Volume 24 Issue 1
Jan.  2009
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LI Ming, WU Er-ping, SUO Jian-qin. Design and study of combustor for micro-turbojet engine[J]. Journal of Aerospace Power, 2009, 24(1): 70-74.
Citation: LI Ming, WU Er-ping, SUO Jian-qin. Design and study of combustor for micro-turbojet engine[J]. Journal of Aerospace Power, 2009, 24(1): 70-74.
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Design and study of combustor for micro-turbojet engine

  • School of Power and Energy, Northwestern Polytechnical University, Xi'an 710072, China

  • Received Date: 2008-07-24
  • Rev Recd Date: 2008-11-28
  • Publish Date: 2009-01-28
    Abstract
  • An annular combustor with evaporation tubes was designed for certain micro-turbojet engine.According to performance requirements of the engine,designed main components of the combustor,calculated flow distribution and flowage parameters of the combustor.Refers to overall structure of the engine,designed test apparatus of the combustor and carried out the several performance experiments.The results show that the designed combustor meets the demand for structural project,main components and overall performance.

     

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