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- Repairing Technology of High Pressure Turbine Blade Tip Crack for an Aero -Engine 某型发动机高压涡轮叶片叶尖裂纹修复工艺研究
- Effect of temperature and rotational speed on radial clearance of turbine blade tip 温度与转速对涡轮叶尖径向间隙的影响
- Statistical design for turbine blades tip clearance loss analysis 航空发动机涡轮叶尖间隙损失的统计设计
- turbine blade tip 涡轮叶尖
- Wuxi Turbine Blade Works Co., Ltd. 无锡透平叶片有限公司。
- KEY WORDS Anisotropic, Constitutive model, Viscoplastic, Turbine blade. 关键词：正交异性，本构模型，粘塑性，涡轮叶片
- Abstract: A 3D numerical solution of transonic turbulent flowfield inside a compressor rotor is analyzed with a consideration of blade tip clearance. 文摘:借助于考虑叶片顶部间隙的压气机转子内跨音速湍流流场的三维数值解，得到了该转子流场中的复杂涡系与波系结构。
- Its h.p.and m.p.sealing glands and blade tip sealing were modified with an American adjustable sealing. 1997年7月在第二次大修中引进了美国布莱登可调式汽封，对其高、中压汽封及叶顶汽封进行改造。
- 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。
- 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。
- The wall thickness of the hollow aeroengine turbine blade is a critical parameter for ensuring its strength. 航空发动机空心涡轮叶片的壁厚是保证叶片强度的一个关键参数。
- An example of rabbet feature manufacturability of a turbine blade was given to show the method available. 最后以涡轮叶片榫头特征的可制造性分析为应用实例，说明该方法的有效性和实用性。
- This paper presents the scheme of a versatile robot for on-site repair of hydraulic turbine blade. 介绍了一种多功能的水轮机叶片坑内修复机器人方案和研究进展。
- The RE-aluminizing technique and coating structure of gas turbine blade made of alloy M38G are studied. 研究了涡轮叶片材料M38G合金渗稀土-铝涂层的工艺过程和组织结构。
- The parameter influence of rotor free-wake method was presented, including blade discrete segments, vortices grid density and wake length.Several areas were made from blade root to blade tip. 摘要介绍了自由涡方法中多个参数的影响，包括桨叶离散段数、有弯度翼型的涡网格密度、尾迹的长度。
- This steam is used to turn turbine blades of electric generators. 这蒸汽被用来推动发电机的涡轮叶片。
- The flow separation and great range low energy flow occur at the 10% span range of second rotor blade tip near stall point firstly, which was the main reason for the compressor stall. 在近失速点压气机第二排转子叶片吸力面近尖部10%25叶展范围内，最先出现导致叶片失速的大范围分离和低能堵塞团；
- Turbine blade inspection poses some unique challenges, such as analyzing the twist of a newly manufactured blade compared to the CAD model. 对涡轮叶片检验面临一些独特的挑战,如分析新制造出的叶片相对于CAD模型的扭曲程度。
- Full-Scale Structural Testing of Wind Turbine Blades TS Ed. 风力发电机组叶片满量程试验。
- In this paper, heat transfer and fluid flow in passage for trailing edge of turbine blade with pin-fin arrays is studied numerically. 本文应用湍流模型对涡轮叶片尾缘针肋通道的换热与流动进行了二维数值模拟研究。
