Full annular rig development of the FT8 gas turbine combustor

被引:0
|
作者
Fox, T.G. [1 ]
Schlein, B.C. [1 ]
机构
[1] Pratt and Whitney Aircraft, East Hartford, United States
关键词
Gas Turbines;
D O I
暂无
中图分类号
学科分类号
摘要
引用
收藏
页码:27 / 32
相关论文
共 50 条
  • [21] Experiment on combustion characteristics of aeroderivative gas turbine twins annular combustor
    Liu A.
    Zhu Y.
    Chen B.
    Liu K.
    Zeng W.
    Wang C.
    Chen, Baodong, 1793, Beijing University of Aeronautics and Astronautics (BUAA) (32): : 1793 - 1800
  • [22] Development of a catalytically assisted combustor for a gas turbine
    Ozawa, Y
    Fujii, T
    Sato, M
    Kanazawa, T
    Inoue, H
    CATALYSIS TODAY, 1999, 47 (1-4) : 399 - 405
  • [23] CHALLENGES IN AERO GAS TURBINE COMBUSTOR DEVELOPMENT
    Maurya, Dalton
    Jayaprakash, G. N.
    Badarinath, C.
    PROCEEDINGS OF THE ASME TURBO EXPO 2009, VOL 2, 2009, : 351 - 357
  • [24] Low NOx Annular Type Combustor for 20 kW Gas Turbine Engine
    Solanki H.K.
    Kulshreshtha D.B.
    Chaudhari N.R.
    Journal of The Institution of Engineers (India): Series C, 2020, 101 (06) : 1035 - 1042
  • [25] Experimental Evaluation of Overload Capability of an Annular Combustor Casing of a Gas Turbine Engine
    S. K. Panigrahi
    N. Sarangi
    U. Chandrasekhar
    Experimental Techniques, 2016, 40 : 841 - 848
  • [26] CHARACTERIZATION OF AVIATION SOOT EMISSIONS WITH A HIGH-PRESSURE GAS TURBINE COMBUSTOR RIG
    Liscinsky, David S.
    Yu, Zhenhong
    Jennings, Archer
    Peck, Jay
    True, Bruce
    Freedman, Andrew
    Herndon, Scott C.
    Miake-Lye, Richard C.
    PROCEEDINGS OF THE ASME TURBO EXPO: TURBINE TECHNICAL CONFERENCE AND EXPOSITION, 2014, VOL 4A, 2014,
  • [27] Experimental Evaluation of Overload Capability of an Annular Combustor Casing of a Gas Turbine Engine
    Panigrahi, S. K.
    Sarangi, N.
    Chandrasekhar, U.
    EXPERIMENTAL TECHNIQUES, 2016, 40 (02) : 841 - 848
  • [28] CHARACTERISTIC TIME IGNITION MODEL EXTENDED TO AN ANNULAR GAS-TURBINE COMBUSTOR
    PETERS, JE
    MELLOR, AM
    JOURNAL OF ENERGY, 1982, 6 (06): : 439 - 441
  • [29] Effect of Spray Cone Angle on Flame Stability in an Annular Gas Turbine Combustor
    Mishra, R. K.
    Kumar, S. Kishore
    Chandel, Sunil
    INTERNATIONAL JOURNAL OF TURBO & JET-ENGINES, 2016, 33 (01) : 35 - 44
  • [30] Assessment of Exit Temperature Pattern Factors in an Annular Gas Turbine Combustor: An Overview
    Muduli, S. K.
    Mishra, R. K.
    Mishra, P. C.
    INTERNATIONAL JOURNAL OF TURBO & JET-ENGINES, 2021, 38 (04) : 351 - 361