压气机叶型,compressor blades
1)compressor blades压气机叶型
英文短句/例句
1.The Study of Blade Design of Aspirated Transonic Compressor;跨声速附面层吸气式压气机叶型设计研究
2.Blade Optimization Desighn for a Ground-Based Heavy-Duty Gas Turbine Incorporating Transition Modeling考虑转捩影响的地面重型燃气轮机压气机叶型优化设计
3.Influence of Blade Thickness on Flutter Characteristics in Fan/Compressor风扇/压气机叶型厚度对颤振特性的影响
4.Numerical optimization of compressor blade profile based on the control theory基于控制理论的压气机叶型数值优化方法
5.Optimal Design of Compressor Blade Profile and Aspirated Hole;压气机叶片型面及吹吸气孔优化设计
6.Damage Analysis of High Pressure Compressor Blade in Aero-engine某型发动机高压压气机叶片打伤原因分析
7.A Study on Geometric Methods for Designing Supersonic Aerofoil of Axial Flow Compressor轴流压气机超音叶片叶型几何设计方法的研究
8.Numerical Simulation of the Aerodynamic Performance of the Improved Compressor Blade叶型改型对压气机跨音速叶栅气动性能影响的研究
9.A Study of New Type Configuration of Blade Cascade in Axial Compressors;轴流压气机叶栅新型气动布局结构的研究
10.Verification Test of Troubleshooting Concept for an Aeroengine Compressor Rotor Blade Tip Crack Failure某型发动机压气机转子叶片叶尖裂纹故障排除方案试验验证
11.Research on Laser Measurement System of Vane of Aero-engine Compressor航空压气机叶片型面激光测量系统研究
12.Flow Characteristics of Stator Wake in Small Axial Compressor小型轴流压气机静叶排出口尾迹流动特性
13.interlobe space(容积式压气机) 叶间容积
14.impeller for fans, gas pumps or compressors风扇、气泵或压缩机叶轮
15.An Approximate Calculation of Aerodynamic Load for a Certain Type of Aero-engine Compressor Blade某型航空发动机压气机叶片气动负荷的近似计算
16.Analysis on Manufacturing Technologies of M701F Heavy-duty Gas Turbine Compressor 13 Stage Moving Blade TipM701F重型燃气轮机压气机第13级动叶片的加工工艺分析
17.The Analysis of Vibration and Fracture of the Stage 4 Compressor Blade in a Typical Aeroengine某型发动机第4级压气机叶片振动特性及断裂机理分析
18.Technology of Machining for Inner and Outer Blade Carrier-Ring Localization in Compressor of 266 MW Heavy Gas Turbine266MW重型燃机压气机静叶环内外环国产化加工工艺
相关短句/例句
compressor cascade压气机叶
3)Compressor blade压气机叶片
1.Recent applications and research of erosion resistant coating of compressor blade are summarized.综述了压气机叶片抗冲蚀涂层的研究进展、应用情况以及为了改善涂层性能而进行的多元合金化、多层涂层方面的研究,展望了今后压气机叶片抗冲蚀涂层的发展方向。
2.Fine grain cast IN718 compressor blade form abroad has been analyzed.解剖、分析了国外细晶铸造IN718压气机叶片。
3.The structure design and off set optimization of compressor blades are conducted by the system, and as a result, the blades are restructured.对航空发动机压气机转子叶片结构进行了特征分析和归纳,提取了典型特征结构和特征参数,建立了基于UG软件的压气机叶片特征设计系统,利用该系统进行了叶片的特征结构设计和多种形式的罩量优化,在此基础上对叶片结构进行了重构。
4)Compressor Impeller压气机叶轮
1.Taking into consideration the material nonlinearity of turbocharger compressor impellers and turbine wheels,we carry out elastoplasticity numerical analysis of their burst speed based on FEM software ANSYS.基于ANSYS有限元分析软件,对车用涡轮增压器涡轮叶轮和压气机叶轮进行了材料非线性弹塑性有限元数值分析,计算了涡轮叶轮和压气机叶轮在离心载荷作用下的破裂转速,并与试验结果进行了对比。
2.From the analysis of compressor impeller of vehicle turbocharger stress characters,the calculation and analysis methods of impeller structural strength were described.通过对车用增压器压气机叶轮内应力特点的分析,确定了叶轮强度的计算方法,介绍了利用有限元分析软件对叶轮内部应力进行分析的过程,并就强度分析中的关键步骤和技术难点进行了讨论。
3.A compressor impeller with a diameter of 120 mm has been machined successfully with this system.运用该系统编制了直径 12 0 mm的压气机叶轮的五轴加工程序 ,并成功地进行了叶轮加工 。
5)impeller[英][im"pel?][美][?m"p?l?]压气机叶轮
1.Based on the FE parametric quadratic programming(PQP) method,the stress distribution of 3-D frictional contact problem ofimpeller-shaft sleeve-shaft assembly was analyzed.以某柴油机涡轮增压器的压气机为例,基于多重子结构技术,建立了增压器压气机叶轮、轴套和轴的三维整体有摩擦弹性接触的计算模型,采用有限元参数二次规划法,对其进行有限元分析。
6)compressor stator压气机静叶
1.The potential of predicting separations in turbomachinery of detached eddy simulation (DES) was researched by applying it to simulate high Reynolds-number complex flows ofcompressor stator with massive separations near endwalls.将分离涡模拟方法应用于高雷诺数压气机静叶有大分离的复杂流动计算中,研究该方法对分离的模拟能力。
延伸阅读
压气1.平息怒气。
