Skip to main content
Log in

Effects of H2/CO/CH4 syngas composition variation on the NO x and CO emission characteristics in a partially-premixed gas turbine combustor

  • Article
  • Published:
Science China Technological Sciences Aims and scope Submit manuscript

Abstract

This paper reports the effects of variations in the fuel composition of H2/CO/CH4 syngas on the characteristics of NO x and CO emissions in a partially-premixed gas turbine combustor. Combustion tests were conducted on a full range of fuel compositions by varying each component gas from 0% to 100% at heat inputs of 40 and 50 kWth. Flame temperature, combustor liner temperature, ignition delay time, and flame structure were investigated computationally and experimentally to judge whether they are significant indicators of NO x and CO formation. The characteristics of and reasons for NO x and CO emissions were investigated by analyzing the emission mechanisms and relationships among fuel property, equivalence ratio, flame temperature, liner temperature, flame shape. The flame structures were investigated using the following flame visualization methods: (1) time-averaged OH* chemiluminescence and its Abel-deconvolution; (2) direct photography; and (3) instantaneous OH-PLIF. The flame structures were greatly changed by the fuel composition and heat input, and they were subjected to key affecting parameters of the temperatures of the flames and the liners. NO x and CO emissions also largely varied according to fuel composition and heat input, showing neither linearly nor exponentially clear proportional trends toward the syngas compositions because of the singular conditions. For example, only the 100% CO flame at low load emitted lots of CO, whereas complete combustion was observed in other cases. However, the qualitative observations showed that the root causes of NO x emission behaviors were flame temperature and flame structure, which were directly related to the residence time in the flame. Various sets of practical test results were obtained, and these results could contribute to the optimal selection of the fuel-feeding condition when fuel is changed from natural gas to syngas in order to minimize NO x and CO emissions with stable combustion.

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. Tian X J, Xing S X, Cui Y F, et al. CIVB flashback analysis of hydrogen flame based on azimuthal vorticity at mixing zone exit. Sci China Tech Sci, 2014, 57: 2466–2474

    Article  Google Scholar 

  2. Warnatz J, Maas U, Dibble R W. Combustion, Second ed. Germany: Springer, 1999. 219–231

    Book  MATH  Google Scholar 

  3. Walton S M, He X, Zigler B T, et al. An experimental investigation of the ignition properties of hydrogen and carbon monoxide mixtures for syngas turbine applications. Proc Combust Inst, 2007, 31: 3147–3154

    Article  Google Scholar 

  4. Natarajan J, Lieuwen T, Seitzman J. Laminar flame speeds of H2/CO mixtures: Effect of CO2 dilution, preheat temperature, and pressure. Comb and flame, 2007, 151: 104–119

    Article  Google Scholar 

  5. Lieuwen T, McDonell V, Petersen E, et al. Fuel flexibility influences on premixed combustor blowout, flashback, autoignition, and stability. J Eng Gas Turbine Power, 2008, 130: 011506

    Article  Google Scholar 

  6. Dodo S, Asai T, Koizumi H, et al. Performance of a multiple-injection dry low NOx combustor with hydrogen-rich syngas fuels. J Eng Gas Turbine Power, 2013, 135: 011501

    Article  Google Scholar 

  7. Littlejohn D, Cheng R K, Noble D R, et al. Laboratory investigations of low-swirl injectors operating with syngases. J Eng Gas Turbine Power, 2010, 132: 011502

    Article  Google Scholar 

  8. Hasegawa T, Tamaru T. Gas turbine combustion technology reducing both fuel-NOx and thermal NOx emissions for oxygen-blown IGCC with hot/dry synthetic gas cleanup. J Eng Gas Turbine Power, 2007, 129: 358–369

    Article  Google Scholar 

  9. Huang M, Shao W, Xiong Y, et al. Effect of fuel injection velocity on MILD combustion of syngas in axially-staged combustor. Appl Ther Eng, 2014, 66: 485–492

