Optical diagnostics applied to a gas turbine pilot burner

被引：0
|
作者：
Seyfried, H. [1 ,4 ]
Brackmann, C. [1 ,4 ]
Lindholm, A. [1 ,4 ]
Linne, M. [1 ,4 ]
Barreras, F. [2 ]
Bank, R.V.D. [3 ]
机构：
[1] Lund University, S-221 00, Lund, Sweden
[2] Laboratory for Research in Combustion Technology, Spanish National Research Council, 50018 Zaragoza, Spain
[3] Rolls-Royce Deutschland, Ltd., Company KG, 15827 Blankenfelde-Mahlow, Germany
[4] Division of Combustion Physics, Faculty of Engineering LTH
来源：
AIAA Journal | 2007年 / 45卷 / 11期
关键词：
This paper presents the application of several optical measurement techniques for the characterization of the combustion behavior of the pilot burner of a gas turbine combustor developed according to the lean premixed prevaporized concept The vaporization of the kerosene fuel (Jet-A) injected by a pilot spray and its consequent mixing with air has been visualized using combined laser-induced fluorescence and Mie scattering measurements. The laser-induced fluorescence/Mie measurements can be used to estimate the length and time scales for evaporation and mixing with air of kerosene (Jet-A) for the lean; premixed; and prevaporized pilot burner. In addition; the feasibility of using laser-induced incandescence for soot characterization has been investigated. Finally; spontaneous flame emission (i.e; chemiluminescence and thermal radiation) have been measured providing information on the overall characteristics of the combustion;
D O I：
暂无
中图分类号：
学科分类号：
摘要：
Journal article (JA)
引用
收藏
页码：2702 / 2709
相关论文
共 50 条
  • [1] Optical diagnostics applied to a gas turbine pilot burner
    Seyfried, H.
    Brackmann, C.
    Lindholm, A.
    Linne, M.
    Barreras, F.
    v. d. Bank, R.
    AIAA JOURNAL, 2007, 45 (11) : 2702 - 2709
  • [2] Optical diagnostics in gas turbine combustors
    Woodruff, SD
    PROCESS MONITORING WITH OPTICAL FIBERS AND HARSH ENVIRONMENT SENSORS, 1999, 3538 : 92 - 98
  • [3] PILOT-PILOT INTERACTION EFFECTS ON A PROTOTYPE DLE GAS TURBINE BURNER COMBUSTION
    Kundu, Atanu
    Klingmann, Jens
    Subash, Arman Ahamed
    Collin, Robert
    PROCEEDINGS OF THE ASME TURBO EXPO: TURBINE TECHNICAL CONFERENCE AND EXPOSITION, 2016, VOL 4B, 2016,
  • [4] Optical control and diagnostics sensors for gas turbine machinery
    Trolinger, James D.
    Jenkins, Thomas P.
    Heeg, Bauke
    PHOTONIC INNOVATIONS AND SOLUTIONS FOR COMPLEX ENVIRONMENTS AND SYSTEMS (PISCES), 2012, 8482
  • [5] High-Speed Fuel/Hydroxyl Radical Imaging in a Gas Turbine Pilot Burner
    Lantz, A.
    Collin, R.
    Sjoholm, J.
    Li, Z. S.
    Petersson, P.
    Alden, M.
    AIAA JOURNAL, 2012, 50 (04) : 971 - 976
  • [6] ASSESSMENT OF THE COMBUSTION BEHAVIOR OF A PILOT-SCALE GAS TURBINE BURNER USING IMAGE PROCESSING
    De Giorgi, Maria Grazia
    Sciolti, Aldebara
    Campilongo, Stefano
    Ficarella, Antonio
    PROCEEDINGS OF THE ASME POWER CONFERENCE, 2014, VOL 1, 2014,
  • [7] Numerical Simulation Of Burner For Micro Gas Turbine
    Jia Lei
    Liu Shi
    Huang Yaosong
    Wang Neng
    Wang Fuzhen
    Li Zhihong
    ADVANCED MATERIALS DESIGN AND MECHANICS, 2012, 569 : 51 - 55
  • [8] Failure analysis of gas turbine burner tips
    Pelaseyed, S. S.
    Attarian, M.
    Kermajani, M.
    Abdi, A.
    ENGINEERING FAILURE ANALYSIS, 2019, 99 : 7 - 17
  • [9] Naval gas turbine diagnostics
    Charchalis, A
    Korczewski, Z
    MARINE TECHNOLOGY II, 1997, : 227 - 236
  • [10] A review of gas turbine engine with inter-stage turbine burner
    Yin, Feijia
    Rao, Arvind Gangoli
    PROGRESS IN AEROSPACE SCIENCES, 2020, 121
12345