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飞机燃油测量传感器优化布局技术

袁梅 何一强 董韶鹏 牛奔

袁梅, 何一强, 董韶鹏, 等 . 飞机燃油测量传感器优化布局技术[J]. 北京航空航天大学学报, 2015, 41(11): 2036-2043. doi: 10.13700/j.bh.1001-5965.2014.0745
引用本文: 袁梅, 何一强, 董韶鹏, 等 . 飞机燃油测量传感器优化布局技术[J]. 北京航空航天大学学报, 2015, 41(11): 2036-2043. doi: 10.13700/j.bh.1001-5965.2014.0745
YUAN Mei, HE Yiqiang, DONG Shaopeng, et al. Aircraft fuel measurement sensor optimal layout technology[J]. Journal of Beijing University of Aeronautics and Astronautics, 2015, 41(11): 2036-2043. doi: 10.13700/j.bh.1001-5965.2014.0745(in Chinese)
Citation: YUAN Mei, HE Yiqiang, DONG Shaopeng, et al. Aircraft fuel measurement sensor optimal layout technology[J]. Journal of Beijing University of Aeronautics and Astronautics, 2015, 41(11): 2036-2043. doi: 10.13700/j.bh.1001-5965.2014.0745(in Chinese)

飞机燃油测量传感器优化布局技术

doi: 10.13700/j.bh.1001-5965.2014.0745
详细信息
    通讯作者:

    袁梅(1967-),女,江苏泰州人,副教授,yuanm@buaa.edu.cn,主要研究方向为检测技术及自动化装置、计算机测控系统、先进传感技术、虚拟仪器技术、复杂系统健康监测技术.

  • 中图分类号: TP29;V228.1

Aircraft fuel measurement sensor optimal layout technology

  • 摘要: 实时、准确地测量出飞机各油箱的剩余油量,对飞机飞行安全十分重要.为了提高飞机燃油的测量精度,设计了一种基于粒子群算法(PSO)的燃油测量传感器优化布局方法.首先,引入燃油实体的概念,建立了某机翼复杂、带隔断多腔油箱CAD模型及箱内燃油实体模型;其次,基于Unigraphics NX(UG)二次开发,完成了飞机不同姿态下、复杂不规则多腔油箱燃油体积的解算;再次,提出了飞机油箱最大燃油可测区(LMR)的概念,并以此作为优化目标进行传感器优化布局;最后,引入可设置边界距离因子(BDF),解决了传感器布局时与油箱壁距离过近的问题.结果表明,该方法实现了多根燃油传感器的布局,可以不受油箱形状和大小的限制,有效避开了油箱内部的干涉区域,保证不同飞行姿态下油量测量的连续性,并使得飞机燃油的可测范围达到较高水平.

     

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出版历程
  • 收稿日期:  2014-12-01
  • 修回日期:  2014-12-26
  • 刊出日期:  2015-11-20

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