Experiment study on predicting burst speed of disk by modified average stress method
-
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.
-
Key words:
- compressor disk /
- radial burst /
- burst test /
- burst speed /
- modified average stress method
-
[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. 航空涡轮喷气和涡轮风扇发动机通用规范: [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]. 2版 .北京:北京航空航天大学出版社,2014.[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.
点击查看大图
计量
- 文章访问数: 74
- HTML浏览量: 5
- PDF量: 70
- 被引次数: 0