    Article  Google Scholar 

  10. Huang M, Zhang Z, Shao W, et al. Coal-derived syngas MILD combustion in parallel jet forward flow combustor. Appl Ther Eng, 2014, 71: 161–168

    Article  Google Scholar 

  11. Li P, Mi J, Dally B B, et al. Progress and recent trend in MILD combustion. Sci China Tech Sci, 2011, 54: 255–269

    Article  Google Scholar 

  12. Lee M C, Seo S B, Yoon J, et al. Experimental study on the effect of N2, CO2, and steam dilution on the combustion performance of H2 and CO synthetic gas in an industrial gas turbine. Fuel, 2012, 102: 431–438

    Article  Google Scholar 

  13. Davis D W, Therkelsen P L, Littlejohn D, et al. Effects of hydrogen on the thermo-acoustics coupling mechanisms of low-swirl injector flames in a model gas turbine combustor. Proc Combust Inst, 2013, 34: 3135–3143

    Article  Google Scholar 

  14. Allison P M, Driscoll J F, Ihme M. Acoustic characterization of a partially-premixed gas turbine model combustor: Syngas and hydrocarbon fuel comparisons. Proc Combust Inst, 2013, 34: 3145–3153

    Article  Google Scholar 

  15. Joo S, Yoon J, Kim J, et al. NOx emissions characteristics of the partially premixed combustion of H2/CO/CH4 syngas using artificial neural networks. Appl Ther Eng, 2015, 80: 436–444

    Article  Google Scholar 

  16. Williams T C, Shaddix C R. Contamination of carbon monoxide with metal carbonyls: Implications for combustion research. Combust Sci Tech, 2007, 179: 1225–1230

    Article  Google Scholar 

  17. Lee M C, Yoon J, Joo S, et al. Investigation into the cause of high multi-mode combustion instability of H2/CO/CH4 syngas in a partially premixed gas turbine model combustor. Proc Comb Inst, 2015, 35: 3263–3271

    Article  Google Scholar 

  18. Park J, Lee M C. Combustion instability characteristics of H2/CO/ CH4 syngases and synthetic natural gases in a partially-premixed gas turbine combustor: Part II–Time lag analysis. Int J of Hydrogen Energy, 2016,41: 1304–1312

    Article  Google Scholar 

  19. Turns S R. An Introduction to Combustion. Singapore: McGraw-Hill, 1999. 527–560

    Google Scholar 

  20. Petersen E L, Hall J M, Smith S D, et al. Ignition of lean methane- based fuel blends at gas turbine pressures. J Eng Gas Turbines Power, 2007, 129: 937–944

    Article  Google Scholar 

  21. Vries J, Petersen E L. Autoignition of methane-based fuel blends under gas turbine conditions. Proc Combust Inst, 2007, 31: 3163–3171

    Article  Google Scholar 

  22. La Violette M, Perez R. On the prediction of pollutant emission indices from gas turbine combustion chambers. In: Proceedings of American Society of Mechanical Engineers Turbo Expo. Copenhagen: American Society of Mechanical Engineers, 2012

    Google Scholar 

  23. La Violette M, Strawson M. On the prediction of nitrogen oxides from gas turbine combustion chambers using neural networks. In: Proceedings of A American Society of Mechanical Engineers Turbo Expo, Berlin: American Society of Mechanical Engineers, 2008

    Google Scholar 

Download references

Author information

Authors and Affiliations

Authors

Corresponding author

Correspondence to Min Chul Lee.

Rights and permissions

Reprints and permissions

About this article

Check for updates. Verify currency and authenticity via CrossMark

Cite this article

Lee, M.C. Effects of H2/CO/CH4 syngas composition variation on the NO x and CO emission characteristics in a partially-premixed gas turbine combustor. Sci. China Technol. Sci. 59, 1804–1813 (2016). https://doi.org/10.1007/s11431-016-0099-x

Download citation

  • Received:

  • Accepted:

  • Published:

  • Issue Date:

  • DOI: https://doi.org/10.1007/s11431-016-0099-x

Keywords

Navigation