留言板

尊敬的读者、作者、审稿人, 关于本刊的投稿、审稿、编辑和出版的任何问题, 您可以本页添加留言。我们将尽快给您答复。谢谢您的支持!

姓名
邮箱
手机号码
标题
留言内容
验证码

整体叶盘叶片焊缝裂纹相控阵超声检测

马立印 李洋 周正干

马立印, 李洋, 周正干等 . 整体叶盘叶片焊缝裂纹相控阵超声检测[J]. 北京航空航天大学学报, 2017, 43(9): 1900-1908. doi: 10.13700/j.bh.1001-5965.2016.0683
引用本文: 马立印, 李洋, 周正干等 . 整体叶盘叶片焊缝裂纹相控阵超声检测[J]. 北京航空航天大学学报, 2017, 43(9): 1900-1908. doi: 10.13700/j.bh.1001-5965.2016.0683
MA Liyin, LI Yang, ZHOU Zhengganet al. Detection of welding crack in blisk blade based on ultrasonic phased array[J]. Journal of Beijing University of Aeronautics and Astronautics, 2017, 43(9): 1900-1908. doi: 10.13700/j.bh.1001-5965.2016.0683(in Chinese)
Citation: MA Liyin, LI Yang, ZHOU Zhengganet al. Detection of welding crack in blisk blade based on ultrasonic phased array[J]. Journal of Beijing University of Aeronautics and Astronautics, 2017, 43(9): 1900-1908. doi: 10.13700/j.bh.1001-5965.2016.0683(in Chinese)

整体叶盘叶片焊缝裂纹相控阵超声检测

doi: 10.13700/j.bh.1001-5965.2016.0683
基金项目: 

国家自然科学基金 51375027

工信部民用飞机专项科研项目 MJZ-G-2013-05

详细信息
    作者简介:

    马立印  男, 硕士研究生; 主要研究方向:超声无损检测技术

    周正干  男, 博士, 教授, 博士生导师; 主要研究方向:超声及红外无损检测

    通讯作者:

    周正干, E-mail:zzhenggan@buaa.edu.cn

  • 中图分类号: V250.2;TB553

Detection of welding crack in blisk blade based on ultrasonic phased array

Funds: 

National Natural Science Foundation of China 51375027

Special Research Project of Civil Aircraft of Ministry of Industry and Telecommunications MJZ-G-2013-05

More Information
  • 摘要:

    裂纹是线性摩擦焊整体叶盘结构制造过程中叶片焊缝区域常见的缺陷类型之一。由于叶片焊缝区域结构复杂且裂纹缺陷尺寸小,因此焊缝区域裂纹缺陷的检测难度大。为了满足新工艺的应用要求,研究了焊缝区域的相控阵超声全覆盖检测方法,建立了焊缝区域相控阵超声检测的有限元仿真模型,研究了裂纹特征参数和声束聚焦点位置对检测方案的影响,验证了检测方案的可行性与正确性。构建了机器人化的相控阵超声检测系统,模拟了声束在线性摩擦焊叶片试样中的传播过程,实现了对叶片中预制裂纹缺陷的识别。研究结果表明,设计的检测方案能够满足叶片快速检测的要求。

     

  • 图 1  声压往返透过率

    Figure 1.  Sound pressure reciprocating transmittance

    图 2  楔块设计流程示意图

    Figure 2.  Schematic diagram of wedge design procedure

    图 3  楔块在叶片表面的耦合位置

    Figure 3.  Wedge's coupling position on blade surface

    图 4  有限元仿真计算模型

    Figure 4.  Calculation model of finite element simulation

    图 5  有缺陷和无缺陷模型的信号

    Figure 5.  Signal of models with and without defect

    图 6  裂纹宽度对可检测性影响

    Figure 6.  Influence of crack width on detectability

    图 7  裂纹角度对可检测性影响

    Figure 7.  Influence of crack angle on detectability

    图 8  裂纹深度对可检测性影响

    Figure 8.  Influence of crack depth on detectability

    图 9  聚焦位置对可检测性影响

    Figure 9.  Influence of focal position on detectability

    图 10  线性摩擦焊叶片试样

    Figure 10.  Linear friction welding blade specimen

    图 11  试验装置示意图

    Figure 11.  Schematic diagram of test device

    图 12  位置1检测结果

    Figure 12.  Detection results of position 1

    图 13  位置2检测结果

    Figure 13.  Detection results of position 2

    图 14  位置3检测结果

    Figure 14.  Detection results of position 3

    表  1  试验参数

    Table  1.   Test parameters

    参数 数值
    探头频率/MHz 5
    阵元个数 32
    孔径大小 32
    聚焦深度/mm 10~20
    扫查角度/(°) 40~70
    增益/dB 60
    激励电压/V 400
    注:扫查方式为S扫。
    下载: 导出CSV
  • [1] 刘杰, 郑宁, 徐朋飞, 等.整体叶盘结构叶片弹性变形规律及其对风扇气动性能的影响[J].科学技术与工程, 2014, 14(34):302-306. doi: 10.3969/j.issn.1671-1815.2014.34.058

