Volume 29 Issue 11
Nov.  2014
Turn off MathJax
Article Contents
HAO Yan-hua, HUANG Zhi-jian. Optimization design of tenon connection structure based on coordinate correlation method[J]. Journal of Aerospace Power, 2014, 29(11): 2716-2721. doi: 10.13224/j.cnki.jasp.2014.11.024
Citation: HAO Yan-hua, HUANG Zhi-jian. Optimization design of tenon connection structure based on coordinate correlation method[J]. Journal of Aerospace Power, 2014, 29(11): 2716-2721. doi: 10.13224/j.cnki.jasp.2014.11.024

Optimization design of tenon connection structure based on coordinate correlation method

doi: 10.13224/j.cnki.jasp.2014.11.024
  • Received Date: 2013-11-11
  • Publish Date: 2014-11-28
  • To solve the problem about the design optimization process interruption due to geometric dimensional interference in the process of structure optimization design, a method(coordinate correlation method) was established, making suitable for optimization design of structure modeling. This method was applied to aeroengine tenon connection structure optimization design; the process was smooth, and structural modeling of 790 times was completed without any problems due to geometric changes. The optimization design results show that the maximum stress on the groove throat area drops by 19.1% though the changes before and after optimization of tenon connection structure shape are not big. The stress levels are significantly lower, and the structure model meets the engineering requirements.

     

  • loading
  • [1]
    吕辉停,郝艳华,黄致建,等.弧形燕尾榫结构设计及形状优化[J].航空动力学报,2011,26(6):1295-1300. LV Huiting,HAO Yanhua,HUANG Zhijian,et al.Structure design and shape optimization in arc dovetail[J].Journal of Aerospace Power,2011,26(6):1295-1300.(in Chinese)
    [2]
    杨伟,郝艳华,黄致建.圆弧榫风扇盘结构的优化设计[J].华侨大学学报,2013,34(6):601-604. YANG Wei,HAO Yanhua,HUANG Zhijian.Structure optimization design of arc tenon fan disc[J].Journal of Huaqiao University,2013,34(6):601-604.(in Chinese)
    [3]
    胡仁喜,王庆五,闫石.ANSYS8.2机械设计高级应用实例[M].北京:机械工业出版社,2005.
    [4]
    杨敏超,孙苏亚.涡轮榫头/榫槽的结构优化设计[J].航空动力学报,2010,25(8):1876-1882. YANG Minchao,SUN Suya.Structural optimization of turbine tenon/mortise[J].Journal of Aerospace Power,2010,25(8):1876-1882.(in Chinese)
    [5]
    刘长福,邓明.航空发动机结构设计分析[M].西安:西北工业大学出版社,2010.
    [6]
    陈光.航空发动机结构设计分析[M].北京:北京航空航天大学出版社,2006.
    [7]
    李宏新,黄致建,张力,等.一种排除带凸肩风扇叶片榫头故障的新方法[J].航空发动机,2002(2):27-30. LI Hongxin,HUANG Zhijian,ZHANG Li,et al.New technique for eliminating fault of the tenon of fan blade with mid-span shroud[J].Aeroengine,2002(2):27-30.(in Chinese)
    [8]
    饶寿期,徐鹤山.航空涡喷、涡扇发动机结构设计准则:第3册 叶片[R].北京:中国航空工业总公司发动机系统工程局,1997.
    [9]
    吕文林,陈俊粤.航空涡喷、涡扇发动机结构设计准则:第2册 轮盘[R].北京:中国航空工业总公司发动机系统工程局,1997.
    [10]
    刘惟信,孟嗣宗.机械最优化设计[M].北京:清华大学出版社,1994.
    [11]
    师访.ANSYS二次开发及应用详解[M].北京:中国水利水电出版社,2012.
    [12]
    莫维尼.有限元分析:ANSYS理论与应用[M].北京:电子工业出版社,2008.
    [13]
    张涛.ANSYS APDL参数化有限元分析技术及其应用实例[M].北京:中国水利水电出版社,2013.
    [14]
    龚曙光,谢桂兰,黄云清.ANSYS参数化编程与命令手册[M].北京:机械工业出版社,2009.
    [15]
    孙全颖.机械优化设计[M].哈尔滨:哈尔滨工业大学出版社,2007.
    [16]
    尹泽勇,欧园霞,任培正,等.航空发动机设计手册:第18册 叶片轮盘及主轴强度分析[M].北京:航空工业出版社,2001.
    [17]
    北京航空材料研究所.航空发动机设计用材料数据手册[M].北京:航空工业出版社,1990.
    [18]
    罗尔斯-罗伊斯公司.EGD-3斯贝Mk202发动机应力标准[S].丁爱祥,吴君,译.北京:国际航空编辑部,1979.
  • 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 (1446) PDF downloads(862) Cited by()
    Proportional views
    Related

    /

    DownLoad:  Full-Size Img  PowerPoint
    Return
    Return