Advanced Search
Volume 39 Issue 6
Jun.  2013
Turn off MathJax
Article Contents
Abstract
References
Journal of Beijing University of Aeronautics and Astronautics  > 2013  >  (6): 808-812.
Xiang Kaiheng, Xiao Yelun. Study of System Simulation of Satellite Constellation[J]. Journal of Beijing University of Aeronautics and Astronautics, 1999, 25(6): 629-632. (in Chinese)
Citation: Tang Jiapeng, Xi Ping, Hu Bifu, et al. Knowledge-driven rapid design on aircraft wing structure[J]. Journal of Beijing University of Aeronautics and Astronautics, 2013, (6): 808-812. (in Chinese)
shu

Knowledge-driven rapid design on aircraft wing structure

  • 1.

    School of Mechanical Engineering and Automation, Beijing University of Aeronautics and Astronautics, Beijing 100191, China

  • 2. Shanghai Academy of Spaceflight Technology, Shanghai 201109, China

  • Received Date: 18 Jun 2012
  • Publish Date: 30 Jun 2013
    Abstract
  • In order to improve the quality and efficiency of aircraft wing structure in the preliminary design stage, modeling process of aircraft wing structure was studied. The coordinate of the structure layout and component location parameters rules were defined. Rapid modeling method of wing structure based on the template was represented. The appropriate parametric tool which can meet the development requirements of the wing structure was selected and rapid design system of knowledge-driven aircraft wing structure was developed. Knowledge of design methods, rules and expert experience was encapsulated into a template. Automatic layout of the wing structure was achieved and a layout model was generated. Solid modeling was processed separately according to the different generation logics of layout model. Parametric modeling of the geometric characteristics of the body through user-defined features (UDF) technology was accomplished and automatically instantiated on the basis of the layout model. Finally, aircraft wing box structure example was given to demonstrate that the method is feasible and effective.

     

    • FullText(HTML)
    • References(9)
  • [1]
    Sridhar Chintapalli.The development of a preliminary structural design optimization method of an aircraft wing-box skin-stringer panels[J].Aerospace Science and Technology,2010(14):188-198
    [2]
    Christof Ledermann,Paolo Ermanni.Dynamic CAD objects for structural optimization in preliminary aircraft design[J].Aerospace Science and Technology,2006(10):601-610
    [3]
    La Rocca Gianfranco,Van Tooren Michel J L.A knowledge based engineering approach to support automatic generation of FE models in aircraft design [C]//45th AIAA Aerospace Sciences Meeting.Reno,Nevada:American Institute of Aeronautics and Astronautics,2007,17:11724-11735
    [4]
    La Rocca Gianfranco,Van Tooren Michel J L.Knowledge-based engineering approach to support aircraft multidisciplinary design and optimization[J].Journal of Aircraft,2009,46(6):1875-1885
    [5]
    罗明强,冯昊成,刘虎,等.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,2009,35(4):468-471
    Luo Mingqiang,Feng Haocheng,Liu Hu,et al.Rapid wing structure design and automated scheme adjustment for civil aircraft[J].Journal of Beijing University of Aeronautics and Astronautics,2009,35(4):468-471(in Chinese)
    [6]
    Sensmeier M,Samareh J.Automatic aircraft structural topology generation for multidisciplinary optimization and weight estimation [C]//46th AIAA/ASME/ASC Structures and Materials Conference.Austin,Texas:American Institute of Aeronautics and Astronautics,2005:1893
    [7]
    王义林,胡贤罡,张启丰.基于模板的汽车覆盖件拉延模具结构参数化设计[J].模具,2009,5(4):98-101
    Wang Yilin,Hu Xian-gang,Zhang Qifeng.Parameterized design of the drawing dies structure for automobile panel on the basis of the template[J].Die and Mould,2009,5(4):98-101(in Chinese)
    [8]
    张敏,苏兰海.基于CAA 的CATIA 用户自定义特征创建[J].机械设计与制造,2008,7(6):87-89
    Zhang Min,Su Lanhai.The creation of user defined geometric feature based on CAA/CATIA[J].Machinery Design and Manufacture,2008,7(6):87-89(in Chinese)
    [9]
    Ledermann C,Hanske C,Wenzel J,et al.Associative parametric CAE methods in the aircraft pre-design[J].Aerospace Science and Technology,2005,9(7):641-651
    • Relative Articles

