Volume 35 Issue 8
Aug.  2009
Turn off MathJax
Article Contents
Song Yuwang, Xi Ping. Research and application of analysis leads design method[J]. Journal of Beijing University of Aeronautics and Astronautics, 2009, 35(8): 980-985. (in Chinese)
Citation: Song Yuwang, Xi Ping. Research and application of analysis leads design method[J]. Journal of Beijing University of Aeronautics and Astronautics, 2009, 35(8): 980-985. (in Chinese)

Research and application of analysis leads design method

  • Received Date: 20 Jun 2008
  • Publish Date: 31 Aug 2009
  • The analysis leads design(ALD) method was advanced to summarize the key concepts and analyze the essential ideas from the iterative phenomena during the product design process. The concepts of design information(DI), design activity(DA), design model(DM), design file(DF) and analysis leads design flow(ALDF) in the ALD method were defined. As self-driven design flow, ALDF was the core concept of the ALD method. The process of establishing the ALDF was the ALD method. The design information and the design activity of the ALD flow were elaborated. The serial and parallel methods to order the design activity of the ALDF were emphasized, of which the function of time cost was given. The product design plan was optimized by the ALDF to improve the design quality and efficiency. Some key techniques of the ALD method were resolved, and the ALD method was exemplified by the structure design of the turbo-jet blade. And the conditions, the self-driven design flow, the diagram of geometry variables and performance variables of the example were given.

     

  • loading
  • [1] 王振国,陈小前,罗文彩,等.飞行器多学科设计优化理论与应用研究[M].北京:国防工业出版社,2006:35 Wang Zhenguo, Chen Xiaoqian, Luo Wencai, et al. Research on the theory and application of multidisciplinary design optimization of flight vechicles[M]. Beijing:National Defence Industry Press,2006:35(in Chinese) [2] Pahl G, Beitz W. Engineering design[M]. London: Springer, 2001 [3] 吴立强,尹泽勇,蔡显新.航空发动机涡轮叶片的多学科设计优化[J].航空动力学报, 2005, 20 (5):795-801 Wu Liqiang, Yin Zeyong, Cai Xianxin. MDO technology applied to the aeroengine turbine blade design[J]. Journal of Aerospace Power, 2005, 20(5):795-801(in Chinese) [4] 舒彪,韩前鹏,邓家褆.基于多学科涡轮叶片气动设计优化[J].南京航空航天大学学报,2005,37(6):714-719 Shu Biao, Han Qianpeng, Deng Jiati. Aerodynamic design optimization of turbine blade based on multidiscipline[J]. Journal of Nanjing University of Aeronautics & Astronautics,2005,37(6):714-719(in Chinese) [5] 宋玉旺, 席平. 基于特征造型技术的涡轮叶片参数化设计[J]. 北京航空航天大学学报, 2004, 30(4):321-324 Song Yuwang, Xi Ping.Parametric design of turbine blades based on feature modeling[J]. Journal of Beijing University of Aeronautics and Astronautics,2004,30(4):321-324(in Chinese) [6] 宋玉旺,余伟巍,朱剑,等.变壁厚涡轮叶片参数化设计[J].计算机辅助设计与图形学报,2008,20(3):304-309 Song Yuwang, Yu Weiwei, Zhu Jian, et al. Parametric design of turbo-jet blades with unequal thickness[J]. Journal of Computer-Aided Design & Computer Graphics, 2008,20(3):304-309(in Chinese)
  • 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

    Article Metrics

    Article views(2617) PDF downloads(875) Cited by()
    Proportional views
    Related

    /

    DownLoad:  Full-Size Img  PowerPoint
    Return
    Return