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International Journal of Energetic Materials and Chemical Propulsion
ESCI SJR: 0.149 SNIP: 0.16 CiteScore™: 0.29

ISSN Imprimir: 2150-766X
ISSN On-line: 2150-7678

International Journal of Energetic Materials and Chemical Propulsion

DOI: 10.1615/IntJEnergeticMaterialsChemProp.v8.i6.20
pages 489-500

INTERACTION BETWEEN TWO CYLINDERS IN A PULSE DETONATION ENGINE

Toshiyuki Tsuji
Department of Mechanical Engineering, Saitama University, 255, Shimo-Okubo, Sakura-ku, Saitama, Saitama 338-8570 Japan
Shinichi Shirakawa
Department of Mechanical Engineering, Saitama University, 255, Shimo-Okubo, Sakura-ku, Saitama, Saitama 338-8570 Japan
Teruo Yoshihashi
Department of Mechanical Engineering, Saitama University, 255, Shimo-Okubo, Sakura-ku, Saitama, Saitama 338-8570 Japan
Tetsuro Obara
Department of Mechanical Engineering, Saitama University, 255, Shimo-Okubo, Sakura-ku, Saitama, Saitama 338-8570 Japan
Shigeharu Ohyagi
Department of Mechanical Engineering, Saitama University, 255, Shimo-Okubo, Sakura-ku, Saitama, Saitama 338-8570 Japan

RESUMO

This paper reports the results of an experimental study to determine the effects of interaction between two cylinders of a pulse detonation engine as well as to estimate the thermal efficiency of the system with a turbine. An interaction between the tubes occurs if a diffracted shock wave propagates into the other tube, which disturbs its filling process. The system is able to be operated in 40 Hz per tube, which means 80 Hz in total. The thermal efficiency of this system was estimated by measuring work done by a compressor, driven by the turbine. It is concluded that for designing a multi-cylinder system, it is important to consider the interference between the tubes and the nozzle.

Referências

  1. Roy, G.D., Frolov, S.M., Borisov, A.A., and Netzer, D.W., Pulse Detonation Propulsion: Challenges, Current Status, and Future Perspective.

  2. Sakurai,T., Yamane, N., Obara,T., and Ohyagi, S., A Study on Thermodynamic Cycle of Pulse Detonation Gas Turbine Engine.

  3. Sakurai, T., Obara, T., Ohyagi, S., and Murayama, M., Experimental Study of Pulse Detonation Turbine Engine toward Power Generator.

  4. Maeda, S., Kasahara, J., Tanaka, K., Matsuo, A., and Endo, T., Performance Test of a Pulse Detonation Turbine Engine Using a Small Turbine.

  5. Adam R., Anthony F., and Anthony J.D., Experimental Investigations of an Axial Turbine Driven by a Multi-Tube Pulsed Detonation Combustor System.

  6. Hamazoe, R., Hino, T., Muro, H., Takemoto, M., Yatsufusa, T., Endo, T., Taki, S., and Kanemitsu, T., Improvement of Operation Frequency of the Multi-Tube Pulse Detonation Engine.

  7. Fuhua, M., Jeong-Yeol, C., and Vigor, Y., Thrust Chamber Dynamics and Propulsive Performance of Multi-Tube Pulse Detonation Engine.

  8. Aaron, J.G., Nicholas, C., and Ephraim, G., Performance Measurements of a Pulse Detonation Combustor Array Integrated with an Axial Flow Turbine.


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