| Citation: | CHEN Yanyan, QIN Shiyong, SUN Haihe, WEI Dasheng, DU Wenjun, PANG Yanlong. 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 |
| [1] |
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.
|
| [2] |
中国人民解放军总装备部.
|
| [3] |
GJB 241A-2010[S].北京:总装备部军标出版发行部,2010:26.
|
| [4] |
[3] Department of Defense.Engine structural integrity program (ENSIP)[M].Washington,US:United States Airforce,2004.
|
| [5] |
[4] 陈光.航空发动机结构设计分析[M].
|
| [6] |
[5] 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.
|
| [7] |
[6] ROBINSON E L.Bursting tests of steam-turbine disk wheels[J].Transaction of American Society of Mechanical Engineers,1944,66(5):373-386.
|
| [8] |
[7] 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.
|
| [9] |
[8] 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.
|
| [10] |
[9] 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.
|
| [11] |
[10] 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.
|
| [12] |
[11] 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.
|
| [13] |
[12] 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.
|
| [14] |
[13] MACALUSO S B,KELLER R B.Liquid rocket engine turbines[R].NASA SP-8110,1974.
|
| [15] |
[14] BARACK W N,DOMAS P A.An improved turbine disk design to increase reliability of aircraft jet engines[R].NASA CR-135033,1976.
|
| [16] |
[15] MANAVI B.Centrifugal rotor tri-hub burst for containment system validation[R].Barcelona,Spain:ASME Turbo Expo:Power for Land,Sea and Air,2006.
|
| [17] |
[16] 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.
|
| [18] |
[17] 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.
|
| [19] |
[18] KASLJEVIC K.Correlation of numerical simulation methods and failure criteria to experimental burst test[D].Lund,Sweden:Lund University,2020.
|
| [20] |
[19] 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.
|
| [21] |
[20] 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.
|
| [22] |
[21] 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.
|
| [23] |
[22] 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.
|