  • Relative Articles

    [1]LU X，SUN Y N，TANG J，et al. Kinematic characteristics analysis of vehicle-aircraft towing taxi system considering wheel deformation[J]. Journal of Beijing University of Aeronautics and Astronautics，2025，51（2）：478-486 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2023.0029.
    [2]JIN B，LI S Y，LIU N N，et al. Kinematic absolute and relative orbit determination of Swarm satellites with heterogeneous orbits[J]. Journal of Beijing University of Aeronautics and Astronautics，2025，51（2）：409-418 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2023.0039.
    [3]TIAN D K，ZHANG J W，JIN L，et al. Design and analysis of morphing wing mechanism based on equilateral Bennett mechanism[J]. Journal of Beijing University of Aeronautics and Astronautics，2025，51（3）：742-752 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2023.0139.
    [4]ZHANG Y M，DAI Y T，WEI R K，et al. Experiment on dynamic response alleviation of a wing with variable-camber flexible trailing edge[J]. Journal of Beijing University of Aeronautics and Astronautics，2024，50（10）：3239-3249 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2022.0761.
    [5]LIU S Y，YANG H L，ZHANG Z G，et al. Vibration control of flexible spacecraft with output constraints and external disturbances[J]. Journal of Beijing University of Aeronautics and Astronautics，2024，50（5）：1560-1567 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2022.0622.
    [6]GENG Z W，ZHANG J，KONG N，et al. Design and analysis of space repeatable mechanical locking and electromagnetic unlocking mechanisms[J]. Journal of Beijing University of Aeronautics and Astronautics，2024，50（12）：3947-3956 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2022.0918.
    [7]LI Y，ZHANG X X，SUN F Q，et al. Belief reliability modeling for assembly accuracy of spaceborne SAR antenna deployable mechanism[J]. Journal of Beijing University of Aeronautics and Astronautics，2024，50（1）：134-143 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2022.0234.
    [8]LIU Y H，HUANG Y，TAN H，et al. On-line prediction method of wing flexible baseline based on autoregressive model[J]. Journal of Beijing University of Aeronautics and Astronautics，2024，50（11）：3426-3433 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2022.0865.
    [9]DONG B X，QIN T，YANG X，et al. Human-machine collaborative control of forward shovel hydraulic mining excavators[J]. Journal of Beijing University of Aeronautics and Astronautics，2024，50（6）：1952-1959 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2022.0517.
    [10]LI Xing-fei, HAN Jia-xin, TUO Wei-xiao, LIU Ya-qi, WANG Tian-yu. Influence analysis of flexure support characteristics on performance of inertial reference unit[J]. Journal of Beijing University of Aeronautics and Astronautics. doi: 10.13700/j.bh.1001-5965.2023.0461
    [11]MENG G，HUANG H，WU W G，et al. Parasitic rotation of large stroke compliant micro-positioning platform[J]. Journal of Beijing University of Aeronautics and Astronautics，2023，49（3）：665-673 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2021.0272.
    [12]ZHANG Z，WANG P，ZHOU H Y. Reliability analysis of nozzle adjustment mechanism with interval distribution parameters[J]. Journal of Beijing University of Aeronautics and Astronautics，2023，49（12）：3377-3385 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2022.0089.
    [13]HE T Y，DONG Y，WANG H，et al. Design and optimization of modular parabolic deployable mechanism[J]. Journal of Beijing University of Aeronautics and Astronautics，2023，49（9）：2473-2481 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2021.0652.
    [14]YANG Z J，WANG G，ZHAO R J，et al. Dynamic analysis of deployment impact of trim-wing mechanism of Mars entry capsules[J]. Journal of Beijing University of Aeronautics and Astronautics，2023，49（2）：422-429 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2021.0234.
    [15]WU Y，XIE C C，YANG C. Optimal design of shape and motion parameters of a flapping wing[J]. Journal of Beijing University of Aeronautics and Astronautics，2023，49（12）：3311-3320 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2022.0146.
    [16]HE L T，FANG H R，CHEN Y F，et al. Design and performance analysis of spatial large extension parallel mechanism[J]. Journal of Beijing University of Aeronautics and Astronautics，2023，49（7）：1722-1734 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2021.0548.
    [17]YANG Yi-feng, WANG Yi, LIU Ao-yu, LI Jia, XIE Li-yang. Calculation and error analysis of kinematic accuracy reliability of VSV adjustment mechanism[J]. Journal of Beijing University of Aeronautics and Astronautics. doi: 10.13700/j.bh.1001-5965.2023.0410
    [18]DU Xianchen, LIU Xue'ao, DONG Yang, WANG Hui, HE Tianyu, WANG Chunjie. Design and dimensional synthesis of a variable wing sweep mechanism[J]. Journal of Beijing University of Aeronautics and Astronautics, 2022, 48(12): 2502-2509. doi: 10.13700/j.bh.1001-5965.2021.0125
    [19]NIE Liangyi, DING Huafeng, WANG Jun, BI Shusheng. Branch graph method for crank judgement of complex multi-loop linkage[J]. Journal of Beijing University of Aeronautics and Astronautics, 2022, 48(10): 1863-1874. doi: 10.13700/j.bh.1001-5965.2021.0152
    [20]ZHANG Libo, LI Yupeng, ZHU Deming, FU Yongling. Inverse kinematic solution of nursing robot based on genetic algorithm[J]. Journal of Beijing University of Aeronautics and Astronautics, 2022, 48(10): 1925-1932. doi: 10.13700/j.bh.1001-5965.2021.0042
    • Supplements(0)
    • Cited By
  • 加载中

Catalog

    通讯作者: 陈斌, bchen63@163.com
    • 1. 

      沈阳化工大学材料科学与工程学院 沈阳 110142

    1. 本站搜索
    2. 百度学术搜索
    3. 万方数据库搜索
    4. CNKI搜索
    Get Citation
    PDF
    XML

    Article Metrics

    Article views(1521) PDF downloads(675) Cited by()
    Proportional views
    Related

    Copyright © Journal of Beijing University of Aeronautics and Astronautics

    Address: Editorial Department of Journal of Beijing University of Aeronautics and Astronautics, 37 Xueyuan Road, Haidian District, Beijing Post Code: 100191 Email: jbuaa@buaa.edu.cn

    Supported by: Beijing Renhe Information Technology Co., Ltd.    

    /

    DownLoad:  Full-Size Img  PowerPoint
    Return
    Return