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Tytuł artykułu

Investigations of the ignition and combustion processes in the single compression engine

Treść / Zawartość
Identyfikatory
Warianty tytułu
Języki publikacji
EN
Abstrakty
EN
An aim of work was analysing of combustion and ignition processes in chambers with small volume at the use of different sorts of fuels, fuel liquid and air mixtures and fuel gas ones. For experiments, the machine of single compression the cubic capacity of 400 mm3 approx and average piston speeds 4 m/s was used. Investigated physical processes allowed better recognizing processes occurring in miniature- real engines. For the feeding of the machine of single compression, homogeneous mixtures of hydrogen with air, propane with air and mixtures methyl and ethyl alcohol in the stoichiometric relation with air were used. Adequately earlier prepared mixtures warranted the repeatability conditions of the experiment. Experiments effected with the machine of single compression showed small increases of pressure from combustion process. The occurrence this can be explained with significant heat conduction to walls during comparatively long compressing and combustion. In carried research with the machine of single compression with very large ratio surface combustion chamber to its volume, one obtained comparatively low value of the maximum compression pressure. The researches showed that on processes of compression, combustion and ignition, the greater influence had geometry of combustion chamber, average piston speed than sorts applied fuels.
Twórcy
autor
  • Institute of Aeronautics Al. Krakowska 110/114, 02 - 265 Warszawa, Poland tel. 48 22 846 00 11, fax. 48 22 846 44 32, hakra@ilot.edu.pl
Bibliografia
  • [1] Fernandez-Pello, C., Micro-PowerGeneration Using Combustion: Issues and Approaches,29th International Symposium on Combustion, July 2002.
  • [2] Dornheim, M. A., Several Micro Air Vehicles in Flight Test Programs, Aviation Week and Space Technology. 12.07.1999.
  • [3] Dornheim, M. A., Turbojet on a Chip to Run in 2000, Aviation Week and Space Technology.12.07.1999.
  • [4] Paul, R. N., Kapoor R., Kim, J.-H., Menon, S., Simultation of Reciprocating Micro-Engine with Two Opposed Combustion Chambers, XXVIII International Symposium on Combustion. University of Edinburgh, Scotland, July 30 - August 4, 2000. The Combustion Institute. 2000.
  • [5] Aichlamayr, H., Kittelson, D., Zachariah, M. R., Yan W., Bonne U., Investigations into a MEMS Based Free - Piston Microengine, XXVIII International Symposium on Combustion. University of Edinburg, Scotland, July 30 - August 4, 2000. The Combustion Institute, 2000.
  • [6] Maruta, K., Takeda, K., Sitski, L., Borer K., Ronney P. D., Wussow, S. and Deutschmann, O., Catalytic Combustion in Microchannel for MEMS Power Generation, Third Asia-Pacific Conference on Combustion, Seoul, Korea, June 24-27, 2001.
  • [7] Herron, T., Wang, H., Peterson, R. B., Performance of a reciprocating expander-compressor for a miniature heat-actuated heat pump, Proceedings of the 3rd International Energy Conversion Engineering Conference and Exhibit, 2005.
  • [8] Peirs, J., Reynaerts, D., Verplaetsen, F., Development of an axial microturbine for a portable gas turbine generator, Journal of Micromechanics and Microengineering, Vol. 13, pp. 190-195, 2003.
  • [9] Isomura, K., Murayama, M. Teramoto, S. Hikichi, K., Endo, Y., Experimental verification of the feasibility of a 100 W class micro-scale gas turbine at an impeller diameter of 10 mm,Journal of Micromechanics and Microengineering, 16:S254–S261, 2006.
  • [10] Green, D. V., Miller, C. G., Santavicca, D. A., Sharp, K. V., Pulsed micro catalytic combustor for use in a solid piston microengine, Proceedings of the ASME International Mechanical Engineering Congress and Exposition, IMECE2004-61644, 2004.
  • [11] Lee, D. H., Park, D. E., Yoon, J. B., Kwon, S., Yoon, E., Fabrication and Micromechanics, Test of a MEMS Combustor and Reciprocating Device, Journal of Microengineering and Micromechanics, Vol.12, pp. 26-34, 2002.
Typ dokumentu
Bibliografia
Identyfikator YADDA
bwmeta1.element.baztech-article-BUJ8-0004-0013
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