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- 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。
- By comparing data form the controllable calculating program and results of blowing tests,it offers a method to simulate the aerodynamic property of gas turbine blade. 介绍了采用可控扩压计算程序计算的压气机叶片数据与吹风试验结果的对照结论,提出采用可控扩压方法设计的燃气透平叶片的气动性能可以通过程序计算模拟。
- The tool design and tool motion can take care of reaching surfaces such as blind cavities and pockets in walls.ECM is used for machining of gas turbine blades. 另外，电解加工与切削加工相结合（例如电解磨削，电解珩磨，电解研磨等），往往可以取得很好的加工效果。
- The no machining directional solidification hollow turbine blades, hollow guide vans and complex structure parts used in aero engine and gas turbine made by vacuum precision investment casting. 航空发动机、燃机等精铸真空无余量空心涡轮、导向叶片及复杂结构件。多种热处理炉上用料盘,夹具等耐热合金钢精铸件。
- The gas turbine feeds on the fuel it pumps. 燃气轮机以它所抽入的燃料为能源。
- Local Heat Transfer Characteristics in "Impingement-Film" Cooling Style About Inner Side of Gas Turbine Blade 涡轮叶片内"冲击-气膜出流"局部换热特性数值模拟
- First Chinese Instance Base for CAD System of Investment Casting Mould Used in Gas Turbine Blade Manufacture 涡轮叶片精铸模具CAD系统实例库的设计与研究
- The Interior Heat Transfer Characteristics of Gas Turbine Blade Due to Dense Film Cooling Holes 密集型气膜出流内部冷气侧换热特性实验研究
- The Interior Heat Transfer Characteristics of Gas Turbine Blade Due to Sparse Film Cooling Holes 稀疏型气膜出流内部冷气侧换热特性实验研究
- Wuxi Turbine Blade Works Co., Ltd. 无锡透平叶片有限公司。
- Research on Modeling Technologies of Aviation Gas Turbine Blades 航空燃气涡轮叶片造型技术研究
- porous gas turbine blade 多孔燃气涡轮叶片
- The blade of a gas turbine fractured and the unit stopped unnaturally in a refinery. 某炼化厂烟气轮机一动叶片断裂引起停机事故。
- Kawasima T,Iinuma H,Minagawa N.Optical Semiconductor Blade Vibration Monitoring System for Gas Turbine Engine[J]. 胡广书.;数字信号处理之理论、算法与实现[M]
- An Analysis of the Vibration Characteristics of a Gas Turbine Bladed Disc 燃气轮机叶片轮盘振动特性分析
- 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
- Effects of Platform Friction Damper on Resonant Stresses in Gas Turbine Blades 缘板摩擦阻尼器的减振实验研究
- The process of blade root profile in gas turbine and revising calculation of profile of turning tool is discussed in detail in the paper. 就燃气轮机叶片叶根齿形加工及所用车刀刀齿型线的修正计算做了详细论述。
- 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。
- Using 3-D rigid-viscoplastic finite element method, the multi-stage forging process of a gas turbine compressor blade was simulated. 利用刚粘塑性有限元法,对某重型燃机压气机叶片的多工步锻造过程进行了三维有限元模拟。
