A method for producing the blade / vane aerofoil emanating from a foot for turbines, compressors and the like.

• 1. 用于修整用于气体涡轮机的压缩机或涡轮机叶片的方法 [P] . 中国专利： CN103079754B . 2016.08.03
• 2. 用于修整用于气体涡轮机的压缩机或涡轮机叶片的方法 [P] . 中国专利： CN103079754A . 2013-05-01
• 3. Aerofoil blade in particular that constituting a vane of turbine engine fan and compressor [P] . PL201181B1 . 2009-03-31

  机译： 尤其是构成涡轮发动机风扇和压缩机叶片的翼型叶片

• 4. AEROFOIL BLADE IN PARTICULAR THAT CONSTITUTING A VANE OF TURBINE ENGINE FAN AND COMPRESSOR [P] . PL344738A1 . 2001-07-02

  机译： 涡轮叶片，特别是构成涡轮发动机风扇和压缩机叶片的叶片

• 5. Process for producing a turbine blade or vane with an oxide on a metallic layer, use of such a turbine blade or vane, a turbine and a method for operating a turbine [P] . 美国专利： US2010061836A1 . 2010-03-11

  机译： 用于在金属层上制造具有氧化物的涡轮叶片或叶片的方法，这种涡轮叶片或叶片的用途，涡轮机以及用于操作涡轮机的方法

• 1. Hashin Failure Theory Based Damage Assessment Methodology of Composite Tidal Turbine Blades and Implications for the Blade Design [J] . YU Guo-qing, REN Yi-ru, ZHANG Tian-tian, 中国海洋工程（英文版） . 2018,第002期
• 2. Modeling Methods and Test Verification of Root Insert Contact Interface for Wind Turbine Blade [J] . Li Hui, Wang Tongguang 南京航空航天大学学报（英文版） . 2016,第001期
• 3. Vibration reliability analysis for aeroengine compressor blade based on support vector machine response surface method [J] . GAO Hai-feng, BAI Guang-chen 中南大学学报（英文版） . 2015,第005期
• 4. DEVELOPMENT OF DESIGN METHOD FOR SUPERSONIC TURBINE AEROFOILS NEAR THE TIP OF LONG BLADES IN STEAM TURBINES PART 2: CONFIGURATION DETAILS AND VALIDATION [C] . Shigeki Senoo, Hideki Ono ASME turbo expo: turbine technical conference and exposition . 2013
• 5. Flow and heat transfer in an L-shaped cooling passage with ribs and pin fins for the trailing edge of a gas-turbine vane and blade. [D] . Pardeshi, Irsha. 2013
• 6. High Sensitive Methods for Health Monitoring of Compressor Blades and Fatigue Detection [O] . Mirosław Witoś 2013
• 7. INFLUENCE OF VANED DIFFUSER ON DANGEROUS BLADE VIBRATION DUE TO BLADE FLOW INTERACTIONS IN A CENTRIFUGAL COMPRESSOR [O] . D. Jin, Z. Jiang, H. Hasemann, 2016

• 1. A　HIGH　PERFORMANCE　DS　CAST　Ni_3Al　BASE　ALLOY　FOR　ADVANCED　GAS　TURBINE　BLADES　AND　VANES [J] . HAN Yafang (Institute of Aeronautical Materials Beijing 100095 China)CHATURVEDIMC(University of Manitoba Winnipeg Manitoba Canada R3T2N2) . 金属学报：英文版 . 1995,第Z1期
• 2. Nonlinear Pre⁃deformation Method for Compressor Rotor Blade [J] . Yongliang Wang ,Shihao Li ,Longkai Zheng . 哈尔滨工业大学学报:英文版 . 2021,第4期
• 3. 用于风机新型叶片设计的典型仿鸮翼翼型气动性能研究 [C] . LI Dian ,李典 ,LIU Xiaomin . 2015第二届中国国际风机学术会议 . 2015
• 4. 基于数据融合的涡轮机叶片振动测量方法研究 [A] . 任三群 . 2017