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参数化大型客机方案实例库研究 被引量:2

Research on Case Base of Parameterized Large Civil Aircraft
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摘要 为充分利用和借鉴已有的大型客机方案实例信息,建立了参数化大型客机方案实例库,并在一个开放式飞机总体设计环境中完成了方案实例三维建模和相关参数入库,提出了面向对象的参数化实例方法。在此基础上实现了对实例库中客机参数的管理、参数分析,并通过初始布局方案的模块化设计,为总体设计阶段新方案的快速设计及初步分析奠定了一定的基础。最后通过应用示例说明了实例库在总体设计阶段的运用。 In order to utilize and study more effectively information of existing examples of large civil aircraft entities,a case base of parameterized large civil aircraft is established,and in the open conceptual aircraft design system,the examples of three-dimensional modeling are completed and related parameters are stored in the case base.Then,the method of surface parameter to the object instance is proposed.On this basis,the management of aircraft parameters in the case base and parameter analysis is realized.In addition,a new method is proposed that can form a new layout project through parts modular design and adjustment.All this lay the foundation for the quick design and preliminary analysis of new programs in the concept design stage.Finally, an instance of application examples illustrates the use of case base in the overall design phase.
作者 田永亮 刘虎 罗明强 武哲 Tian Yongliang, Liu Hu, Luo Mingqiang, Wu Zhe (School of Aeronautic Science and Engineering, Beijing University of Aeronautics and Astronautics, Beijing 100191, China)
出处 《航空学报》 EI CAS CSCD 北大核心 2010年第11期2202-2208,共7页 Acta Aeronautica et Astronautica Sinica
基金 致谢 感谢王晓璐老师对本文提出的宝贵意见.
关键词 飞机设计 实例库 参数化模型 参数选择 部件组合设计 aircraft design case base parametric model preference parts modular design
作者简介 田永亮(1985-)男,硕士研究生。主要研究方向:飞机总体设计技术及相关领域。Tel:010-82315871E—mail:flyawaytian@163.com 刘虎(1980-)男,副教授。主要研究方向:飞机总体设计技术及相关领域。通讯作者:刘虎E-mail:aerodesigner@163.com. 罗明强(1981-)男,博士。主要研究方向:飞机总体设计技术及相关领域。E-mail:lmq19810222@163.com. 武哲(1957-)男,教授。主要研究方向:飞机总体设计技术及相关领域。Email:wuzhe@buaa.edu.cn
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参考文献14

  • 1顾诵芬编著..飞机总体设计[M].北京:北京航空航天大学出版社,2001:409.
  • 2Simos D. PIANO user's guide[EB/OL]. Lissys Limited. (2008- 06 -21)[2009- 07 -21]. http://www, lissys, demon. co. uk/feats, html. 被引量:1
  • 3中国航空信息中心.世界飞机手册[M].北京:航空工业出版社,2001. 被引量:2
  • 4Paul J. Jane's all the world's aircraft 2004-2005[M]. Alexandria: .lane's Information Group Inc. , 2005. 被引量:1
  • 5罗明强,刘虎,武哲.开放式飞机总体设计环境的原型研究[J].航空学报,2008,29(4):954-959. 被引量:9
  • 6刘虎..飞机概念设计支持理论与原型系统研究[D].北京航空航天大学,2004:
  • 7Liu H. Case-based reasoning for developing initial aircraft coneepts[C]//Collection of Technical Papers 44th AIAA Aerospace Sciences Meeting. 2006, 23: 17825 -17834. 被引量:1
  • 8罗明强,冯昊成,刘虎,武哲.民用飞机机翼结构快速设计及自动化调整[J].北京航空航天大学学报,2009(4):468-471. 被引量:11
  • 9737 airplane characteristics for airport planning[EB/OL]. (2005-10- 01) [2009-04-15]. http: //www. boeing, com/ commercial/737family/specs, html. 被引量:1
  • 10767 airplane characteristics for airport planning[EB/OL]. (2005-12-01)[2009-04-20]. http://www. boeing, com/ commercial/767 family/specs, html. 被引量:1

二级参考文献23

  • 1Leifsson L T. Multidisciplinary design optimization of low-noise transport aircraft [ D]. Virginia: Department of Aerospace and Ocean Engineering, Virginia Polytechnic Institute and State Uni versity, 2006 被引量:1
  • 2Wagner T, Valasek J. Comparison of computational methods for stability and control analysis[ R]. AIAA Paper 2005-140, 2005 被引量:1
  • 3Fidanci M, Miller J R, Strauss D J. Integrating automated multi- disciplinary optimization in preliminary design of non-traditlonal aircraft[ R]. ADA380252, 2000 被引量:1
  • 4Roskam J, Anemaat W A. General aviation aircraft design methodology in a PC environment[ R]. AIAA Paper 96-5520, 1996 被引量:1
  • 5Raymer D P. Aircraft design : a conceptual approach [ M ]. 3rd edition. Reston: AIAA Inc, 1999 被引量:1
  • 6Wagner T, Valasek J. Comparison of computational methods for stability and control analysis [R]. AIAA- 2005-140, 2005. 被引量:1
  • 7Griffiths R C, Visser K D. Panel code estimates of wind tunnel wall and support interference effects on the HSCT [R]. AIAA-2000-4020, 2000. 被引量:1
  • 8Knapp M, Lednicer D. MGAERO validation using KC 135 flight and tunnel data[R]. AIAA-2000-4021. 2000. 被引量:1
  • 9Abanto J, Pelletier D,Garon A,et al. Verification of some commercial CFD codes on atypical CFD problems [R].AIAA-2005-682, 2005. 被引量:1
  • 10Mike R. MSC/NASTRAN 2001 DMAP programmer's guide[M]. MSC. Software Corporation, 2002. 被引量:1

共引文献14

同被引文献29

  • 1卢新来,刘虎,武哲.直升机概念设计中的部件参数化[J].北京航空航天大学学报,2006,32(1):46-49. 被引量:3
  • 2[5]李为吉.飞机总体设计[M].西安:西北工业大学出版社,2005.209-216. 被引量:5
  • 3Sensmerier M D, Samareh J R. Automatic aircraft struc- tural topology generation for muhidisciplinary optimiza- tion and weight estimation. AIAA-2005-1893, 2005. 被引量:1
  • 4Masonud R R, A framework for preliminary design of air- craft structures based on process information. NASA NAG-1-1716, 1998. 被引量:1
  • 5Raymer D P. Aircraft design: a conceptual approach. 3rd ed. Reston: AIAA Inc., 1999. 被引量:1
  • 6陈迎春,宋文滨,刘洪.民用飞机总体设计.上海:上海交通大学出版社,2010. 被引量:1
  • 7Roskam J. Aircraft design. Ottawa: Roskam Aviation and Engineering Corporation, 1985. 被引量:1
  • 8Kulfan B M. Universal parametric geometry representa- tion method. Journal of Aircraft, 2008, 45(1): 142-158. 被引量:1
  • 9Kulfan B M, Bussoletti J E. Fundamental parametric ge- ometry representations for aircraft component shapes. AIAA-2006-6948, 2006. 被引量:1
  • 10Liu H, Wu Z, Wang G L, et al. Implementation of a sketch based approach to conceptual aircraft design syn- thesis and modeling. Chinese Journal of Aeronautics, 2004, 17(4): 207-214. 被引量:1

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