Volume 35 Issue 1
Jan.  2020
Turn off MathJax
Article Contents
SU Siyuan, HU Chunming, LIU Na. Experiment on cold start of piston aviation kerosene engine[J]. Journal of Aerospace Power, 2020, 35(1): 97-105. doi: 10.13224/j.cnki.jasp.2020.01.012
Citation: SU Siyuan, HU Chunming, LIU Na. Experiment on cold start of piston aviation kerosene engine[J]. Journal of Aerospace Power, 2020, 35(1): 97-105. doi: 10.13224/j.cnki.jasp.2020.01.012

Experiment on cold start of piston aviation kerosene engine

doi: 10.13224/j.cnki.jasp.2020.01.012
  • Received Date: 2019-07-03
  • Publish Date: 2020-01-28
  • Targeting the influencing factors such as starting speed, fuel temperature and ignition energy, an experimental research on the cold start performance of aviation kerosene engine was carried out on a single-cylinder testing machine with a displacement of 650 mL. The results showed that with the increase of the starting speed, the starting time became shorter but then longer, the starting time was the shortest when the starting speed was 1 200 r/min. The rise of the fuel temperature improved the cold starting performance and combustion characteristics. Under the given test conditions, the engine can be successfully started when the fuel temperature was 50 ℃. Increasing ignition energy had a positive effect on the formation of the fire core and the flame propagation, which can significantly shorten the starting time, but when the ignition energy increased to 75 mJ, the improvement effect was not obvious.

     

  • loading
  • [1]
    LI S H,JIN Y,NI K S.Study on the ignition factor of piston kerosene engine[J].Advanced Materials Research,2013,779-780:705-710.
    [2]
    LI S H,JIN Y,NI K S.Study on the ignition factor of piston kerosene engine[J].Advanced Materials Research,2013,779-780:705-710.
    [3]
    KALGHATGI G T.Fuel anti-knock quality:Part Ⅰ engine studies[R].SAE Technical Paper 2001-01-3584,2001.
    [4]
    DUDDY B J,LEE J,WALLUK M,et al.Conversion of a spark-ignited aircraft engine to JP-8 heavy fuel for use in unmanned aerial vehicles[J].SAE International Journal of Engines,2011,4(1):82-93.
    [5]
    WEINZIERL S,WILDEMANN R,HANULA B.The design and development of a light-weight,high-speed,diesel engine for unmanned aerial vehicles[R].SAE Technical Paper 2002-01-0160,2002.
    [6]
    FALKOWSKI D T,ABATA D L,CHO P.The performance of a spark-ignited stratified-charge two stroke engine operating on a kerosine based aviation fuel[R].SAE Technical Paper 972737,1997.
    [7]
    苏鑫鑫,洛静.美国军用无人机的发展新动态[J].飞航导弹,2007(5):27-30. SU Xinxin,LUO Jing.New developments in the US military drones[J].Flying Missile,2007(5):27-30.(in Chinese)
    [8]
    HOOPER P.Experimental experience of cold starting a spark ignition UAV engine using low volatility fuel[J].Aircraft Engineering and Aerospace Technology,2015,89(1):106-111.
    [9]
    CATHCART G,DICKSON G,AHERNS.The application of air-assist direct injection for spark-ignited heavy fuel 2stroke and 4stroke engines[R].SAE Technical Paper,2005-32-0065,2005.
    [10]
    毕延飞.航空重油直喷发动机冷起动性能优化研究[D].天津:天津大学,2017. BI Yanfei.Research on cold start performance optimization of aviation heavy oil direct injection engine[D].Tianjin:Tianjin University,2017.(in Chinese)
    [11]
    胡春明,李骥琦,白洪林,等.航空直喷发动机缸内混合气形成的试验[J].航空动力学报,2012,27(9):1921-1927. HU Chunming,LI Jiqi,BAI Honglin,et al.Experiment of in-cylinder mixture formation process low-pressure GDI engine[J].Journal of Aerospace Power,2012,27(9):1921-1927.(in Chinese)
    [12]
    许善珍,魏民祥,杨光.二冲程煤油发动机稳态工况最小点火能量[J].科学技术与工程,2018,18(7):60-66. XU Shanzhen,WEI Minxiang,YANG Guang.Minimum ignition energy of steady-state conditions for two-stroke kerosene engine[J].Science Technology and Engineering,2018,18(7):60-66.(in Chinese)
    [13]
    刘锐,魏民祥,杨海青,王永伟,贝太学等.二冲程点燃式直喷煤油发动机冷起动控制策略[J].航空动力学报,2017,32(1):213-220. LIU Rui,WEI Minxiang,YANG Haiqing,et al.Cold startcontrol strategy of a two-stroke direct injection spark-ignited kerosene engine[J].Journal of Aerospace Power,2017,32(1):213-220.(in Chinese)
    [14]
    刘志敏,李理光,邓宝清,等.基于首次着火循环的低温冷起动特性[J].燃烧科学与技术,2005,11(4):554-559. LIU Zhimin,LI Liguang,DENG Baoqing,et al.Combustion characteristics of cold start at low temperature based on the first firing cycle analysis[J].Journal of Combustion Science and Technology,2005,11(4):554-559.(in Chinese)
    [15]
    马帅.点燃式航空直喷发动机冷起动工作过程的仿真研究[D].天津:天津大学,2016. MA Shuai.The simulation study on the cold starting process of ignition aviation direct injection engine[D].Tianjin:Tianjin University,2016.(in Chinese)
    [16]
    何邦全,张岩,谢辉,等.过量空气系数对HCCI汽油机燃烧特性的影响[J].燃烧科学与技术,2007,13(4):287-292. HE Bangquan,ZHANG Yan,XIE Hui,et al.Effect of lambda on combustion characteristics of an hcci gasoline engine[J].Journal of Combustion Science and Technology,2007,13(4):287-292.(in Chinese)
    [17]
    张君才.吉布斯自由能变的计算及应用[J].咸阳师范专科学校学报,1999,14(3):49-53. ZHANG Juncai.Calculation and application of Gibbs free energy change[J].Journal of Xianyang Teachers College,1999,14(3):49-53.(in Chinese)
    [18]
    梁金虎,王苏,张灿,等.RP-3航空煤油点火特性研究[J].力学学报,2014,46(3):352-360. LIANG Jinhu,WANG Su,ZHANG Can,et al.Studies on the autoignition characteristics of RP-3 aviation kerosene[J].Chinese Journal of Theoretical and Applied Mechanics,2014,46(3):352-360.(in Chinese)
    [19]
    郑大勇,颜勇,张卫红.氢氧火箭发动机性能敏感性分析[J].火箭推进,2011,37(4):18-23. ZHENG Dayong,YAN Yong,ZHANG Weihong.Analysis for performance parameter sensitivity of hydrogen/oxygen rocket engine[J].Journal of Rocket Propulsion,2011,37(4):18-23.(in Chinese)
    [20]
    王都,盛利,冒晓建,等.点火能量对稀燃增压CNG发动机性能影响的试验研究[J].汽车工程,2009,31(10):915-918. WANG Du,SHENG Li,MAO Xiaojian,et al. Experimental research on the influence of ignition energy on the performance of lean burn supercharged CNG engine[J].Automotive Engineering,2009,31(10):915-918.(in Chinese)
    [21]
    周龙保,刘忠长,高宗英,等.内燃机学[M].北京:机械工业出版社,2011.
  • 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 (889) PDF downloads(418) Cited by()
    Proportional views
    Related

    /

    DownLoad:  Full-Size Img  PowerPoint
    Return
    Return