    LIU J, ZHENG N, XU P F, et al.Blade flexibility deformation pattern of the blisk structure and it's influence on the aerodynamic performance of fan[J].Science Technology and Engineering, 2014, 14(34):302-306(in Chinese). doi: 10.3969/j.issn.1671-1815.2014.34.058
    [2] YANG Y H, LIU D, LUO Z J.Microstructure homogeneity evaluation for TC11 blisk forging using loss function based on Taguchi method[J].Rare Metal Materials and Engineering, 2011, 401(4):565-570. http://www.sciencedirect.com/science/article/pii/S1875537211600258
    [3] KLOCKE F, SCHMITT R, ZEIS M, et al.Technological and economical assessment of alternative process chains for blisk manufacture[J].Procedia CIRP, 2015, 35:67-72. doi: 10.1016/j.procir.2015.08.052
    [4] RAVI-KUMAR B V R.A review on blisk technology[J].International Journal of Innovative Research in Science, Engineering and Technology, 2013, 2(5):1353-1358. http://www.oalib.com/paper/2170964
    [5] 张海燕, 张连锋.航空发动机整体叶盘制造技术国内外发展概述[J].航空制造技术, 2013(23):38-41. doi: 10.3969/j.issn.1671-833X.2013.23.002

    ZHANG H Y, ZHANG L F.Development overview of aeroengine integral blisk and its manufacturing technology at home and abroad[J].Aeronautical Manufacturing Technology, 2013(23):38-41(in Chinese). doi: 10.3969/j.issn.1671-833X.2013.23.002
    [6] 朱瑞峰, 白钢, 苏利龙, 等.线性摩擦焊及其研究应用现状[J].热加工工艺, 2009, 38(9):100-103. http://www.cnki.com.cn/Article/CJFDTOTAL-SJGY200909034.htm

    ZHU R F, BAI G, SU L L, et al.Research and application of linear friction welding[J].Hot Working Technology, 2009, 38(9):100-103(in Chinese). http://www.cnki.com.cn/Article/CJFDTOTAL-SJGY200909034.htm
    [7] 杨剑赟. 钛合金线性摩擦焊塑性流动对焊缝成形影响[D]. 南昌: 南昌航空大学, 2012: 25-30. http://cdmd.cnki.com.cn/Article/CDMD-10406-1012032921.htm

    YANG J Y.The influence of plastic flow on the weld formation of linear friction welding for titanium alloy[D].Nanchang:Nanchang Hangkong University, 2012:25-30(in Chinese). http://cdmd.cnki.com.cn/Article/CDMD-10406-1012032921.htm
    [8] Technical Committee of American Society for Testing and Materials.Standard reference radiographs of investment steel castings for aerospace applications:ASTM E192-2004[S].Philadelphia:ASTM, 2004:1-4. http://cds.cern.ch/record/522508?ln=ja
    [9] 靳世久, 杨晓霞, 陈世利, 等.超声相控阵检测技术的发展及应用[J].电子测量与仪器学报, 2014, 28(9):925-934. http://www.cnki.com.cn/Article/CJFDTOTAL-DZIY201409001.htm

    JIN S J, YANG X X, CHEN S L, et al.Development and application of ultrasonic phased array inspection technology[J].Journal of Electronic Measurement and Instrumentation, 2014, 28(9):925-934(in Chinese). http://www.cnki.com.cn/Article/CJFDTOTAL-DZIY201409001.htm
    [10] KOMURA I, NAGAI S, KASHIWAYA H, et al.Improved ultrasonic testing by phased array technique and its application[J].Nuclear Engineering and Design, 1985, 87:185-191. doi: 10.1016/0029-5493(85)90107-4
    [11] MACNAB A, CAMPBELL M J.Ultrasonic phased arrays for nondestructive testing[J].NDT International, 1987, 6(20):333-337. http://www.sciencedirect.com/science/article/pii/0308912687902902
    [12] 常文爽. 低压汽轮机叶轮轮缘裂纹的超声相控阵检测[D]. 天津: 天津大学, 2012: 25-36. http://cdmd.cnki.com.cn/Article/CDMD-10056-1013039907.htm

    CHANG W S.Ultrasonic phased array testing of cracks in low-pressure turbine disc rim[D].Tianjin:Tianjin University, 2012:25-36(in Chinese). http://cdmd.cnki.com.cn/Article/CDMD-10056-1013039907.htm
    [13] CHARLESWORTH C.Phased array ultrasonic inspection of low-pressure steam turbine rotors-curved axial entry fir tree roots[J].Insight, 2011, 2(53):37-44. http://www.ingentaconnect.com/content/bindt/insight/2011/00000053/00000002/art00004
    [14] 郑辉, 林树青.超声检测[M].2版.北京:中国劳动社会保障出版社, 2008:36-43.

    ZHENG H, LIN S Q.Ultrasonic testing[M].2nd ed.Beijing:China Labour & Social Security Publishing House, 2008:36-43(in Chinese).
    [15] 李家伟, 陈积懋.无损检测手册[M].北京:机械工业出版社, 2002:157-163.

    LI J W, CHEN J M.Nondestructive testing manual[M].Beijing:China Machine Press, 2002:157-163(in Chinese).
    [16] 徐娜, 何方成, 周正干.基于动态孔径聚焦的L型构件相控阵超声检测[J].北京航空航天大学学报, 2015, 41(6):1000-1006. http://bhxb.buaa.edu.cn/CN/abstract/abstract13281.shtml

    XU N, HE F C, ZHOU Z G.Ultrasonic phased array inspection of L-shaped components based on dynamic aperture focusing[J].Journal of Beijing University of Aeronautics and Astronautics, 2015, 41(6):1000-1006(in Chinese). http://bhxb.buaa.edu.cn/CN/abstract/abstract13281.shtml
  • 加载中
图(14) / 表(1)
计量
  • 文章访问数:  929
  • HTML全文浏览量:  107
  • PDF下载量:  683
  • 被引次数: 0
出版历程
  • 收稿日期:  2016-08-24
  • 录用日期:  2016-12-16
  • 网络出版日期:  2017-09-20

目录

    /

    返回文章
    返回
    常见问答