DETECTABLE DATUM MARKERS FOR GAS TURBINE ENGINE COMPONENTS FOR MEASURING DISTORTION

• 1. 检测可流动物质样品中的生物标记物的存在的方法、用于检测可流动物质样品中的生物标记物的检测器组件及用于检测可流动物质样品中的生物标记物的存在的检测器单元 [P] . 中国专利： CN112424607A . 2021-02-26
• 2. 用于燃气涡轮发动机构件的测量扭曲的可检测数据标记 [P] . 中国专利： CN107121121A . 2017-09-01
• 3. DETECTABLE DATUM MARKERS FOR GAS TURBINE ENGINE COMPONENTS FOR MEASURING DISTORTION [P] . 欧洲知识产权局专利： EP3211366B1 . 2019-09-25

  机译： 用于测量变形的燃气轮机发动机组件的可检测基准标记

• 4. Detectable datum markers for gas turbine engine components for measuring distortion [P] . 美国专利： US10030534B2 . 2018-07-24

  机译： 用于燃气涡轮发动机部件的可检测基准标记，用于测量变形

• 5. DETECTABLE DATUM MARKERS FOR GAS TURBINE ENGINE COMPONENTS FOR MEASURING DISTORTION [P] . IN201744005445A . 2017-08-25

  机译： 用于测量变形的燃气轮机发动机组件的可检测基准标记

• 1. Uncertainty of measurement for large product verification: evaluation of large aero gas turbine engine datums [J] . Muelaner J. E., Wang Z., Keogh P. S., Measurement Science & Technology . 2016,第11期
• 2. Strip distortion generator for simulating inlet flow distortion in gas turbine engine ground test facilities [J] . M. Saleem Yusoof, M. Sivapragasam, M.D. Deshpande Propulsion and Power Research . 2016,第4期
• 3. Endwall aerodynamic losses from turbine components within gas turbine engines [J] . Phil Ligrani, Geoffrey Potts, Arshia Fatemi Propulsion and Power Research . 2017,第1期
• 4. Numerical Simulation of Cast Distortion in Gas Turbine Engine Components [C] . A.A.Inozemtsev, A.S. Dubrovskaya, K.A. Dongauser International Conference on Modelling of Casting, Welding and Advanced Solidification Processes . 2015
• 5. Unsteady Reynolds-averaged Navier-Stokes simulations of inlet distortion in the fan system of a gas-turbine aero-engine. [D] . Spotts, Nathan. 2015
• 6. Single-Coil Eddy Current Sensors and Their Application for Monitoring the Dangerous States of Gas-Turbine Engines [O] . Sergey Borovik, Yuriy Sekisov 2020
• 7. Detecting Flaws in the Presence of Strong Geometry Signals in F100 Gas Turbine Engine Components [O] . Ko, Ray T. 1989
• 8. Thermal Residual Stress Relaxation and Distortion in Surface Enhanced Gas Turbine Engine Components [R] . Prevey, P. , Hombach, D. , Mason, P. 1998

• 1. Potentials of manufacture and repair of nickel base turbine components used in aero engines and power plants by laser metal deposition and laser drilling [J] . I.Kelbassa ,K.Walther ,L.Trippe . 航空动力学报 . 2007,第5期
• 2. A real-time measuring technology for studying distortion of hydraulic turbine blade castings during heat treatment process [J] . Yu Hailiang ,Kang Jinwu ,Nie Gang . 中国铸造 . 2011,第003期
• 3. Current Status and Prospects of Supercomputing Used for Gas Turbine Engines Design [J] . Omair Alhatim . 能源与动力工程 . 2016,第002期
• 4. Modelling internal air systems ingas turbine engines [J] . J Michael Owen . 航空动力学报 . 2007,第4期
• 5. PROPERTIES, WELDABILITY AND APPLICATIONS OF ADVANCED WROUGHT SUPERALLOYS FOR GAS TURBINE ENGINES [J] . D.L. Klarstrom ,V.R. Ishwar ,M.D. Rowe . 金属学报：英文版 . 2005,第1期
• 6. 基于单目视觉的三维测量系统及在钢管组件变形检测的应用 [C] . TANG Yun-chao ,唐昀超 ,LI Li-juan . 第26全国结构工程学术会议 . 2017
• 7. 基于捷联基准及变形测量的分布式姿态基准系统研究 [A] . 裴福俊 . 2005