Skip to main content
Log in

In-situ measurement of reflection coefficient and its application to predicting combustion instability in a gas turbine combustor

  • Original Article
  • Published:
Journal of Mechanical Science and Technology Aims and scope Submit manuscript

Abstract

Here, a procedure that uses in-situ data recorded by two microphones placed inside an operating gas turbine combustor to determine the reflection coefficient is proposed. The procedure is validated against previously reported results and further employed to determine the coefficients of feeding lines supplying a partially premixed gas turbine combustor. With the help of lumped network code, a prediction analysis of combustion instability in a combustor is also conducted using the measured reflection coefficients, R(ω), which are a function of frequency. The prediction results are compared with those from other acoustic boundaries, including both analytical models and a measured single-valued approach. The predictions, based on R(ω), are shown to be more accurate than those from any other boundary methods considered. A comparison of the predicted combustion instability frequencies from this study with corresponding experimental results shows that the developed procedure for determining the coefficient is reliable and has great potential.

This is a preview of subscription content, log in via an institution to check access.

Access this article

Price excludes VAT (USA)
Tax calculation will be finalised during checkout.

Instant access to the full article PDF.

Similar content being viewed by others

References

  1. UNFCCC, The Paris Agreement, UN Framework Convention on Climate Change, United Nations (2015).

    Google Scholar 

  2. I. Gokalp and E. Lebas, Alternative fuels for industrial gas turbines, Appl. Therm. Eng., 24 (2004) 1655–1663.

    Article  Google Scholar 

  3. T. Lieuwen, V. McDonell, E. Petersen and D. Santavicca, Fuel flexibility influences on premixed combustor blowout, flashback, autoignition, tand stability, J. Eng. Gas Turbines Power, 130 (2008) 011506.

    Article  Google Scholar 

  4. S. Taamallah, K. Vogiatzaki, F. M. Alzahrani, E. M. A. Mokheimer, M. A. Habib and A. F. Ghoniem, Fuel flexibility, stability and emissions in premixed hydrogen-rich gas turbine combustion: technology, fundamentals, and numerical simulations, Appl. Energy, 154 (2015) 1020–1047.

    Article  Google Scholar 

  5. P. Chiesa, G. Lozza and L. Mazzocchi, Using hydrogen as gas turbine fuel, J. Eng. Gas Turbines Power, 127 (2005) 73–80.

    Article  Google Scholar 

  6. B. Ge, Y. Ji, Z. Zhang, S. Zang, Y. Tian, H. Yu, M. Chen, G. Jiao and D. Zhang, Experiment study on the combustion performance of hydrogen-enriched natural gas in a DLE burner, Int. J. Hydrogen Energy, 44 (2019) 14023–14031.

    Article  Google Scholar 

  7. J. Goldmeer, Power to Gas: Hydrogen for Power Generation, GEA33861, GE Power, Schenectady, NY (2019).

    Google Scholar 

  8. S. Patel, Siemens’ roadmap to 100 % hydrogen gas turbines, POWER Magazine, Access Intelligence, LLC., Rockville, MD (2020).

    Google Scholar 

  9. S. Patel, MHPS secures first order for hydrogen-capable J series gas turbines, POWER Magazine, Access Intelligence, LLC., Rockville, MD (2020).

    Google Scholar 

  10. T. C. Lieuwen and V. Yang, Combustion Instabilities in Gas Turbine Engines: Operational Experience, Fundamental Mechanisms and Modelling, American Institute of Aeronautics and Astronautics, Inc., Reston, VA (2005).

    Google Scholar 

  11. K. T. Kim, J. G. Lee, B. D. Quay and D. A. Santavicca, Spatially distributed flame transfer functions for predicting combustion dynamics in lean premixed gas turbine combustor, Combust. Flame, 157 (2010) 1718–1730.

    Article  Google Scholar 

  12. K. T. Kim, J. G. Lee, B. D. Quay and D. A. Santavicca, Response of partially premixed flames to acoustic velocity and equivalence ratio perturbations, Combust. Flame, 157 (2010) 1731–1744.

    Article  Google Scholar 

  13. J. Yoon, S. Joo, J. Kim, M. C. Lee, J. G. Lee and Y. Yoon, Effects of convection time on the high harmonic combustion instability in a partially premixed combustor, Proc. Combust. Inst., 36 (2017) 3753–3761.

    Article  Google Scholar 

  14. D. W. Davis, P. L. Therkelsen, D. Littlejohn and R. K. Cheng, Effects of hydrogen on the thermo-acoustics coupling mechanisms of low-swirl injector flames in a model gas turbine combustor, Proc. Combust. Inst., 34 (2013) 3135–3143.

    Article  Google Scholar 

  15. S. J. Shanbhogue, Y. S. Sanusi, S. Taamallah, M. A. Habib, E. M. A. Mokheimer and A. F. Ghoniem, Flame macrostructures, combustion instability and extinction strain scaling in swirl stabilized premixed CH4/H2 combustion, Combust. Flame, 163 (2016) 494–507.

    Article  Google Scholar 

  16. M. E. Harvazinski, W. E. Anderson and C. L. Merkle, Combustion instability diagnostics using the Rayleigh index, 47thAIAA/ASME/SAE/AASEE Joint Propulsion Conf. and Exhibit (2011) 1–20.

  17. N. N. Deshmukh and S. D. Sharma, Coefficient of Rayleigh index based performance evaluation of radial micro jet injection technique for thermo-acoustic instability control, Measurement, 151 (2020) 07245.

