Based on the data of a physical experiment, the possibility of increasing the efficiency of combustion of fuel in power plants with the use of a multipoint plasma ignition of a fuel mixture in a cylindrical combustion chamber of such an installation by a subcritical streamer discharge initiated on the combustion chamber surface by a half-wave resonator is discussed. The dependences of the flame front propagation time and the rate of pressure increase in the combustion chamber on the initial pressure and composition of the fuel mixture characterized by the fuel excess coefficient, were studied Based on the results of measurements, the optimal fuel excess coefficient was determined, which provides the highest pressure and the highest rate of pressure increase in the combustion chamber during streamer ignition of fuel in it.
机构:
Univ So Calif, Pulsed Power Res Grp, Los Angeles, CA 90089 USAUniv So Calif, Pulsed Power Res Grp, Los Angeles, CA 90089 USA
Pendleton, S. J.
Bowman, S.
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Ohio State Univ, Michael A Chaszeyka Nonequilibrium Thermodynam La, Columbus, OH 43210 USAUniv So Calif, Pulsed Power Res Grp, Los Angeles, CA 90089 USA
Bowman, S.
Carter, C.
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USAF, Res Lab, Wright Patterson AFB, OH 45433 USAUniv So Calif, Pulsed Power Res Grp, Los Angeles, CA 90089 USA
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Univ So Calif, Pulsed Power Res Grp, Los Angeles, CA 90089 USAUniv So Calif, Pulsed Power Res Grp, Los Angeles, CA 90089 USA
Pendleton, S. J.
Montello, A.
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Ohio State Univ, Michael A Chaszeyka Nonequilibrium Thermodynam La, Columbus, OH 43210 USAUniv So Calif, Pulsed Power Res Grp, Los Angeles, CA 90089 USA
Montello, A.
Carter, C.
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USAF, Res Lab, Wright Patterson AFB, OH 45433 USAUniv So Calif, Pulsed Power Res Grp, Los Angeles, CA 90089 USA
Carter, C.
Lempert, W.
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Ohio State Univ, Michael A Chaszeyka Nonequilibrium Thermodynam La, Columbus, OH 43210 USAUniv So Calif, Pulsed Power Res Grp, Los Angeles, CA 90089 USA
Lempert, W.
Gundersen, M. A.
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Univ So Calif, Pulsed Power Res Grp, Los Angeles, CA 90089 USAUniv So Calif, Pulsed Power Res Grp, Los Angeles, CA 90089 USA
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Univ Tokyo, Dept Elect Engn & Informat Syst, 7-3-1 Hongo, Bunkyo City, Tokyo 1138654, JapanUniv Tokyo, Dept Elect Engn & Informat Syst, 7-3-1 Hongo, Bunkyo City, Tokyo 1138654, Japan
Wei, Zhenyu
Komuro, Atsushi
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Univ Tokyo, Dept Adv Energy, 5-1-5 Kashiwanoha, Kashiwa, Chiba 2278568, JapanUniv Tokyo, Dept Elect Engn & Informat Syst, 7-3-1 Hongo, Bunkyo City, Tokyo 1138654, Japan
Komuro, Atsushi
Ono, Ryo
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Univ Tokyo, Dept Adv Energy, 5-1-5 Kashiwanoha, Kashiwa, Chiba 2278568, JapanUniv Tokyo, Dept Elect Engn & Informat Syst, 7-3-1 Hongo, Bunkyo City, Tokyo 1138654, Japan
机构:
Air Force Engn Univ, Sci & Technol Plasma Dynam Lab, Xian 710038, Shaanxi, Peoples R China
Xi An Jiao Tong Univ, Sch Mech Engn, Inst Aeroengine, Xian 710049, Shaanxi, Peoples R ChinaAir Force Engn Univ, Sci & Technol Plasma Dynam Lab, Xian 710038, Shaanxi, Peoples R China
Lin, Bingxuan
Wu, Yun
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Air Force Engn Univ, Sci & Technol Plasma Dynam Lab, Xian 710038, Shaanxi, Peoples R China
Xi An Jiao Tong Univ, Sch Mech Engn, Inst Aeroengine, Xian 710049, Shaanxi, Peoples R ChinaAir Force Engn Univ, Sci & Technol Plasma Dynam Lab, Xian 710038, Shaanxi, Peoples R China
Wu, Yun
Zhang, Zhibo
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Air Force Engn Univ, Sci & Technol Plasma Dynam Lab, Xian 710038, Shaanxi, Peoples R ChinaAir Force Engn Univ, Sci & Technol Plasma Dynam Lab, Xian 710038, Shaanxi, Peoples R China
Zhang, Zhibo
Bian, Dongliang
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Air Force Engn Univ, Sci & Technol Plasma Dynam Lab, Xian 710038, Shaanxi, Peoples R ChinaAir Force Engn Univ, Sci & Technol Plasma Dynam Lab, Xian 710038, Shaanxi, Peoples R China
Bian, Dongliang
Jin, Di
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Air Force Engn Univ, Sci & Technol Plasma Dynam Lab, Xian 710038, Shaanxi, Peoples R China
Tsinghua Univ, Dept Energy & Power Engn, Minist Educ, Key Lab Thermal Sci & Power Engn, Beijing 100084, Peoples R ChinaAir Force Engn Univ, Sci & Technol Plasma Dynam Lab, Xian 710038, Shaanxi, Peoples R China