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飞机使用升限对增压活塞发动机的匹配要求

徐斌 谭龙兴 杨世春 姬芬竹

徐斌, 谭龙兴, 杨世春, 等 . 飞机使用升限对增压活塞发动机的匹配要求[J]. 北京航空航天大学学报, 2014, 40(12): 1643-1647. doi: 10.13700/j.bh.1001-5965.2013.0746
引用本文: 徐斌, 谭龙兴, 杨世春, 等 . 飞机使用升限对增压活塞发动机的匹配要求[J]. 北京航空航天大学学报, 2014, 40(12): 1643-1647. doi: 10.13700/j.bh.1001-5965.2013.0746
Xu Bin, Tan Longxing, Yang Shichun, et al. Requirement from maximum rate of climbing of aircraft service ceiling to turbocharged reciprocating engine[J]. Journal of Beijing University of Aeronautics and Astronautics, 2014, 40(12): 1643-1647. doi: 10.13700/j.bh.1001-5965.2013.0746(in Chinese)
Citation: Xu Bin, Tan Longxing, Yang Shichun, et al. Requirement from maximum rate of climbing of aircraft service ceiling to turbocharged reciprocating engine[J]. Journal of Beijing University of Aeronautics and Astronautics, 2014, 40(12): 1643-1647. doi: 10.13700/j.bh.1001-5965.2013.0746(in Chinese)

飞机使用升限对增压活塞发动机的匹配要求

doi: 10.13700/j.bh.1001-5965.2013.0746
基金项目: 航空科学基金资助项目(2013ZB51018)
详细信息
    通讯作者:

    姬芬竹

  • 中图分类号: V234.1

Requirement from maximum rate of climbing of aircraft service ceiling to turbocharged reciprocating engine

  • 摘要: 发动机工况调节范围对无人机的安全运行具有重要影响.通过对增压活塞发动机与飞机的动力学分析,得到了使用升限上最大爬升率对螺旋桨和发动机的动力要求,提出了使用升限上发动机可调范围与剩余功率的要求.对增压器匹配提出了新的要求,即使用升限范围内保证飞机巡航工况能够恢复海平面功率.通过某发动机的仿真分析,确定了其使用升限高度的可调工况范围,理论分析了增压器参数对可调范围的影响,给出了匹配原理与建议.该过程也可用来校验使用升限高度下安全性可调裕度,有助于安全操控.

     

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出版历程
  • 收稿日期:  2014-01-08
  • 网络出版日期:  2014-12-20

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