Large eddy simulation of film cooling under rotating condition[J]. Journal of Beijing University of Aeronautics and Astronautics, 2010, 36(5): 529-533. (in Chinese)
Citation: Xu Bin, Wei Ling, Zhao Penget al. Match analysis on two-stage turbo charging system of piston aero-engine[J]. Journal of Beijing University of Aeronautics and Astronautics, 2008, 34(05): 551-554. (in Chinese)

Match analysis on two-stage turbo charging system of piston aero-engine

  • Received Date: 23 Apr 2007
  • Publish Date: 31 May 2008
  • To reach the motive force requirement of high altitude light aero-plane, a two-stage turbo charging system matching design analysis was performed for a turbo charging piston aero-engine. The software package of AVL boost was used to establish a theoretical analytic model of the supercharged prototype engine. The model was verified and validated though experiments. The model of two-stage turbocharging engine was set up on the basis of the model of prototype engine, and the matching calculates had been done. The characteristics of engine in different altitude above sea level were calculated, and the effects of engine major parameters for the performance were analyzed. The rule of the bypass valve regulating the two-stage turbocharging system was studied. The variation trend of high and low stage compressor-s total pressure ratio versus the different altitude was defined. The result shows that the two-stage turbocharging system can provide high boost pressure, which can be maintained the requested engine power. These work reaches the anticipated design object.

     

  • [1] 朱大鑫.涡轮增压与涡轮增压器[M].北京:机械工业出版社,1992 Zhu Daxin. Turbocharging and turbocharger [M].Beijing: China Machine Press, 1992(in Chinese) [2] 陈妍,王洪明.一种带涡轮增压器的活塞发动机调节及其特性[J].北京航空航天大学学报,1998,24(1):16-20 Chen Yan, Wang Hongming. Control and performance of a turbo supercharged piston engine [J].Journal of Beijing University of Aeronautics and Astronautics, 1998, 24(1):16-20(in Chinese) [3] 陈华舫.空气动力学基础[M].第2版.北京:北京航空学院出版社,1987 Chen Huafang.The basics of aerodynamics [M].2nd ed. Beijing: Beijing University of Aeronautics and Astronautics Press, 1987 (in Chinese) [4] Benson R S, Svetnicka F V. Two-stage turbocharging of diesel engines: a matching procedure and an experimental investigation .SAE Technical Papers,740740,1974 [5] Zhang Hong, Ma Chaochen. Development of turbocharger for improving diesel engine matching performance [J]. Journal of Beijing Institute of Technology, 2002, (2):146-149
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