航空学报 > 2009, Vol. 30 Issue (4): 649-653

大型民用客机起飞重量估算方法

李成功,程静,刘沛清   

  1. 北京航空航天大学 航空科学与工程学院
  • 收稿日期:2008-02-26 修回日期:2008-05-09 出版日期:2009-04-25 发布日期:2009-04-25
  • 通讯作者: 李成功

Take-off Weight Calculation Method for Civil Airplanes

Li Chenggong, Cheng Jing, Liu Peiqing   

  1. School of Aeronautic Science and Engineering, Beijing University of Aeronautics and Astronautics
  • Received:2008-02-26 Revised:2008-05-09 Online:2009-04-25 Published:2009-04-25
  • Contact: Li Chenggong

摘要: 推导了一种在概念设计阶段快速估算大型民用客机起飞重量的方法,针对近年来新型民用飞机的设计数据对计算公式的系数进行了重新修正,从而更加准确估算未来民用客机设计起飞重量。对该方法的收敛性以及解的存在性进行了分析。以中国将进行研制的干线民用客机为例,对该计算方法的有效性进行了实际的计算验证,分析了起飞重量的合理取值范围。其计算方法以及计算结果对中国未来干线民用客机的设计具有直接参考价值。

关键词: 起飞重量, 民用客机, 估算, 收敛性, 干线

Abstract: A method for determining civil airplane take-off weight for a given mission profile is presented which can rapidly estimate the weight of a large civil airplane in the conceptual design process for the manufacture of airplanes. The coefficients in the calculation formula are revised based on the design data of recent commercial airplanes to predict the weight more precisely. Existence of the solutions by this method and the convergence property of this method are also justified in this article. The estimation method is verified by a design example of an arterial civil airplane for China. The reasonable range of the calculation result of the airplane is also discussed in the article. These results can be of direct value to future design for China’s civil airplane project.

Key words: take-off weight, civil airplane, estimation, convergence, artery

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