1)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。
英文短句/例句
1.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
2.A opmizing sequencing of compressor vanes based on simulated annealing partheno genetic algorithm基于退火单亲算法的压气机叶片排序
3.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
4.Research on the Key Manufacture Techniques of Gas Turbine Pressure Blades;燃气轮机压气机叶片重点制造技术的研究
5.Integrated Structure and Vibration Optimization Design of Turbocharger Compressor Blade增压器压气机叶片结构/振动一体化优化设计
6.Multi-objective 3D Aerodynamic Optimization of Twisted Stacking of Compressor Blades压气机叶片扭曲规律的多目标三维气动优化
7.The Analysis on Surface Compositions of Airplane Engine Blade Irradiated by Intense Pulsed Ion Beam强流辐照飞机压气机叶片表层成分分析
8.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
9.The Test of Natural Frequency and The Calculation of Finite Element of Compressor Blade;压气机叶片的固有频率测试和有限元计算
10.Influence of Blade Roughness on Compressor Performance Deterioration压气机叶片粗糙度对其性能衰退的影响研究
11.The Sort Algorithm for the Air-compressor Blade Based on Simulated Annealing Partheno Genetic Algorithm基于退火单亲遗传算法的压气机叶片排序算法
12.Research on Fracture of Compressor Blade Dovetail from Fretting Wear微动磨损引起的压气机叶片榫头断裂故障研究
13.Multi-objective 3D Optimization of Compressor Blade Based on Genetic Algorithm基于遗传算法的压气机叶片的多目标三维优化
14.the blade of a rotor (as in the compressor of a jet engine).喷气式飞机的压缩机的转动体的叶片。
15.Aerodynamic Optimization Design of Vaned Diffuser for Centrifugal Compressor under Stage Environment级环境下离心压气机扩压器叶片气动优化设计
16.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
17.Numerical simulation of the aerodynamics performance of swept and curved blade on the compressor stator叶片弯掠对压气机静子叶片气动性能影响的三维数值模拟
18.Crack Analysis and Research on Compressor Blades in a Typical Aeroengine发动机压气机整流器叶片裂纹成因及对策研究
相关短句/例句
rotor blade of compressor压气机转子叶片
3)splitter compressor大小叶片压气机
4)Axial Compressor Blade轴流压气机叶片
1.Optmizaton and Analysis of Axial Compressor Blade;轴流压气机叶片优化设计及分析
5)bowed compressor blade压气机弯曲叶片
6)vane compressor叶片式压气机
延伸阅读
压气机叶片材料压气机叶片材料materials for compressor blade yoqIJI yeP，on collloo压气机叶片材料(materials for compressorblade)压气机叶片工作在空气氧化锈蚀的环境中，必须有良好的抗氧化锈蚀的能力。在海洋条件下工作时，还要有抗海水腐性的能力。动叶片还需承受很强的离心应力和振动应力等，要求有高的强度、良好的抗振性能、韧性和抗疲劳强度。 现有的重型徽气轮机压气机叶片的工作温度低于500℃，广泛采用含12%~13% Cr的马氏体不锈钢制造动叶片和静叶片.这是由于，12%~13%Cr钢不但有足够的强度，良好的抗氧化腐蚀性能外，还有优良的抗振性能。航空嫌气轮机中为了减轻重量，早期曾广泛采用铝合金做叶片，但由于强度与抗腐蚀性能均较差，现已被俄合金取代。傲合金不仅强度好、较轻，而且抗海水腐蚀的能力强，但高温性能较差，常用作工作温度低于300~400℃的叶片材料。航机改型燃气轮机的压气机叶片一般用铁合金或含Cr不锈钢制造。
