期刊文献+

基于参数化模型的大型民用飞机设计航程研究 被引量:6

Design range research of large civil aircraft based on parametric model
原文传递
导出
摘要 航程和座级直接反映民用客机的市场定位,是飞机产品能否被市场广泛接受的关键因素。目前全球大型客机市场由波音和空客两家公司垄断,又细分为窄体客机、宽体客机和超大型客机等市场。其中,宽体客机的航程跨度较大,是否发展中、短程宽体客机的争论从未终止。伴随空客公司推出A330区域型客机,中短程宽体客机是否有利可图的争论更加炙手可热。有鉴于此,基于全参数化飞机模型,研究了特定座级下设计航程与机翼、发动机、特征重量、气动特性以及燃油经济性之间的关系,分析了设计航程对民用飞机总体设计带来的影响,从技术层面阐述了设计航程变化带来的收益及代价。 Seats number and design range, as direct reflection of marketing orientation, are the key parameters of a civil aircraft. The current global large airliner market is dominated by Boeing and Airbus, including narrow body aircraft, wide body aircraft and super large aircraft, among which the wide body aircrafts have a large scope of design range, Both Airbus and Boeing have settled the new generation of wide body aircraft as the remote type. However, the controversy of the de- velopment of medium and short range wide body aircraft has never stopped. As Airbus has launched the A330Reginal pro- ject, the profit of medium and short range wide body aircraft becomes hot debate. In view of this, large airliner with certain seats level is selected in this paper to analyze the combined impact of design range on wing, engine, aerodynamic perform- ance, characteristic weights, fuel efficiency and the operating cost, the influence of design range on civil aircraft overall de- sign is also illuminated. Finally the benefit and losses due to design range variation are concluded in the technical prospec-tive.
出处 《航空学报》 EI CAS CSCD 北大核心 2016年第1期112-121,共10页 Acta Aeronautica et Astronautica Sinica
关键词 大型客机 民用飞机 设计航程 总体设计 综合优化 参数化 airliner civil aircraft design ranger overall design synthesis optimization parametric
作者简介 马超男,硕士研究生,工程师。主要研究方向:气动布局及概念方案设计。Tel:021-20865536E-mail:machao@comac.cc 吴大卫男,博士,高级工程师。主要研究方向:飞机总体布局设计。Tel:021-20865535E-mail:wudawei@comae.cc 俞金海男,研究员。主要研究方向:飞机总体气动设计。Tel:021-20864096E-mail:yujinhai@comac.cc 陈迎春男,博士,研究员。主要研究方向:民用飞机设计。Tel:021-20865010E-mail:chenyingchun@comac.cc
  • 相关文献

参考文献13

  • 1艾德·奥波特.运输类飞机的空气动力设计[M].顾诵芬,吴兴世,杨新军,译.上海:上海交通大学出版社,2010:240-303.
  • 2UPTON J. Lockheed L-1011 TriStar-Airliner Tech Vol. 8 [M]. 2001.. 24-27.
  • 3OAG Company. Global air transport outlook[R]. 2014.
  • 4WOODSON S H, DEJARNETTE F R, CAMPBELL J F. An interactive three-dimensional boundary-layer method for transonic flow over swept wings: AIAA-1989-0112[R]. Reston AIAA, 1989.
  • 5HUA J, ZHANG Z Y. Transonic wing design for trans-port aircraft[C]//ICAS Proceedings, 1990, 2: 1316-1322.
  • 6VOLPE G, JAMESON A. Transonic potential flow calcu- lations by two artificial density methods[C]//4th AIAA and ASME, Fluid Mechanics, Plasma Dynamics and La- sers Conference, 1986: 12-14.
  • 7陈俊章,刘盂诏,孙振家.飞机设计手册第8册:重量平衡与控制[M].北京:航空工业出版社,1999:45-55.
  • 8EGBERT T. Synthesis of subsonic airplane design[M]. Delft Delft University Press, 1996: 280-283.
  • 9DANIEL P R. Aircraft design: A conceptual approach fourth edition[M]. Reston AIAA, 2006 21-23.
  • 10OBERT E. Aerodynamic design of transport aircraft[M]. Delft: Delft University Press, 2009: 7-8, 551-552.

共引文献3

同被引文献31

引证文献6

二级引证文献9

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部