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温度对飞机燃油射流泵工作特性影响

邵垒 刘卫华 潘俊 刘文怡 冯诗愚

邵垒, 刘卫华, 潘俊, 刘文怡, 冯诗愚. 温度对飞机燃油射流泵工作特性影响[J]. 航空动力学报, 2016, 31(9): 2073-2079. doi: 10.13224/j.cnki.jasp.2016.09.004
引用本文: 邵垒, 刘卫华, 潘俊, 刘文怡, 冯诗愚. 温度对飞机燃油射流泵工作特性影响[J]. 航空动力学报, 2016, 31(9): 2073-2079. doi: 10.13224/j.cnki.jasp.2016.09.004
SHAO Lei, LIU Wei-hua, PAN Jun, LIU Wen-yi, FENG Shi-yu. Effect on working characteristic of fuel injection pump in aircrafts of temperature[J]. Journal of Aerospace Power, 2016, 31(9): 2073-2079. doi: 10.13224/j.cnki.jasp.2016.09.004
Citation: SHAO Lei, LIU Wei-hua, PAN Jun, LIU Wen-yi, FENG Shi-yu. Effect on working characteristic of fuel injection pump in aircrafts of temperature[J]. Journal of Aerospace Power, 2016, 31(9): 2073-2079. doi: 10.13224/j.cnki.jasp.2016.09.004

温度对飞机燃油射流泵工作特性影响

doi: 10.13224/j.cnki.jasp.2016.09.004
基金项目: 

国家自然科学基金(50906066);航空科学基金(20122852038,20132852040);江苏高校优势学科建设工程资助项目

详细信息
    作者简介:

    邵垒(1989-),男,重庆奉节人,博士生,主要研究方向为飞行器燃油系统和人机环境工程.

    通讯作者:

    冯诗愚(1974-),男,浙江绍兴人,副教授,博士,主要研究方向为飞行器燃油系统和人机环境工程.E-mail:shiyuf@nuaa.edu.cn

  • 中图分类号: V228

Effect on working characteristic of fuel injection pump in aircrafts of temperature

  • 摘要: 建立了射流泵数学模型,采用数值计算方法对其工作特性进行了模拟,搭建了实验台,采用RP-3燃油,通过实验数据验证了模型的正确性.在此基础上,分别选择了RP-3和JET-A两种燃油,计算了从-40℃~40℃温度下,不同操作压力对射流泵流量比的影响.结果表明:燃油温度高于0℃时,温度对射流泵工作特性影响并不明显,随着温度的降低,射流泵性能与标准温度下(20℃)偏差越来越大,且压比越高此偏差越明显.当温度高于0℃时,采用RP-3和JET-A燃油性能相差不大,RP-3燃油性能略优于JET-A燃油,但是在低温下,RP-3燃油性能远高于JET-A燃油.因此当燃油温度较低且压比较高时,必须充分考虑温度对射流泵特性的影响.

     

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出版历程
  • 收稿日期:  2014-12-11
  • 刊出日期:  2016-09-28

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