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涡轮     
相关语句
  turbine
     Study on Crack Growth Life of Powder Metallurgy Superalloy Turbine Disk Containing Inclusions
     含夹杂粉末高温合金涡轮盘裂纹扩展寿命研究
短句来源
     The Research on the Turbine Classifier and the System Properties as Well as the Numerical Simulation of Classification Flow Field
     涡轮分级机及其系统的性能研究与分级流场的计算机仿真
短句来源
     Anti-Erosion Theory on Elastic Coating of Hydraulic Turbine and Its Application
     水机涡轮弹性涂层抗冲蚀理论及应用
短句来源
     Calculation of Temperature Field and Thermal Stress of Turbine Disk with Finite Element Method
     用有限单元法计算涡轮盘的温度场和热应力
短句来源
     THE EXPERIMENT RESEARCH ON THE TURBINE DESIGN OF CIRCULATION CONTROL METHOD
     控制环量设计涡轮的实验研究
短句来源
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  turbines
     Two speed control loop schemes for power turbines of turboshaft engine are analyzed by comparison.
     比较分析了航空涡轴发动机动力涡轮转速回路的2种控制方案(单回路控制方案和串级控制方案)。
短句来源
     A VARYING SPECIFIC HEAT METHOD FOR S 2 CALCULATION OF MULTI-STAGE TURBINES
     多级涡轮S_2流面的变比热气动热力计算方法
短句来源
     The properties of coatings for hot corroxion protection of gas turbines operating in a lower grade diesel oil in foreign countries was briefly introduced. The best protective effects of rich - Cr MCr Al X ( M=Ni,Co,Ni Co,X=Y ,Si,Hf) coating was defined.
     介绍了国外燃用低质柴油的地面燃机一级涡轮叶片及导向叶片防护涂层的抗腐蚀性能 ,肯定了高 Cr- MCr Al X (M=Ni、 Co、 Ni Co,X=Y、 Si、 Hf)涂层防护效果。
短句来源
     Variable Specific Heat Model for Gas Turbines Simulation Calculations Using Modelica and Dymola
     采用Modelica和Dymola的燃气涡轮的变比热仿真计算模型
短句来源
     Analysis on The Loss Model of Variable Geometry Turbines
     变几何燃气涡轮损失模型的分析
短句来源
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  turbo
     On Strengthening the Friction Welding Joint between K418 Turbo Disk and 42CrMo Shaft
     K418涡轮盘和42CrMo轴摩擦焊接头的强化
短句来源
     Analysis of the Unqualified Cause of Impact Toughness of Turbo Disc(1Cr11MoV Steel) of Model 2N261 Turbocharger
     ZN261增压器涡轮盘(1Cr11MoV钢)冲击韧性不合格原因分析
短句来源
     It is pointed out that torque characteristics are optimized,torques in the range from1750r /min to4600r /min held on210N·m,when the AUDI A6engine is equipped with the exhaust turbo charge r.
     指出AudiA6发动机装备废气涡轮增压器后,优化了扭矩输出特性,使得在1750r/min~4600r/min内均保持在210N·m的大扭矩输出。
短句来源
     MRCP used non breath hold heavily T 2 weighted turbo spin echo (TSE) sequence with respiratory triggering and fat suppression techniques (TR/TE=2000/700ms).
     MRCP采用不屏气涡轮自旋回波(TSE)序列的重度T2加权像扫描(TR/TE=2000ms/700ms),并应用呼吸触发及脂肪抑制技术。
短句来源
     Abstract The vacuum system with the turbo molecular pump is used to helium mass spectrometer leakdetector, ZhP-30,detecting in the type of the counter diffusion;
     ZhP-30型氦质谱检漏仪采用涡轮分子泵真空系统,以逆扩散方式检漏;
短句来源
更多       
  a turbine
     Reliability Research for the Low Cycle Fatigue Life of a Turbine Disk
     涡轮盘低循环疲劳寿命可靠性研究
短句来源
     Dynamic Characteristics Study of a Power Turbine Rotor of a Turbine Shaft Engine
     涡轴发动机动力涡轮转子动力特性研究
短句来源
     A turbine aerodynamic design system is established that is capable for modeling of a bowed - twist - sweep blade with analysis and optimization of the flow field structure applied to the aerodynamic design.
     通过将结构分析与优化引申到气动设计中,建立了具有弯、扭、掠叶片流场结构分析能力的燃气涡轮气动设计体系,并将这一体系进一步划分为四个子体系。
短句来源
     The transient temperature and stress field during starting of a turbine first stage disc's 3-dimensional model has been calculated by using the general finite element calculation program ANSYS.
     用通用有限元计算程序ANSYS对某燃气轮机启动过程中透平第一级涡轮盘的三维模型瞬态温度和应力场进行计算。
短句来源
     A turbine impeller viscometer has been used for determining the rheological properties of filamentous erythromycine fermentation broth. In the whole fermentation process fermentation broth behaves as Casson-fluid. Rheological equation can be shown as, τ(t)~(1/2)=τ_0(t)~(1/2)+K_c(t)(?)
     采用涡轮搅拌桨粘度计,测定了丝状菌丝体红霉素发酵液的流变性质在整个发酵过程中发酵液呈Casson型流体,流变方程为τ(t)~(1/2)=τ_o(t)~(1/2)+K_c(t)(?)
短句来源
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  turbine
Imitation of the characteristics of the wind turbine based on DC motor
      
