Experiment study on predicting burst speed of disk by modified average stress method

Yanyan CHEN; Shiyong QIN; Haihe SUN; Dasheng WEI; Wenjun DU; Yanlong PANG

doi:10.13224/j.cnki.jasp.20210651

Chinese

您当前的位置：

首页 >

文章列表页 >

Experiment study on predicting burst speed of disk by modified average stress method

Structure,Strength and Vibration | 更新时间：2025-04-07

- Experiment study on predicting burst speed of disk by modified average stress method
- Journal of Aerospace Power Vol. 37, Issue 5, Pages: 954-963(2022)
- 作者机构：
  
  1.中国航空发动机集团有限公司四川燃气涡轮研究院，成都 610500
  2.北京航空航天大学能源与动力工程学院，北京 100191
- 作者简介：
- 基金信息：
- DOI：10.13224/j.cnki.jasp.20210651
  CLC：
- 稿件说明：
移动端阅览
Yanyan CHEN, Shiyong QIN, Haihe SUN, et al. Experiment study on predicting burst speed of disk by modified average stress method[J]. Journal of Aerospace Power, 2022, 37(5): 954-963.
DOI：

Yanyan CHEN, Shiyong QIN, Haihe SUN, et al. Experiment study on predicting burst speed of disk by modified average stress method[J]. Journal of Aerospace Power, 2022, 37(5): 954-963. DOI： 10.13224/j.cnki.jasp.20210651.

摘要

基于修正平均应力法，分析了TC17钛合金压气机轮盘型面尺寸参数对径向和周向破裂转速的影响，并对破裂模式的转变进行预判。进而设计了针对径向破裂模式的轮盘试验件，并开展了TC17钛合金压气机轮盘的破裂试验。轮盘破裂试验结果与修正平均应力法计算结果吻合较好，计算的破裂转速储备与试验结果的误差由修正前的7.24%下降为修正后的0.72%，可为工程应用提供依据。

Abstract

Based on the modified average stress method，the effects of the profile dimension parameters of TC17 titanium alloy compressor disk on the radial and circumferential burst speed were analyzed，and the transformation of burst mode was predicted.Furthermore，the test disks for radial burst mode were designed，and burst tests of TC17 titanium alloy compressor disk were carried out.The test results of disk burst are in good agreement with the calculated results of the modified average stress method.The error between the calculated burst speed reserve and the test results decreases from 7.24% before correction to 0.72% after correction，which can provide a basis for engineering application.

关键词

Keywords

references

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（研究报告）第二册：轮盘 [R]. 北京 : 中国航空工业总公司发动机系统工程局 , 1997 .

中国人民解放军总装备部 . 航空涡轮喷气和涡轮风扇发动机通用规范 : GJB 241A⁃2010 [S]. 北京 : 总装备部军标出版发行部 , 2010 : 26 .

Department of Defense . Engine structural integrity program （ENSIP） [M]. Washington,US : United States Airforce , 2004 .

陈光 . 航空发动机结构设计分析 [M]. 2版 . 北京 : 北京航空航天大学出版社 , 2014 .

BHAUMIK S K , BHASKARAN T A , RANGARAJU R , et al . Failure of turbine rotor blisk of an aircraft engine [J]. Engineering Failure Analysis , 2002 , 9 （ 3 ）: 287 ⁃ 301 .

ROBINSON E L . Bursting tests of steam‑turbine disk wheels [J]. Transaction of American Society of Mechanical Engineers ， 1944 , 66 （ 5 ）: 373 ⁃ 386 .

HOLMS A G , JENKINS J E . Effect of strength and ductility on burst characteristics of rotating disks [R]. Washington,US : National Advisory Committee for Aeronautics , 1948 .

PERCY M J , BALL K , MELLOR P B . An experimental study of the burst strength of rotating disks [J]. International Journal of Mechanical Sciences , 1974 , 16 （ 11 ）: 809 ⁃ 817 .

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 .

