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提高四冲程点燃式重油航空发动机抗爆性措施

陈方超 杨海青 刘锐 丁昌露 杨琦

陈方超, 杨海青, 刘锐, 丁昌露, 杨琦. 提高四冲程点燃式重油航空发动机抗爆性措施[J]. 航空动力学报, 2018, 33(3): 611-619. doi: 10.13224/j.cnki.jasp.2018.03.013
引用本文: 陈方超, 杨海青, 刘锐, 丁昌露, 杨琦. 提高四冲程点燃式重油航空发动机抗爆性措施[J]. 航空动力学报, 2018, 33(3): 611-619. doi: 10.13224/j.cnki.jasp.2018.03.013
Measures to improve anti-knock quality for four-stroke ignited kerosene aviation engine[J]. Journal of Aerospace Power, 2018, 33(3): 611-619. doi: 10.13224/j.cnki.jasp.2018.03.013
Citation: Measures to improve anti-knock quality for four-stroke ignited kerosene aviation engine[J]. Journal of Aerospace Power, 2018, 33(3): 611-619. doi: 10.13224/j.cnki.jasp.2018.03.013

提高四冲程点燃式重油航空发动机抗爆性措施

doi: 10.13224/j.cnki.jasp.2018.03.013

Measures to improve anti-knock quality for four-stroke ignited kerosene aviation engine

  • 摘要: 应用GT-Power软件,对某四冲程点燃式航空活塞增压发动机进行使用不同燃料的一维性能仿真分析,针对低辛烷值燃料易发生爆震的特性,分别采用添加抗爆添加剂、调整发动机的压缩比、增压压力、空燃比、缸径、点火提前角等参数,在抑制爆震的前提下尽可能实现发动机功率恢复。将原93#汽油燃料换成辛烷值为61的特种煤油燃料后,在不扩大气缸直径和扩大气缸直径两种方案下,发动机功率恢复分别达到原型机的89%和95%,油耗率分别增加5.4%和6.1%,排气温度分别提高11.4%和13.4%。

     

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出版历程
  • 收稿日期:  2016-09-08
  • 刊出日期:  2018-03-28

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