Volume 18 Issue 6
Dec.  2003
Turn off MathJax
Article Contents
HUANG Guo-ping, LI Bo, WEN Quan, LIANG De-wang. Top Level Design of Micro Turbine Jet Engine[J]. Journal of Aerospace Power, 2003, 18(6): 832-838.
Citation: HUANG Guo-ping, LI Bo, WEN Quan, LIANG De-wang. Top Level Design of Micro Turbine Jet Engine[J]. Journal of Aerospace Power, 2003, 18(6): 832-838.

Top Level Design of Micro Turbine Jet Engine

  • Received Date: 2003-03-29
  • Rev Recd Date: 2003-08-09
  • Publish Date: 2003-12-28
  • The top-level design of micro turbine jet-engine is presented in the paper.Firstly,the relationship between dimensions and performance of micro turbine engine is analysed.Results show that micro turbine engines have potential larger ratio of thrust to weight than conventional engines.A preliminary design of a micro turbine engine is illustrated on the basis of the related technologies that can be achieved recently.Parametric analysis of performance,such as:thrust,specific fuel consumption,energy efficiency,exhaust gas temperature,was performed by changing one or two of 7 variables.In order to assess if the design of the micro turbine engine is capable of generating the reguired thrust when put into practice,a convenient criterion is formulated,and three designs of micro turbine engine are obtained for high,moderate and low performance.

     

  • loading
  • 加载中

Catalog

    通讯作者: 陈斌, bchen63@163.com
    • 1. 

      沈阳化工大学材料科学与工程学院 沈阳 110142

    1. 本站搜索
    2. 百度学术搜索
    3. 万方数据库搜索
    4. CNKI搜索

    Article Metrics

    Article views (2934) PDF downloads(621) Cited by()
    Proportional views
    Related

    /

    DownLoad:  Full-Size Img  PowerPoint
    Return
    Return