Rated Estimate of Gas Turbine Engine Compressor Blade Survivability.

被引：0
|
作者：
Prokopenko, A.V.
Baumshtein, M.V.
机构：
来源：
Problemy Prochnosti | 1981年 / 05期
关键词：
Compendex;
D O I：
暂无
中图分类号：
学科分类号：
摘要：
GAS TURBINES
引用
收藏
相关论文
共 50 条
  • [21] Pitting Corrosion Induced Fatigue Fracture on a Gas Turbine Compressor Blade
    Neidel, A.
    Riesenbeck, S.
    PRAKTISCHE METALLOGRAPHIE-PRACTICAL METALLOGRAPHY, 2012, 49 (01): : 35 - 48
  • [22] RIG TESTING OF THE OPERABILITY OF A TRANSONIC COMPRESSOR BLADE OF AN INDUSTRIAL GAS TURBINE
    Kang, Hyunsu
    Ahn, Sungjong
    Hwang, Kyusic
    Bock, Justin
    Kang, Jeongseek
    Montgomery, Matthew
    PROCEEDINGS OF THE ASME TURBO EXPO: TURBOMACHINERY TECHNICAL CONFERENCE AND EXPOSITION, 2019, VOL 7A, 2019,
  • [23] Root cause analysis of a gas turbine compressor stator blade failure
    Gavelli, Filippo
    Foulds, Jude
    Sire, Robert
    Kytomaa, Harri
    Proceedings of the ASME Power Conference 2005, Pts A and B, 2005, : 1215 - 1223
  • [24] Failure analysis of blades and vanes of a compressor for a gas turbine engine
    Kwon, Hyeok-Jun
    Lee, Dooyoul
    Lee, Young-Kook
    ENGINEERING FAILURE ANALYSIS, 2021, 124
  • [25] SPLIT COMPRESSOR DIFFERENTIAL GAS TURBINE ENGINE FOR VEHICLE PROPULSION
    DOYLE, GN
    WILKINSO.TS
    PARSONS, CA
    MECHANICAL ENGINEERING, 1966, 88 (06) : 70 - &
  • [26] Failure Investigation of a 6th Stage Compressor Blade on a ETF40B Gas Turbine Engine
    Slogar, Gerrick
    Prus, Gary
    Canilang, Benjamin
    PROCEEDINGS OF THE ASME TURBO EXPO 2011, VOL 4, 2012, : 843 - 852
  • [27] INFLUENCE OF BLADE FILLETS ON THE PERFORMANCE OF A 15 STAGE GAS TURBINE COMPRESSOR
    Kuegeler, E.
    Nuernberger, D.
    Weber, A.
    Engel, K.
    PROCEEDINGS OF THE ASME TURBO EXPO 2008, VOL 6, PT A, 2008, : 415 - 424
  • [28] Metallurgical failure analysis of a rotating blade in the compressor section of a gas turbine
    Ellis, Fred V.
    JOURNAL OF PRESSURE VESSEL TECHNOLOGY-TRANSACTIONS OF THE ASME, 2006, 128 (04): : 632 - 637
  • [29] Development of a Throughflow-Based Simulation Tool for Preliminary Compressor Design Considering Blade Geometry in Gas Turbine Engine
    Liu, Xiaoheng
    Wan, Ke
    Jin, Donghai
    Gui, Xingmin
    APPLIED SCIENCES-BASEL, 2021, 11 (01): : 1 - 22
  • [30] Erosion performance and characterization of nanolayer (Ti,Cr)N hard coatings for gas turbine engine compressor blade applications
    Reedy, Michael W.
    Eden, Timothy J.
    Potter, John K.
    Wolfe, Douglas E.
    SURFACE & COATINGS TECHNOLOGY, 2011, 206 (2-3): : 464 - 472
12345