Lean Blowout Proximity Sensing in a Low Emission Liquid-Fueled Combustor

被引:0
|
作者
Bompelly, Ravi K. [1 ]
Seitzman, Jerry [2 ]
机构
[1] Mahindra Univ, Dept Mech & Aerosp Engn, Survey 62-1A, Hyderabad 500043, India
[2] Georgia Inst Technol, Sch Aerosp Engn, Atlanta, GA USA
关键词
Lean blowout; LBO; LBO proximity sensing; LBO detection; lean direct injection; LDI; Chemiluminescence; CH-ASTERISK CHEMILUMINESCENCE; HEAT RELEASE RATE; ACTIVE CONTROL; PREDICTION; DYNAMICS;
D O I
10.1080/00102202.2024.2372433
中图分类号
O414.1 [热力学];
学科分类号
摘要
Advanced aircraft engine combustor designs, intended for achieving low NOx emissions, necessitate lean combustion with small operating margins above the LBO boundary, posing a high risk of exhibiting lean blowout (LBO) problems. Employing active LBO controllers receiving input from LBO proximity sensors can allow for narrower margins, thereby yielding multiple performance gains. Although several previous studies investigated LBO proximity sensing, they predominantly focused on premixed gas-fueled combustors. The application of proximity sensing approaches to liquid-fueled combustor designs, relevant to aircraft engines have not received adequate attention. Therefore, this study investigates LBO proximity sensing in a low emission lean direct injection (LDI) liquid-fueled combustor design developed by NASA. The combustor operates at atmospheric pressure with preheated air. The proximity sensing is examined by analyzing both OH* and CH* chemiluminescence signals, with a focus on assessing their relative performances. The signal analysis approaches include spectral, partial extinction event (LBO precursor) detection, signal RMS, and the CH*/OH* ratio, with an emphasis on the first two methods. Both steady-state and transient operating conditions have been examined. The combustor did not exhibit large-scale flame partial extinction and re-ignition events near LBO, as commonly observed in gas-fueled combustors. However, an increase in flame unsteadiness and partial extinction events with very subtle signatures in optical signals, have been observed. Low-pass filtering has been observed to considerably enhance the precursor signatures enabling their improved detection. With a reduction in LBO margin, an increase in signal low-frequency power, RMS, and precursor event occurrence rate have been observed, which were utilized for providing LBO proximity measures. A key finding from this study is that CH* signals provide significantly superior performance compared to OH* for the proximity sensing in all the approaches, and the potential reasons are discussed.
引用
收藏
页数:27
相关论文
共 50 条
  • [41] Sound Pressure Level Analysis of a Liquid-Fueled Lean Premixed Swirl Burner with Various Quarls
    Novotni, Gergely, I
    Jozsa, Viktor
    ACOUSTICS, 2020, 2 (01): : 131 - 146
  • [42] Influence of Swirl and Primary Zone Airflow Rate on the Emissions and Performance of a Liquid-Fueled Gas Turbine Combustor
    Lokini, Parneeth
    Roshan, Dinesh Kumar
    Kushari, Abhijit
    JOURNAL OF ENERGY RESOURCES TECHNOLOGY-TRANSACTIONS OF THE ASME, 2019, 141 (06):
  • [43] Experimental Investigations on Detonation Initiation Characteristics of a Liquid-Fueled Pulse Detonation Combustor at Different Inlet Air Temperatures
    Tan, Wenhao
    Zheng, Longxi
    Lu, Jie
    Wang, Lingyi
    Zhou, Daoen
    ENERGIES, 2022, 15 (23)
  • [44] Forced Flame Response of Turbulent Liquid-Fueled Lean-Direct-Injection Combustion to Fuel Modulations
    Yi, Tongxun
    Santavicca, Domenic A.
    JOURNAL OF PROPULSION AND POWER, 2009, 25 (06) : 1259 - 1271
  • [45] Recent advances in combustion flowfield imaging measurements in high pressure, liquid-fueled, gas turbine combustor concepts
    Locke, RJ
    Hicks, YR
    Zaller, M
    Anderson, RC
    OPTICAL ONLINE INDUSTRIAL PROCESS MONITORING, 1999, 3859 : 80 - 89
  • [46] SYNCHRONIZATION DURING MULTI-MODE THERMOACOUSTIC OSCILLATIONS IN A LIQUID-FUELED GAS TURBINE COMBUSTOR AT ELEVATED PRESSURE
    Passarelli, Mitchell L.
    Cirtwill, J. D. Maxim
    Wabel, Timothy
    Steinberg, Adam M.
    Wickersham, A. J.
    PROCEEDINGS OF THE ASME TURBO EXPO: TURBOMACHINERY TECHNICAL CONFERENCE AND EXPOSITION, 2019, VOL 4B, 2019,
  • [47] Flame Transfer Functions for Liquid-Fueled Swirl-Stabilized Turbulent Lean Direct Fuel Injection Combustion
    Yi, Tongxun
    Santavicca, Domenic A.
    JOURNAL OF ENGINEERING FOR GAS TURBINES AND POWER-TRANSACTIONS OF THE ASME, 2010, 132 (02):
  • [48] Flame transfer functions for liquid-fueled swirl-stabilized turbulent lean direct fuel injection combustion
    Yi, Tongxun
    Santavicca, Domenic A.
    Journal of Engineering for Gas Turbines and Power, 2010, 132 (02) : 1 - 6
  • [49] Comparison of the Flame Dynamics of a Liquid-Fueled Swirl-Stabilized Combustor for Different Degrees of Fuel-Air Premixing
    Kaufmann, Jan
    Vogel, Manuel
    Sattelmayer, Thomas
    JOURNAL OF ENGINEERING FOR GAS TURBINES AND POWER-TRANSACTIONS OF THE ASME, 2024, 146 (03):
  • [50] Experimental study on combustion stability characteristics in liquid-fueled gas turbine model combustor: Fuel sensitivities and flame/flow dynamics
    Ruan, Can
    Chen, Feier
    Yu, Tao
    Cai, Weiwei
    Mao, Yebing
    Qian, Yong
    Li, Xinling
    Lu, Xingcai
    FUEL, 2020, 265