大型涡轮叶片,large-size turbine blades
1)large-size turbine blades大型涡轮叶片
英文短句/例句
1.Dimensional Accuracy Control of Large-Size Turbine Blade:The Reverse Deformation Technology大型涡轮叶片精密铸造尺寸精度控制研究——反变形技术
2.Dimensional Accuracy Control of Investment Casting Large-Size Turbine Blade--Dimensional Stability of Wax Pattern大型涡轮叶片无余量精密铸造尺寸精度控制研究——蜡模尺寸稳定性
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.Investigation of Turbine Blade Modeling Technique Based on NURBS;基于NURBS的涡轮叶片造型技术研究
5.Effects of leading-edge modification on secondary flow in turbine cascades叶片前缘改型对涡轮叶栅二次流的影响
6.Large eddy simulation of separated flow transition on a highly-loaded low pressure turbine profile大负荷低压涡轮叶型分离转捩流动的大涡模拟
7.conduction-cooled turbine blade(导热)冷却式涡轮叶片
8.Aerodynamic performance of a highly-loaded low-pressure turbine profile一种大负荷低压涡轮叶型的气动性能
9.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
10.Study on the High Temperature Performance of Alumina Ceramic Cores for Investmentcasting Turbine Blades涡轮叶片用氧化铝陶瓷型芯高温性能的研究
11.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
12.Model Registration Control Point Set Selection for Turbine Blade Shape Inspection涡轮叶片形状检测中的模型配准控制点集选取
13.A CAD Model Directing Method for Turbine Blade Density Measurement Data SegmentationCAD模型引导的涡轮叶片密集测量数据分割
14.3D Solid Reconstruction and Error Inspection of Big-Twisted Turbo Blade大扭曲度涡轮叶片的三维实体重构与误差检测
15.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。
16.Turbine Blade Parametric Design Method Based on the Convergence-Diffusion Blade Profiles基于收扩叶型的涡轮叶片参数化造型方法与分析
17.A turbine looks like a large wheel with many small radiating Blades around its rim.涡轮机看上去像是绕中轴转动的有很多叶片的大轮子。
18.Experimental Investigation of the Aerodynamic Performance of Bowed Blades in High-turning Linear Turbine Cascades弯叶片对大转角平面涡轮叶栅气动性能影响的实验研究
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)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 disk-blade涡轮盘-叶片
延伸阅读
大型1.形状或规模大的。
