Volume 37 Issue 4
Apr.  2022
Turn off MathJax
Article Contents
Article Navigation >  Journal of Aerospace Power  > 2022  >  37(4): 704-710
WEI Dasheng, MA Mengdi, WANG Yanrong, LI Di, ZHANG Hui. Prediction method and experimental verification of the burst speed of the vortex reducer[J]. Journal of Aerospace Power, 2022, 37(4): 704-710. doi: 10.13224/j.cnki.jasp.20210100
Citation: WEI Dasheng, MA Mengdi, WANG Yanrong, LI Di, ZHANG Hui. Prediction method and experimental verification of the burst speed of the vortex reducer[J]. Journal of Aerospace Power, 2022, 37(4): 704-710. doi: 10.13224/j.cnki.jasp.20210100
shu

Prediction method and experimental verification of the burst speed of the vortex reducer

doi: 10.13224/j.cnki.jasp.20210100
  • 1.

    School of Energy and Power Engineering，Beihang University，Beijing 100191，China

  • 2.

    Jiangxi Research institute，Beihang University，Nanchang 330096，China

  • 3.

    Research and Development Center，Commercial Aircraft Engine Company Limited，Aero Engine Corporation of China，Shanghai 200241，China

  • Received Date: 2021-03-07
  • Publish Date: 2022-04-28
    Abstract
  • The problem of the burst speed of vortex reducer was studied by numerical analysis combined with experiment.According to the stress state of vortex reducer，the simulative specimen was designed，and the failure experiments under the monotonic tensile load were carried out.The failure parameters reflecting the structural stress characteristics were obtained.Furthermore，based on the finite element method，the failure parameters of the simulative specimen were introduced into burst speed prediction of vortex reducer and the influences of different failure criterion on the burst speed prediction were compared.The analysis showed that the stress gradient of simulative specimen was in good agreement with structure，which can accurately describe the structural stress characteristics.Burst speeds calculated by the methods of local plasticity and based on tensile strength of materials were more conservative，which were 15% and 23% lower than those predicted by average stress method，respectively.The method developed has engineering reference value for the failure analysis of structures.

     

    • FullText(HTML)
  • loading
    • References(20)
  • [1]
    NEGULESCU D,PFITZNER M.Secondary air systems in aeroengines employing vortex reducers[C]∥Proceedings of the ASME Turbo Expo:Power for Land,Sea,& Air.New Orleans，US:ASME,2001:1-10.
    [2]
    PFITZNER M,WASCHKA W.Development of an aero engine secondary air system employing vortex reducers[C]∥Proceedings of the 22nd ICAS Congress.Harogate，UK:International Congress of Aeronautical Sciences (ICAS),2000:511.1-511.10.
    [3]
    PEITSCH D,STEIN M,HEIN S,et al.Numerical investigation of vortex reducer flows in the high pressure compressor of modern aeroengines[C]∥Proceedings of the ASME Turbo Expo :Power for Land,Sea,and Air.Amsterdam:ASME,2002:1125-1134.
    [4]
    《航空发动机设计手册》编委会.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,2001:247-253.
    [5]
    吕文林,陈俊粤,田德义,等.航空涡喷、涡扇发动机结构设计准则：第二册[M].北京:中国航空工业总公司发动机系统工程局,1997:264-269.
    [6]
    洪其麟,王屏.计算轮盘破裂转速的大变形解析法[J].航空动力学报,1990,5（4）:321-324.
    [7]
    孙国维.几种材料和结构的轮盘转子破裂准则的试验应用[J].热能动力工程.1988,3（3）:30-35.
    [8]
    REDDY T Y,SRINATH H.Elastic stresses in a rotating anisotropic annular disk of variable thickness and variable density[J].International Journal of Mechanical Sciences.1974,16（2）:85-89.
    [9]
    GUVEN U.Elastic plastic stress in a rotating annular disk of variable thickness and variable density[J].International Journal of Mechanical Sciences.1992,34（2）:133-138.
    [10]
    ERASLAN A N,ORCAN Y.On the rotating elastic-plastic solid disks of variable thickness having concave profiles[J].International Journal of Mechanical Sciences.2002,44（7）:1445-1466.
    [11]
    SQUARCELLA N,FIRRONE C M,ALLARA M,et al.The importance of the material properties on the burst speed of turbine disks for aeronautical applications[J].International Journal of Mechanical Sciences.2014,84:73-83.
    [12]
    万江艳,周柏卓.轮盘弹塑性盘破裂准则的建立及变厚度轮盘破裂转速预测[J].航空发动机,2011,37（5）:4-6.
    [13]
    孙力,胡绪腾,宋迎东.基于连续损伤力学的轮盘超转破裂行为预测与验证[J].航空发动机.2018,44（4）:39-44.
    [14]
    蔡全卓.典型航空发动机轮盘破裂失效研究[D].杭州:浙江大学,2017.
    [15]
    胡清清.基于失效模式的轮盘破裂转速预测方法研究[D].杭州:浙江大学,2020.
    [16]
    王浩然.航空发动机轮盘破裂分析方法研究与应用.[D].南京:南京航空航天大学,2016.
    [17]
    冯引利,吴长波,高鹏,等.某粉末冶金高温合金涡轮盘破裂转速分析[J].航空动力学报,2013,28（3）:501-506.
    [18]
    秦仕勇,冯引利,孙海鹤,等.粉末冶金涡轮盘破裂转速分析与验证[J].燃气涡轮试验与研究,2017,30（5）:36-41.
    [19]
    邵帅,刘秀芝,魏峰,等.某低压涡轮盘破裂转速分析与试验验证[J].航空发动机,2019,45（2）:19-22.
    [20]
    《航空发动机设计用材料数据手册》编委会.航空发动机设计用材料数据手册:第三册[M].北京:航空工业出版社,2008:368-386.
    • Relative Articles
    • 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(1195.0KB)
    XML

    Article Metrics

    Article views (399) PDF downloads(150) Cited by()
    Proportional views
    Related

    Copyright © 《Journal of Aerospace Power》 All Rights Reserved.

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

    /

    DownLoad:  Full-Size Img  PowerPoint
    Return
    Return