数值仿真
6.Analysis of Stress and Vibration of Blade for Aero Turbocharger小型航空涡轮增压器叶片强度振动研究
7.Maintenance Decision of Aeroengine Turbine Blade Based on Bayes Theory基于Bayes理论的航空发动机涡轮叶片维修决策
8.Development of TBCs on Turbine Blade of Aero-engine热障涂层在航空发动机涡轮叶片上的应用
9.conduction-cooled turbine blade(导热)冷却式涡轮叶片
10.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。
11.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
12.Ceramic Coating of Aeroengine Turbine Blade陶瓷涂层在航空发动机涡轮叶片表面处理中的应用
13.Analysis of vibration depression effect ofpin-attached rotor blades of aero gas turbine engines航空燃气涡轮发动机销接转子叶片的减振效果分析
14.Research on Experimental Technique for Fatigue-Creep Life of the Turbine Blade in Aeroengine航空发动机涡轮叶片疲劳—蠕变寿命试验技术研究
15.Research on Ducted Ram Air Turbine Blade Properties for Pod Power Supply System吊舱发电系统涵道式冲压空气涡轮叶片性能的研究
16.Multidisciplinary Design Optimization for 3D Single-Crystal Turbine Blade;航空发动机三维单晶涡轮叶片的多学科设计优化
17.Research and Development of Electrical Discharge Surface Hardening Equipment Applied to Aero-engine Turbine Labyrinth Teeth;航空发动机涡轮叶片封严篦齿电火花表面强化设备的研制
18.Research on Image Segment in Defect Testing of Turbine Blade;航空发动机涡轮叶片缺陷检测中的关键技术研究
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)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
4)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。
5)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。
6)turbine blade of aeroengine航空发动机涡轮叶片
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