WAN Jiangyan , ZHOU Baizhuo . Elastic⁃plastic disc burst criteria establishment and variable thickness disk burst rotational speed prediction [J]. Aeroengine , 2011 , 37 （ 5 ）: 4 ⁃ 6 . （in Chinese）

NOZHNITSKY Y A , SERVETNIK A N . Prevention of hazardous failure of the turbine rotor due to its overspeed [J]. IOP Conference Series:Materials Science and Engineering , 2018 , 449 （ 1 ）: 012025.1 ⁃ 012025.10 .

WILTERDINK P I , HOLMS A G , Manson S S . A theoretical and experimental investigation of the influence of temperature gradients on the deformation and burst speeds of rotating disks [R]. Washington,US : National Advisory Committee for Aeronautics , 1952 .

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 .

FENG Yinli , WU Changbo , GAO Peng , et al . Analysis of power metallurgy superalloy turbine disc's burst speed [J]. Journal of Aerospace Power , 2013 , 28 （ 3 ）: 501 ⁃ 506 . （in Chinese）

MACALUSO S B , KELLER R B . Liquid rocket engine turbines [R]. NASA SP⁃8110 , 1974 .

BARACK W N , DOMAS P A . An improved turbine disk design to increase reliability of aircraft jet engines [R]. NASA CR⁃135033 , 1976 .

MANAVI B . Centrifugal rotor tri⁃hub burst for containment system validation [R]. Barcelona,Spain:ASME Turbo Expo:Power for Land,Sea and Air , 2006 .

KUMAR R , RANJAN V , KUMAR B , et al . Finite element modelling and analysis of the burst margin of a gas turbine disc using an area weighted mean hoop stress method [J]. Engineering Failure Analysis , 2018 , 90 : 425 ⁃ 433 .

比尔格尔 И А , 绍尔 Б Ф , 约西列维奇 Г Б . 机械零件强度计算手册 [M].姚兆生，译. 北京 : 机械工业出版社 , 1979 .

KASLJEVIC K . Correlation of numerical simulation methods and failure criteria to experimental burst test [D]. Lund,Sweden : Lund University , 2020 .

冯引利 , 何云 , 陈伟 , 等 . 轮盘径向破裂转速计算方法分析及修正 [J]. 航空动力学报 , 2014 , 29 （ 11 ）: 2729 ⁃ 2734 .

FENG Yinli , HE Yun , CHEN Wei , et al . Analysis and correction of computational methods on disk radial burst speed [J]. Journal of Aerospace Power , 2014 , 29 （ 11 ）: 2729 ⁃ 2734 . （in Chinese）

宋兆泓 , 熊昌炳 , 郑光华 . 航空燃气涡轮发动机强度设计 [M]. 北京 : 北京航空航天大学 , 2008 .

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 .

DHONDT G , KOHL M . The effect of the geometry and the load level on the dynamic failure of rotating disks [J]. International Journal of Solids and Structures , 1999 , 36 （ 6 ）: 789 ⁃ 812 .

Views

下载量

CSCD

Alert me when the article has been cited

提交

Tools

Publicity Resources

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

Prediction of hoop mode burst speed of disk considering local stress effect

Analysis of crack propagation for a compressor disk with cracks on pin holes

Analysis of power metallurgy superalloy turbine disc's burst speed

基于自适应MOMEDA滚动轴承故障特征提取方法

Related Author

Mengdi MA

Yanrong WANG

Di LI

Hui ZHANG

Dasheng WEI

HU Qingqing

LIAO Mingfu

LIU Yang

Related Institution

Jiangxi Research institute，Beihang University

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

School of Power and Energy,Northwestern Polytechnical University

Hunan Aviation Powerplant Research Institute, Aero Engine Corporation of China

Institute of Process Equipment, Zhejiang University

AI问答

Postal code：100079
Tel：（010）53879206 Email：tmw@bjxintong.com.cn
Technical support is provided by Beijing Founder electronics co., LTD 京ICP备09082226号-64 京公网安备11010602201714号
It is recommended to read the content of this site in Chrome&IE9+. Please switch to extreme mode in browser 360.
Cookies We use cookies to help provide and enhance our service and tailor content. By continuing, you agree to the use of cookies.

⁰