한국항공우주학회지 (Journal of the Korean Society for Aeronautical & Space Sciences)

  • 제42권10호
  • /
  • Pages.858-869
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  • 2014
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  • 1225-1348(pISSN)
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  • 2287-6871(eISSN)
한국항공우주학회 (The Korean Society for Aeronautical and Space Sciences)
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PDE 기반 PGC 추진기관 시스템 연구 동향

Research Activities on PGC Propulsion Systems based on PDE

  • Kim, Ji-Hoon (Department of Aerospace Engineering, Pusan National University) ;
  • Kim, Tae-Young (Department of Aerospace Engineering, Pusan National University) ;
  • Jin, Wan-Sung (Department of Aerospace Engineering, Pusan National University) ;
  • Choi, Jeong-Yeol (Department of Aerospace Engineering, Pusan National University)
  • 투고 : 2014.06.23
  • 심사 : 2014.08.22
  • 발행 : 2014.10.01
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⟨ 이전 논문 다음 논문 ⟩

초록

대부분의 항공우주 추진은 정압 Brayton 사이클에 기초하고 있으나 성능 향상을 위한 압력비 증가는 기계적 한계에 직면하고 있다. 지난 십여 년간 고속 추진에 적합한 연소방식으로 기대 받은 데토네이션 추진이, 최근에는 추진기관과 동력 장치의 열효율을 획기적으로 증대시켜 줄 수 있는 "game-changer"로 연구되고 있다. 즉, 데토네이션 파에 수반하는 강한 충격파의 압축 효과는 기존의 압축 방식에서 얻기 힘든 열효율을 증가시키는 것으로 여겨진다. 본 논문에서는 펄스데토네이션엔진의 최신 기술 동향과 더불어 정적연소에 기초한 압력증가연소 체계의 연구 동향에 대하여 소개할 것이다.

Most of the aerospace propulsion is based on the Brayton cycle, in which the combustion is held through the constant pressure process, but further improvement of performance by increasing compression ratio is challenged by mechanical limits. Detonation propulsions, regarded promising for high-speed propulsion for a lase decade, is more rigorously studied in these days as a game-changer for the improvement of thermodynamic efficiency of propulsion and power generation systems. Since, the additional compression by the strong shock of the detonation wave is considered increasing thermodynamics efficiency that is hardly achievable by the conventional compression systems. Present paper will give an introduction the latest technical trends on the Pulse Detonation Engines(PDEs) and the activities on the Pressure Gain Combustion (PGC) based on Constant Volume Combustion (CVC).

