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Effects of Pressure Variation on the Combustion Characteristics of a Gaseous CH4/O2 Bipropellant in a Model Combustor

모델연소실 내 압력 변화가 메탄/산소 이원추진제의 연소특성에 미치는 영향

  • Choi, Sun (School of Mechanical Engineering, Sungkyunkwan University) ;
  • Kim, Tae Young (School of Mechanical Engineering, Sungkyunkwan University) ;
  • Kim, Hee Kyung (School of Mechanical Engineering, Sungkyunkwan University) ;
  • Koo, Jaye (School of Mechanical and Aerospace Engineering, Korea Aerospace University) ;
  • Kwon, Oh Chae (School of Mechanical Engineering, Sungkyunkwan University)
  • Received : 2016.07.06
  • Accepted : 2016.11.21
  • Published : 2017.02.01

Abstract

Liquid methane ($CH_4$)/oxygen ($O_2$) bipropellants have been recently considered as a next-generation propellant due to eco-friendly and non-toxic properties, low cost and high performance. In this study, the combustion characteristics of gaseous $CH_4/O_2$ nonpremixed coflow flames in a model combustor with variation of internal pressure are investigated through measuring the combustion stability limits and visualizing flames. Results show that the combustion stability limits are extended and the reaction region is widened with increasing internal pressure of the combustion chamber for fuel-rich condition.

메탄($CH_4$)/산소($O_2$) 액체이원추진제는 친환경성, 무독성, 경제성, 우수한 성능 등의 장점으로 최근 들어 차세대 친환경 이원추진제로서 관심을 받고 있다. 본 연구에서는 연소실 내 압력 변화에 따른 기체 메탄/산소 비예혼합 동축 화염의 연소안정한계를 측정하고, 화염 및 유동의 가시화를 통해 분사 조건 및 압력 변화에 따른 화염의 구조와 특성을 파악하였다. 연구 결과 연료과농 조건에서 연소실 내 압력이 증가할 경우 연소안정한계가 확장되고 반응 영역이 증가하는 것을 확인할 수 있었다.

Keywords

References

  1. Lee, T.H. and Lee, C.H., "Review of the Liquid Propulsion Technology," Journal of the Korean Society of Propulsion Engineers, Vol. 17, No. 5, pp. 132-139, 2013. https://doi.org/10.6108/KSPE.2013.17.5.132
  2. Sackheim, R.L. and Masse, R.K., "Green Propulsion Advancement: Challenging the Maturity of Monopropellant Hydrazine," 49th Joint Propulsion Conference, San Jose, C.A., U.S.A., AIAA 2013-3988, Jul. 2013.
  3. Kim, J.S., Jung, H. and Kim, J.H., "State of the Art in the Development of Methane/Oxygen Liquid-bipropellant Rocket Engine," Journal of the Korean Society of Propulsion Engineers, Vol. 17, No. 6, pp. 120-130, 2013. https://doi.org/10.6108/KSPE.2013.17.6.120
  4. Burkhardt, H., Sippel, M., Klevanski, J. and Herbertz, A., "Comparative Study of Kerosene and Methane Propellants for Reusable Liquid Booster Stages," 38th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Indianapolis, I.N., U.S.A., AIAA 2002-5235, Jul. 2002.
  5. Haeseler, D., Mading, C., Gotz, A., Roubinski, V., Khrissanfov, S. and Berejnoy, V., "Recent Developments for Future Launch Vehicle LOx/HC Rocket Engines," 6th International Symposium on Propulsion for Space Transportation of the 21st Century, Versailles, France, AAAF-02-100, May. 2002.
  6. Excoffon, T. and Borromee, J., "Future European Reusable Propulsion Systems," Proceedings of the International Symposium on Space Technology and Science, Vol. 23, No. 2, pp. 2558-2563, 2002.
  7. Singla, G., Scouflaire, P., Rolon, J.C. and Candel, S., "Flame Stabilization in High Pressure LOx/$GH_2$ and $GCH_4$ Combustion," Proceedings of the Combustion Institute, Vol. 31, No. 2, pp. 2215-2222, 2007. https://doi.org/10.1016/j.proci.2006.07.094
  8. Singla, G., Scouflaire, P., Rolon, J.C. and Candel, S., "Transcritical Oxygen/Transcritical or Supercritical Methane Combustion," Proceedings of the Combustion Institute, Vol. 30, No. 2, pp. 2921-2928, 2005. https://doi.org/10.1016/j.proci.2004.08.063
  9. Salgues, D., Mouis, A.-G., Lee, S.-Y., Kalitan, D., Pal, S. and Santoro, R., "Shear and Swirl Coaxial Injector Studies of LOX/GCH4 Rocket Combustion Using Non-instrusive Laser Diagnostics," 44th AIAA Aerospace Sciences Meeting and Exhibit, Reno, N.V., U.S.A., AIAA 2006-757, 2006.
  10. Choi, S., Kim, T.Y., Kim, H.K., Koo, J., Kim, J.S. and Kwon, O.C., "Properties of Inverse Nonpremixed Pure $O_2$/$CH_4$ Coflow Flames in a Model Combustor," Energy, Vol. 93, No. 1 pp. 1105-1115, 2015. https://doi.org/10.1016/j.energy.2015.09.110
  11. Moore, J.D. and Kuo, K.K., "Effect of Switching Methane/Oxygen Reactants in a Coaxial Injector on the Stability of Non-premixed Flames," Combustion Science and Technology, Vol. 180, No. 3, pp. 401-417, 2008. https://doi.org/10.1080/00102200701780887
  12. Maruta, K., Abe, K., Hasegawa, S., Maruyama, S. and Sato, J., "Extinction Characteristics of $CH_4$/$CO_2$ Versus $O_2$/$CO_2$ Counterflow Non-premixed Flames at Elevated Pressures up to 0.7 MPa," Proceedings of the Combustion Institute, Vol. 31, No. 1, pp. 1223-1230, 2007. https://doi.org/10.1016/j.proci.2006.08.013
  13. Liu, F. and Gulder, O, "Effects of Pressure and Preheat on Super-adiabatic Flame Temperatures in Rich Premixed Methane/Air Flames," Combustion Science and Technology, Vol. 180, No. 3, pp. 437-452, 2008. https://doi.org/10.1080/00102200701741285
  14. Chen, Z., Qin, X., Xu, B., Ju, Y. and Liu, F., "Studies of Radiation Absorption on Flame Speed and Flammability Limit of $CO_2$ Diluted Methane Flames at Elevated Pressures," Proceedings of the Combustion Institute, Vol. 31, No. 2, pp. 2693-2700, 2007. https://doi.org/10.1016/j.proci.2006.07.202
  15. Kim, T.Y., Choi, S., Kim, H.K., Jeung, I.S., Koo, J. and Kwon, O.C., "Combustion Properties of gaseous $CH_4$/$O_2$ Coaxial Jet Flames in a Single-element Combustor," Fuel, Vol. 184, pp. 28-35, 2016. https://doi.org/10.1016/j.fuel.2016.07.001
  16. Yuan, Z.G., "The Filtered Abel Transform and Its Application in Combustion Diagnostics," 1995 Fall Meeting, Western State Section of the Combustion Institute, Stanford, C.A., U.S.A., NASA/CR-2003-212121, 2003.