民用飞机系列商载航程匹配设计

蒙文巩; 马东立; 崔飞

民用飞机系列商载航程匹配设计

北京航空航天大学航空科学与工程学院, 北京 100191

详细信息

中图分类号: V211.41
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出版历程
- 收稿日期: 2012-01-05
- 网络出版日期: 2013-02-28

Matching design for payload and range of civil aircraft family

School of Aeronautic Science and Engineering, Beijing University of Aeronautics and Astronautics, Beijing 100191, China

摘要

摘要: 民用飞机产品开发的模式已从"单型飞机"的概念向"飞机系列"概念转化.根据模块化和通用性的策略,发展了飞机系列化设计方法,给出了飞机系列主要参数的设计原则和飞机系列经济性的描述方法,建立了飞机系列商载航程匹配设计模型.分析了商载和航程的匹配关系对飞机系列经济性的影响,利用Pareto多目标遗传算法,完成了某一民用飞机系列商载和航程的匹配设计,对不同设计方案的参数进行了比较分析,取得了较好的设计结果.
- 飞机系列 /
- 通用性 /
- 匹配设计 /
- Pareto遗传算法
Abstract: There has been a pattern transform from single model to family with multiple models for the civil aircraft-developing concept. According to the strategies of modularization and generality,the aircraft family design method was developed. The design principle of the main parameters and the economic description method for the aircraft family were presented. Then the matching design model for payload and range of the aircraft family was established. The impact of the matching relationship of the payload and the range acting on the economy of the aircraft family was analyzed, too. With application of Pareto multi-objective genetic algorithm, the matching design for payload and range of a civil aircraft family was accomplished. The parameter comparison of different design schemes was carried out,and the results are satisfactory.
- aircraft family /
- generality /
- matching design /
- Pareto multi-objective genetic algorithm

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参考文献(13)

[1]	Willcox K,Wakayama S.Simultaneous optimization of a multiple aircraft family [J].Journal of Aircraft,2003,41(4):616-622
[2]	Allison J,Roth B,Kokkolaras M,et al.Papalambros aircraft family design using decomposition-based method [J].AIAA 2006-6950,2006
[3]	雍明培,余雄庆.基于模块化产品平台的飞机族设计技术探讨[J].飞机设计,2006(4):30-37 Yong Mingpei,Yu Xiongqing.Aircraft family design using modular product platform methodology:an exploratory study [J].Aircraft Design,2006(4):30-37(in Chinese)
[4]	Simpson T W,D'Souza B.Assessing variable levels of platform commonality within a product family using a multi-objective genetic algorithm [J].AIAA 2002-5427,2002
[5]	Fujita K.Product variety optimization under modular architecture [J].Computer-Aided Design,2002,34(12):953-965
[6]	雍明培.基于模块化通用平台策略的飞机族设计优化方法[D].南京:南京航空航天大学航空宇航学院,2008 Yong Mingpei.Design optimization method for modular platform-based aircraft family [D].Nanjing:College of Aerospace Engineering,Nanjing University of Aeronautics and Astronautics,2008(in Chinese)
[7]	雍明培,余雄庆.飞机族的机翼气动外形优化方法[J].南京航空航天大学学报,2008,40(4):475-479 Yong Mingpei,Yu Xiongqing.Wing aerodynamic optimization method for aircraft family design [J].Journal of Nanjing University of Aeronautics & Astronautics,2008,40(4):475-479(in Chinese)
[8]	雍明培,余雄庆.一种面向飞机族的结构优化方法[J].航空学报,2008,29(3):664-669 Yong Mingpei,Yu Xiongqing.A structural optimization method for aircraft family [J].Acta Aeronautica et Astronautica Sinica,2008,29(3):664-669(in Chinese)
[9]	李为吉.现代飞机总体综合设计[M].西安:西北工业大学出版社,2001:4-10 Li Weiji.Modern aircraft conceptual design synthesis[D].Xi'an:Northwestern Polytechnical University,2001:4-10(in Chinese)
[10]	陈迎春,宋文滨,刘洪.民用飞机总体设计[M].上海:上海交通大学出版社,2010:30-31 Chen Yingchun,Song Wenbin,Liu Hong.Civil aircraft design [M].Shanghai:Shanghai Jiao Tong University Presss,2010:30-31(in Chinese)
[11]	Koopmans C.Analysis of production as an efficient combination of activities [M].[S.l.]:John Wiley and Sons,1951:33-97
[12]	Crossley W A,Cook A M.Using the two-branch tournament genetic algorithm for multi-objective design[R].AIAA-98-1914,1998
[13]	崔逊学.多目标进化算法及其应用[M].北京:国防工业出版社,2006:48-58 Cui Xunxue.Multi-objective evolutionary algorithms and their applications [M].Beijing:National Defense Industry Press,2006:48-58(in Chinese)