키워드

참고문헌

  1. Turns, S.R., An Introduction to Combustion: Concepts and Applications, 3rd Edition, New York, McGraw-Hill, 2011.
  2. Heiser, W.H., and Pratt, D.T., "Thermo dynamic Cycle Analysis of Pulse Detonation Engines," Journal of Propulsion and Power, Vol.18, No.1, pp.68-76 2002. https://doi.org/10.2514/2.5899
  3. Wu, Y., Ma, F., Yang, V., "System Performance and Thermodynamic Cycle Analysis of Airbreathing Pulse Detonation Engines," Journal of Propulsion and Power, Vol. 19, No. 4, 2003, pp.556-567. https://doi.org/10.2514/2.6166
  4. Zel'Dovich, Ya. B., "On the Theory of Detonation Propagation in Gaseous Systems," Sov. J. Exp. Theor. Phys., Vol. 10, 1940, pp.542-568.
  5. Hoffmann, N., "Reaction Propulsion by Intermittent Detonative Combustion", German Ministry of Supply, AI152365 Volkenrode Translation, 1940.
  6. Nicholls, J. A., Wilkinson, H. R. and Morrison R. B., "Intermittent Detonation as a Thrust-Producing Mechanism," Journal of Jet Propulsion, Vol. 27, No. 5, 1957, pp.534-541. https://doi.org/10.2514/8.12851
  7. Eidelman S., Grossmann W., and Lottati, I., "A review of Propulsion Applications of the Pulsed Detonation Engine Concept," AIAA 89-2446, 25th Joint Propulsion Conference, Jul. 1989.
  8. Bussing, T. R. A., Bratkovich, T. E., and Hinkey Jr., J. B., "Practical Implementation of Pulse Detonations Engines," 33rd Joint Propulsion Conference and Exhibit, Jul. 1997.
  9. Kailasanath, K., "Applications of Detonations to Propulsion : A Review," AIAA 99-1067, 37th AIAA Aerospace Sciences Meeting and Exhibit, Jan. 1999.
  10. Kailasanath, K., "Review of Propulsion Applications of Detonation Waves," AIAA Journal, Vol. 38, No. 9, Sep. 2000, pp. 1698-1708. https://doi.org/10.2514/2.1156
  11. Kailasanath, K., "Recent Developments in the Research on Pulse Detonation Engines," AIAA Journal, Vol. 41, No. 2, Feb. 2003, pp. 145-159. https://doi.org/10.2514/2.1933
  12. Roy, G. D., Frolov, S. M., Borisov, A. A., Netzer, D. W., "Pulse Detonation Propulsion : Challenges, Current Status, and Future Perspective," Progress in Energy and Combustion Science, Vol. 30, May. 2004, pp. 545-672. https://doi.org/10.1016/j.pecs.2004.05.001
  13. Wolanski, P., "Detonative Propulsion," Proceedings of the Combustion Institute, Vol. 34, Nov. 2012, pp. 125-158.
  14. First Holzwarth Experimental Gas Turbine, 1908, Deutsches Museum. http://www.deutsches-museum.de/en/collect ions/machines/power-engines/gas-turbines/holz warth-gas-turbine-1908/
  15. Gunston, B., "Napier Nomad: An engine of outstanding efficiency," Flight, April 1954, pp.543-551, Retrieved 18 December 2009.
  16. Barr, L., "Pulse Detonation Engine Flies into History," Press Release, Air Force Material Command, May, 2008.
  17. Hinkey, J., Williams, J., Henderson, S., Bussing, T., "Rotary-Valved, Multiple-Cycle, Pulse Detonation Engine Experimental Demonstration," AIAA 1997-2746, 33rd Joint Propulsion Conference and Exhibit, 1997.
  18. Dean, A. J., "A Review of PDE Development for Propulsion Application," AIAA 2007-985, 45th AIAA Aerospace Sciences Meeting and Exhibit, Jan. 2007.
  19. Zhang, G.T., Jiang, Y.T., Foo, H.S., Yip, M.S., Falempin, F., and Daniau, E., "First steps for the development and testing of a pulse detonation engine for UAV application," AIAA 2008-2681, May 2008.
  20. Kojima, T., Tsuboi, N., Taguchi, H., Kobayashi, H., Sato, T., Daimon, Y., and Inaba, K., "Design Study of Turbine for Pulse Detonation Combustor," AIAA 2007-5081, 43rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, Jul. 2007.
  21. Kojima, T. and Kobayashi, H., "Analytical and Experimental Study on PDE with Exit Valves for Hypersonic Propulsion System," AIAA 2005-3510, 41st AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, Jul. 2005.
  22. Kasahara, J., Hasegawa, A., Nemoto, T., Yamaguchi, H., Yajima, T., and Kojima, T., "Thrust Demonstration of a Pulse Detonation Rocket "Todoroki", AIAA Paper 2007-5007, July 2007.
