Compared with air blade cooling technology,peformance analysis of various gas turbine cycles using steam blade cooling technology was carried out.
对透平膨胀过程中的传热和作功过程进行简化，建立了叶片冷却的计算模型；采用该模型对简单循环、ＳＴＩＧ和ＩＳＴＩＧ等循环方式中分别采用蒸汽和空气冷却时的性能进行了对比研究，并对在各种循环中蒸汽冷却的应用潜力进行了分
Study on 3D finite element analytic method for vibration characteristics of cooling blade with thermal field;
具有温度场的冷却叶片振动特性计算方法研究
Research on application of micro channel in the blade cooling structure
微小通道在叶片冷却结构中的应用研究
Cooling Passage Design Optimization of Turbine Blades Based on Response Surface Methodology
基于响应面的涡轮叶片冷却通道设计优化
conduction-cooled turbine blade
(导热)冷却式涡轮叶片
Numerical Study on Cooling Deterioration Area Between the Film Cooling Holes of Rotating Blades
旋转叶片气膜冷却孔间冷却死区的数值研究
EFFECT OF TURBULENT INTENSITY ON FULL FILM COVERAGE COOLING EFFECTIVENESS
湍流度对全气膜覆盖冷却叶片的影响
Influence of Various Pin Fin Configurations on Trailing Edge Film Cooling;
不同结构扰流柱对叶片尾缘气膜冷却的影响
Heat Transfer Investigation of Film Cooling on the Leading Edge of Turbine Blade;
涡轮叶片前缘气膜冷却的传热实验研究
Investigation of Trailing Edge Film Cooling by Jets Ejected from a Slot;
涡轮叶片尾缘半劈缝气膜冷却实验研究
Calculate Thermal Field and Analyze Structural Field for Binary Cooling Turbine Blades
双工质冷却涡轮叶片温度场计算与强度分析
Experimental research of turbulated cooling hole machining by ECM
涡轮叶片竹节孔冷却通道电解加工实验研究
APPLICATION OF γ-Re_θ TRANSITION MODEL FOR INTERNAL COOLING SIMULATION
γ-Re_θ转捩模型在内部冷却叶片中的应用
Influence of Air-film Hole Shapes on Turbine Blade Air-film Cooling Effectiveness
气膜孔形状对涡轮叶片气膜冷却效果的影响
Influence of the film cooling hole on the endurance life of the turbine blade
涡轮叶片持久寿命预测中气膜冷却孔的影响
Numerical Investigation of the Flow and Heat Transfer of Steam Cooled Vane;
蒸汽冷却涡轮导向叶片流动与传热的数值模拟和分析
Investigation of the Influence of Density Ratios on Film Cooling on Turbine Blade Surface;
密度比对涡轮叶片气膜冷却特性影响的实验研究
Study on Mechanical Property of Nickel-base Single Crystal Superalloy and Its Application on Cooling Gas Turbine Blade;
镍基单晶合金力学特性及其在冷却涡轮叶片上的应用分析
Recent Advances in the Study of Influence of Air-film Hole Geometrical Structures on Turbine Blade Air-film Cooling
气膜孔几何结构对涡轮叶片气膜冷却影响的研究进展
Conjugate Calculation of Gas Turbine Vanes Cooled with Leading Edge Films
带有前缘气膜冷却燃气轮机叶片的气热耦合研究(英文)