    Article  Google Scholar 

  18. F. Marble and S. Candle, Acoustic disturbances from gas non-uniformities convected through a nozzle, J. Sound Vib., 55 (1977) 225–243.

    Article  Google Scholar 

  19. W. Polifke, Reconstruction of acoustic transfer matrices by instationary computational fluid dynamics, J. Sound Vib., 245(3) (2001) 483–510.

    Article  Google Scholar 

  20. N. N. Deshmukh and S. D. Sharma, Experiments on heat content inside a Rijke tube with suppression of thermo-acoustics instability, Int’l J. Spray Combust. Dynamics, 9(2) (2017) 85–101.

    Article  Google Scholar 

  21. J. Keller, Thermoacoustic oscillations in combustion chambers of gas turbines, AIAA J., 33(12) (1995) 2280–2287.

    Article  Google Scholar 

  22. S. Roux, G. Lartigue, T. Poinsot and T. Berat, Studies of mean and unsteady flow in a swirled combustor using experiments, acoustic analysis and large eddy simulations, Combust. Flame, 141(1–2) (2005) 40–54.

    Article  Google Scholar 

  23. C. E. Martin, L. Benoit, Y. Sommerer, F. Nicoud and T. Poinsot, Large-eddy simulation and acoustic analysis of a swirled staged turbulent combustor, AIAA J., 44(4) (2006) 741–750.

    Article  Google Scholar 

  24. K. I. Matveev and F. E. C. Culick, Limit-cycle properties of a Rijke tube, Eiectronic J. Tech. Acoustics, (2003) 1–13.

  25. F. Richecoeur, T. Schuller, A. Lamraoui and S. Ducruix, Analytical and experimental investigations of gas turbine model combustor acoustics operated at atmospheric pressure, Comptes Rendus Mecanique, 341 (2013) 141–151.

    Article  Google Scholar 

  26. W. J. Song and D. J. Cha, Determination of an acoustic reflection coefficient at the Inlet of a model gas turbine combustor for power generation, J. Korean Soc. Combust., 23(2) (2018) 7–13.

    Article  Google Scholar 

  27. ISO 10534-2:1998, Acoustics — Determination of Sound Absorption Coefficient and Impedance in Impedance Tubes — Part 2: Transfer-Function Method, International Organization for Standardization, Geneva, Switzerland (1998).

    Google Scholar 

  28. A. Lamraoui, F. Richecoeur, T. Schuller and S. Ducruix, A methodology for on the fly acoustic characterization of the feeding line impedances in a turbulent swirled combustor, J. Eng. Gas Turbines Power, 133(1) (2011) 011504.

    Article  Google Scholar 

  29. J. Li, D. Yang, C. Luzzato and A. S. Morgans, Open Source Combustion Instability Low Order Simulator (OSCILOS-Long), Technical Report, Department of Mechanical Engineering, Imperial College London, London, UK (2014).

    Google Scholar 

  30. D. J. Cha, J. K. Song and J. G. Lee, A case study on combustion instability of a model lean premixed gas turbine combustor with open source code OSCILOS, J. Korean Soc. Combust., 20(4) (2015) 10–18.

    Article  Google Scholar 

  31. K. T. Kim, H. J. Lee, J. G. Lee, B. D. Quay and D. A. Santavicca, Flame transfer function measurement and instability frequency prediction using a thermoacoustic model, Proceedings of ASME Turbo Expo (2009) ASME Paper GT2009-60026.

  32. T. Poinsot and D. Veynante, Theoretical and Numerical Combustion, R. T. Edwards, Inc., Philadelphia, PA (2005).

    Google Scholar 

  33. MATLAB, https://kr.mathworks.com/products/matlab.html, The MathWorks, Inc., Seoul (2021).

Download references

Acknowledgments

This work was supported by the International Collaborative Research Program of Hanbat National University, which was granted financial resources from the Ministry of Education, Republic of Korea, in 2020. The authors are grateful to Prof. Jonggeun Lee at the University of Cincinnati and Prof. Youngbin Yoon at Seoul National University for providing their invaluable experimental data.

Author information

Authors and Affiliations

Authors

Corresponding author

Correspondence to Dong Jin Cha.

Additional information

Won Joon Song is an Assistant Professor in the Department of Mechanical Systems Engineering for Energy Convergence at Dongshin University in Naju, Korea. He received his Ph.D. in Mechanical Engineering from the University of Cincinnati, OH, USA. His research interests include auditory system modeling, signal processing for artificial cochlea, hearing loss assessment, online monitoring of combustion stability, and image processing of combustion flames.

Gyu Seong Youn is a Graduate Student in the Department of Building Services Engineering at Hanbat National University in Daejeon, Korea. His research interests include combustion instability in gas turbines for power generation and building energy management.

Dong Jin Cha is a Professor in the Department of Building and Plant Engineering at Hanbat National University in Daejeon, Korea. He received his Ph.D. in Mechanical Engineering from the University of Illinois at Chicago, IL, USA. His research interests include combustion instability in gas turbines for power generation, fluid flows in building and plant engineering.

Rights and permissions

Reprints and permissions

About this article

Check for updates. Verify currency and authenticity via CrossMark

Cite this article

Song, W.J., Youn, G.S. & Cha, D.J. In-situ measurement of reflection coefficient and its application to predicting combustion instability in a gas turbine combustor. J Mech Sci Technol 35, 4261–4270 (2021). https://doi.org/10.1007/s12206-021-0836-1

Download citation

  • Received:

  • Revised:

  • Accepted:

  • Published:

  • Issue Date:

  • DOI: https://doi.org/10.1007/s12206-021-0836-1

Keywords

Navigation