Volume 29 Issue 3
Mar.  2014
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SHAO Fei, WANG Hong-ming. Design principles and experiment on gas generator and high-temp gas release valve for aviation[J]. Journal of Aerospace Power, 2014, 29(3): 719-726. doi: 10.13224/j.cnki.jasp.2014.03.033
Citation: SHAO Fei, WANG Hong-ming. Design principles and experiment on gas generator and high-temp gas release valve for aviation[J]. Journal of Aerospace Power, 2014, 29(3): 719-726. doi: 10.13224/j.cnki.jasp.2014.03.033

Design principles and experiment on gas generator and high-temp gas release valve for aviation

doi: 10.13224/j.cnki.jasp.2014.03.033
  • Received Date: 2013-03-25
  • Publish Date: 2014-03-28
  • The design thoughts of gas generator and high-temp gas release valve were introduced, and their design principles were developed and confirmed experimentally. The experimental results show that, the gas generator can work steadily in the environment where the air mass flow rate is 0.025kg/s, the work temperature being up to 950℃, and the fluctuation of combustion temperature being ±10℃, and high-temp gas release valve has the characteristics of no leakage at 1200℃. The indexes above are higher than those of experiments for vehicles and grounds. Using the gas generator and high-temp gas release valve, the turbocharger characteristic can be obtained accurately and completely, helping to realize optimum altitude performance of state of art aero-piston engine.

     

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  • [1]
    陈妍,王洪铭.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 turbosupercharged piston engine[J].Journal of Beijing University of Aeronautics and Astronautics,1998,24(1):16-20.(in Chinese)
    [2]
    陆家祥.车用内燃机增压[M].北京:机械工业出版社,1993.
    [3]
    沈权.内燃机增压[M].北京:中国铁道出版社,1990.
    [4]
    林建生,谭旭光.燃气轮机与涡轮增压内燃机原理及应用[M].天津:天津大学出版社,2005.
    [5]
    李刚.内燃机[M].北京:中国铁道出版社,2007.
    [6]
    秦有方,陈士尧,王文波.车用内燃机原理[M].北京:北京理工大学出版社,1997.
    [7]
    徐华舫.空气动力学基础[M].北京:国防工业出版社,1979.
    [8]
    Loth J L,Morris G J,Metlapalli P.Staged turbocharging for high altitude IC engines[R].AIAA 97-3294,1997.
    [9]
    钟华贵,刘坤,文国治.车用涡轮增压器试验台与试验技术[J].燃气涡轮试验与研究,2003,16(4):37-41. ZHONG Huagui,LIU Kun,WEN Guozhi.Test rig and test technology of turbocharger for vehicles[J].Gas Turbine Experiment and Research,2003,16(4):37-41.(in Chinese)
    [10]
    于立国,马朝臣,施新,等.车用涡轮增压器涡轮非稳态特性试验研究[J].内燃机工程,2010,31(5):36-40. YU Liguo,MA Chaochen,SHI Xin,et al.Experimental investigation on vehicular turbocharger turbine characteristics under unsteady flow condition[J].Chinese Internal Combustion Engine Engineering,2010,31(5):36-40.(in Chinese)
    [11]
    霍磊,王洪铭.不同燃料对涡轮增压器试验的影响[J].航空动力学报,2012,27(7):1537-1541. HUO Lei,WANG Hongming.Effect of various fuels used on turbocharger experiment[J].Journal of Aerospace Power,2012,27(7):1573-1541.(in Chinese)
    [12]
    宋兆泓.航空发动机故障分析[M].北京:航空工业出版社,1995.
    [13]
    斯廖赫先科.空气喷气发动机原理[M].王振华,陆亚钧,译.北京:国防工业出版社,1982.
    [14]
    王乃行,徐敦镳.航空燃气涡轮发动机原理[M].北京:国防工业出版社,1982.
    [15]
    曾川,王洪铭.微涡喷发动机离心甩油盘环形折流燃烧室的设计与实验研究[J].航空动力学报,2003,18(1):92-96. ZENG Chuan,WANG Hongming.The design and study of the annular combustion chamber with centrifugal fuel injection[J].Journal of Aerospace Power,2003,18(1):92-96.(in Chinese)
    [16]
    王洪铭,朱志伟,张叔农.蒸发室模型试验研究[J].航空动力学报,1992,7(1):65-68. WANG Hongming,ZHU Zhiwei,CHANG Shunong.The experimental study on the performance of evaporator model[J].Journal of Aerospace Power,1992,7(1):65-68.(in Chinese)
    [17]
    孙跃中.蒸发管喷嘴燃油雾化特性试验研究[J].航空动力学报,1989,4(3):277-279. SUN Yuezhong.An experimental study on fuel spray atomizing characteristics of evaporating pipe atomizer[J].Journal of Aerospace Power,1989,4(3):277-279.(in Chinese)
    [18]
    刘鸿志,王洪铭.光电火焰信号传感器:中国,91202796.7[P].1992-05-06.
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