This paper analyzed the operating principles and power and torque characteristics of the wind turbine and the direct current motor (DC motor), and investigated the operating characteristics of the wind turbine compared to that of the DC motor.
      
The torque imitation scheme, which has good performance and high feasibility, together with the whole wind turbine imitation system, was provided.
      
The wind turbine imitation system includes not only a hardware platform composed of PC, data-collection board and thyristor-based velocity-regulator, but also monitor software of wind turbine imitation.
      
As an example, the component numbers of an industrial steam turbine product family is forecasted, forecast result verified and forecast error analyzed.
      
更多          
  turbines
Optimization model for rotor blades of horizontal axis wind turbines
      
This paper presents an optimization model for rotor blades of horizontal axis wind turbines.
      
Heat transfer coefficient of wheel rim of large capacity steam turbines
      
A way of calculating the overall equivalent heat transfer coefficient of wheel rims of large capacity steam turbines is presented.
      
Such cavities are encountered, for example, in the rotors of steam and gas turbines.
      
更多          
  turbo
Corresponding research indicated that SNR estimation deviation degraded the performance of Turbo decoding significantly.
      
In this paper, MAP decoding algorithm with SNR estimation deviation was investigated in detail, and the degradation mechanism of Turbo decoding was explained analytically.
      
The theoretical analysis and computer simulation disclosed the specific reasons for the performance degradation when SNR estimation was less than the actual value, and for the higher sensitivity of SNR estimation to long-frame Turbo codes.
      
Sensitivity analysis of torsional vibration behavior of the shafting of a turbo generator set to changes of its mechanical param
      
Aiming at a 300 MW turbo-generator model, the sensitivity of natural torsional frequencies and modes of torsional vibration (TV) to the rotational inertia and stiffness of the turbo-generator were analyzed.
      
更多          
  a turbine
In a flow through the rim of a turbine machine between the convex and concave surfaces of adjacent blades there arises a transverse gradient of the static pressure.
      
Investigation of two-dimensional transonic flow of a gas through a turbine cascade by a combined method of integral equations an
      
Two numerical methods are basically used to calculate two-dimensional separationless steady flow of an inviscid compressible fluid through a turbine cascade.
      
In an investigation of the flutter of turbines it is necessary to know what is the influence on the unsteady aerodynamic characteristics of a cascade of oscillating profiles of the interaction of cascades in a turbine.
      
Solution of the problem of optimum boundary layer control on the porous surface of a turbine blade
      
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