TY - GEN
T1 - Weakly-pulsated center combustion engine
T2 - AIAA Propulsion and Energy Forum and Exposition, 2019
AU - Kobayashi, Tomotaka
AU - Mikoda, Junya
AU - Kinoshita, Kodai
AU - Makimoto, Hiroki
AU - Kobayashi, Yoshiki
AU - Lujiang, Shi
AU - Konagaya, Remi
AU - Naitoh, Ken
N1 - Funding Information:
This paper is part of the outcome of research performed under the JSPS grant for research projects (25630072). Sincere thanks are also due the members of the Naitoh Laboratory for their help.
Publisher Copyright:
© 2019 by American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.
PY - 2019
Y1 - 2019
N2 - In order to achieve very high thermal efficiency, we developed a prototype engine for aerospace based on a new combustion principle due to colliding pulsed supermulti-jets. The prototype engine has ignition assisting system called “torch system” to stabilize startup. The previous torch system has a problem that ignition is unstable. In the present report, ignitability of torch system is improved by changing gas for combustion in torch from air to oxygen. Emphasis is placed on the fact that air-insulation effect on the side-wall in the new strong torch system occurred. This will occur, because weakly-pulsed pressure wave generated around the torch center hits the side wall, which reflects and pushes back the burned gas toward the chamber center. The result of the experiment indicates a possibility of air-insulation based on weakly-pulsated combustion at around center of combustion chamber “without the supermulti-jets colliding”. The new engine concept may improve thermal efficiency of conventional engines such as those of jet engines and piston engines, although the engine concept based on the supermulti-jets colliding with strong pulse proposed previously by us will bring higher thermal efficiency because of addition of silent high compression.
AB - In order to achieve very high thermal efficiency, we developed a prototype engine for aerospace based on a new combustion principle due to colliding pulsed supermulti-jets. The prototype engine has ignition assisting system called “torch system” to stabilize startup. The previous torch system has a problem that ignition is unstable. In the present report, ignitability of torch system is improved by changing gas for combustion in torch from air to oxygen. Emphasis is placed on the fact that air-insulation effect on the side-wall in the new strong torch system occurred. This will occur, because weakly-pulsed pressure wave generated around the torch center hits the side wall, which reflects and pushes back the burned gas toward the chamber center. The result of the experiment indicates a possibility of air-insulation based on weakly-pulsated combustion at around center of combustion chamber “without the supermulti-jets colliding”. The new engine concept may improve thermal efficiency of conventional engines such as those of jet engines and piston engines, although the engine concept based on the supermulti-jets colliding with strong pulse proposed previously by us will bring higher thermal efficiency because of addition of silent high compression.
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U2 - 10.2514/6.2019-4394
DO - 10.2514/6.2019-4394
M3 - Conference contribution
AN - SCOPUS:85095969813
SN - 9781624105906
T3 - AIAA Propulsion and Energy Forum and Exposition, 2019
BT - AIAA Propulsion and Energy Forum and Exposition, 2019
PB - American Institute of Aeronautics and Astronautics Inc, AIAA
Y2 - 19 August 2019 through 22 August 2019
ER -