ADVANCED TECHNOLOGY FOR COMBUSTION TURBINE HOT SECTION REPAIR.

被引：0
|
作者：
Fishman, Marv
Griller, Steve L.
Lordi, Francis D.
机构：
来源：
Electric forum | 1984年 / 10卷 / 01期
关键词：
COMBUSTION;
D O I：
暂无
中图分类号：
学科分类号：
摘要：
Hot gas path components in heavy-duty industrial gas turbines are generally designed for theoretical lives of tens of thousands of hours based on extensive laboratory testing, evaluation and service experience. Yet because the effects of corrosion, erosion or foreign object damage are not totally predictable, bucket and nozzle distress requiring repair or replacement is a common concern for all gas turbine users. The enormous growth of industrial gas turbine installations throughout the world in the past 10 years has resulted in the need for and development of an extensive refurbishment industry geared to the repair of costly components in the turbine hot section.
引用
收藏
页码：28 / 32
相关论文
共 50 条
  • [31] Advanced materials for Mercury™ 50 gas turbine combustion system
    Price, Jeffrey
    Kimmel, Josh
    Chen, Xiaoqun
    Bhattacharya, Arun
    Fahme, Anthony
    Otsuka, Joel
    Proceedings of the ASME Turbo Expo 2006, Vol 2, 2006, : 261 - 267
  • [32] Potentials for Pressure Gain Combustion in Advanced Gas Turbine Cycles
    Neumann, Nicolai
    Peitsch, Dieter
    APPLIED SCIENCES-BASEL, 2019, 9 (16):
  • [33] Pulse combustion: An advanced technology for efficient drying
    Zbicinski, I
    Benali, M
    Kudra, T
    CHEMICAL ENGINEERING & TECHNOLOGY, 2002, 25 (07) : 687 - 691
  • [34] The technology for shrouding of blades and repair of steam turbine casing
    1600, Energoprogress
  • [35] Biomass fired hot air gas turbine with fluidized bed combustion
    Gaderer, M.
    Gallmetzer, G.
    Spliethoff, H.
    APPLIED THERMAL ENGINEERING, 2010, 30 (13) : 1594 - 1600
  • [36] Damage of hot gas components in gas turbine due to combustion instabilities
    Verhage, AJL
    Jansen, HJ
    Spiele, H
    OCOS 2000: FROM THERMO-ECONOMICS TO SUSTAINABILITY, PTS 1-4, 2000, : 2049 - 2059
  • [37] Repair technology of surface defects on the castings of turbine blades
    Nerovnyj, V.M.
    Svarochnoe Proizvodstvo, (06): : 42 - 45
  • [38] Special issue on advanced combustion technology in internal combustion engines - Foreword
    Murase, E
    JSME INTERNATIONAL JOURNAL SERIES B-FLUIDS AND THERMAL ENGINEERING, 2005, 48 (04) : 631 - 631
  • [39] Development and application of noninvasive technology for study of combustion in a combustion chamber of gas turbine engine
    Inozemtsev, A. A.
    Sazhenkov, A. N.
    Tsatiashvili, V. V.
    Abramchuk, T. V.
    Shipigusev, V. A.
    Andreeva, T. P.
    Gumerov, A. R.
    Ilyin, A. N.
    Gubaidullin, I. T.
    THERMOPHYSICS AND AEROMECHANICS, 2015, 22 (03) : 359 - 369
  • [40] Development and application of noninvasive technology for study of combustion in a combustion chamber of gas turbine engine
    A.A. Inozemtsev
    A.N. Sazhenkov
    V.V. Tsatiashvili
    T.V. Abramchuk
    V.A. Shipigusev
    T.P. Andreeva
    A.R. Gumerov
    A.N. Ilyin
    I.T. Gubaidullin
    Thermophysics and Aeromechanics, 2015, 22 : 359 - 369
12345