  23. Bussing. T., "Vulcan Overview," VULCAN Industry Day Agenda, Jun. 10, 2008
  24. Schauer, F., and Mabbett, A., "Vulcan Engine Demonstration to Turbine-Drive Experiments," 2011 International Workshop on Detonation for Propulsion (IWDP2011), Nov. 2011.
  25. Dean, A. J., Rasheed, A., Tangirala, V., and Pinard, P. F., "Operation and Noise Transmission of an Axial Turbine Driven by a Pulse Detonation Combustor," Proccedings of the ASME Turbo Expo 2005, Jun. 2005.
  26. Endo, T., Susa, A., Kanekiyo, K., Hanta, Y., Mitsunobu, A., Takahashi, T., "Development of Pulse Detonation Technology in Valveless Mode and its Application to Turbine-Drive Experiments," 2011 International Workshop on Detonation for Propulsion (IWDP2011), Nov. 2011.
  27. Sakurai, T., Uiasa, S., "Development of Pulse Detonation Combustor for 1kW-Class Micro Gas Turbine," 2011 International Workshop on Detonation for Propulsion (IWDP2011), Nov. 2011.
  28. Glaser, A.J., Caldwell, N., Gutmark, E., "Performance of an Axial Flow Turbine Driven by Multiple Pulse Detonation Combustors," AIAA 2007-1244, 45th AIAA Aerospace Sciencces Meeting and Exhibit, Jan. 2007.
  29. Kasahara, J., Hasegawa, A., Nemoto, T. and Yamaguchi, H., "Thrust Demonstration of a Pulse Detonation Rocket "Todoroki"," 43rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, Jul. 2007.
  30. Matsuoka, K., Takagi, S., Kasahara, J., Morozumi, T., Kashiwazaki, T., Fujiwara, Y., Matsuo, A., and Funaki, I., "Study on a Rotary-Valved Four-Cylinder Pulse Detonation Rocket : Six Degree-of-Freedom Flight Measurement," AIAA 2014-1319, 52nd Aerospace Sciences Meeting, Jan. 2014.
  31. Matsuoka, K., Esumi, M., Ikeguchi, K. B., Kasahara, J., Matsuo, A., and Funaki, I., "Optical and Thrust Measurement of a Pulse Detonation Combustor with a Coaxial Rotary Valve," Combustion and Flame, Vol. 159, 2012, pp.1321-132. https://doi.org/10.1016/j.combustflame.2011.10.001
  32. Morozumi, T., Sakamoto, R., Kashiwazaki, T., Matsuoka, K., Takagi, S., Kasahara, J., Matsuo, A., and Funaki, I., "Study on a Rotar-Valved Four-Cylinder Pulse Detonation Rocket : Thrust Measurement by Ground Test," AIAA 2014-1317, 52nd Aerospace Sciences Meeting, Jan. 2014.
  33. Kasahara, J., Matsuoka, K., "Experimental Study on a Four-Cylinder Pulse Detonation Rocket Engine Flight Test Model," 2013 International Workshop on Detonation for Propulsion (IWDP2013), Jul. 2013
  34. Wu, M.H., Burke, M.P., Son, S.F. and Yetter, R.A., "Flame acceleration and the transition to detonation of stoichiometric ethylene/oxygen in microscale tubes," Proceedings of the Combustion Institute, Vol. 31, 2007, pp. 2429-2436.
  35. Gao, Y., Lee, J.H.S., and Ng, H. Dick. "Velocity fluctuation near the detonation limits," Combustion and Flame , 2014, in press. http://dx.doi.org/10.1016/j.combustflame.2014.04.020
  36. Wu, M.-H., "Progress in the Development of Pulsed Detonation Microthrusters," 2013 International Workshop on Detonation for Propulsion (IWDP2013), Jul. 2013.
  37. Wu, M.-H., and Lu, T.-H. "Development of a chemical microthruster based on pulsed detonation." Journal of Micromechanics and Microengineering Vol.22 (2012) 105040. https://doi.org/10.1088/0960-1317/22/10/105040
  38. Brophy, C. M., Werner, LT S., and Sinibaldi, J. O., "Performance Charcterization of a Valveless Pulse Detonation Engine," AIAA 2003-1344, 41st Aerospace Sciences Meeting and Exhibit, Jan. 2003.
  39. Wang, Z., Yan, C., Fan, W., Zheng, L., and Qiu, H., "Experimental Study of Kerosene/air Valveless Air-Breathing Pulse Detonation Engines," AIAA 2009-1066, 47th AIAA Aerospace Sciences Meeting Including The New Horizons Forum and Aerospace Exposition, Jan. 2009.
  40. Endo, T., "Thermal Spary by Pulsed Detonations," 2013 International Workshop on Detonation for Propulsion (IWDP2013), Jul. 2013.

피인용 문헌

  1. An Experimental Study on Characteristics of Small-scale PDE under Low-frequency Operating Conditions vol.22, pp.3, 2018, https://doi.org/10.6108/KSPE.2018.22.3.081