首页 | 本学科首页   官方微博 | 高级检索  
     检索      

涡轮盘多轴低循环疲劳寿命预测及试验验证
引用本文:杨俊,李承彬,谢寿生.涡轮盘多轴低循环疲劳寿命预测及试验验证[J].航空动力学报,2011,26(10):2220-2226.
作者姓名:杨俊  李承彬  谢寿生
作者单位:1. 中国人民解放军空军西安局某军事代表室,西安710021/空军工程大学工程学院,西安710051
2. 中国航空工业集团公司西安航空发动机(集团)有限公司,西安,710021
3. 空军工程大学工程学院,西安,710051
基金项目:总装关于某型发动机综合整治科研项目(10116-2004); 西航集团“十一五”可靠性科研项目(XAEC-JPS-JHB-1005-0031)
摘    要:应用单轴及多轴疲劳寿命预测的Von Mises等效应变模型和临界平面模型对某两级涡轮盘传动臂销钉孔的疲劳寿命进行预测.组装和调试了全尺寸两级涡轮盘联合试验件,在旋转试验器上完成了低循环疲劳试验,得到两级涡轮盘传动臂销钉孔试验失效寿命.预测寿命与试验寿命对比分析显示单轴和VonMises等效应变模型预测误差较大;临界平面...

关 键 词:涡轮盘  多轴低循环疲劳  临界平面  寿命预测  SWT(Smith-Watson-Topper)模型  Von  Mises等效应变模型
收稿时间:2010/11/5 0:00:00
修稿时间:4/4/2011 12:00:00 AM

Multiaxial low cycle fatigue life prediction and test verification for turbine disk
YANG Jun,LI Cheng-bin and XIE Shou-sheng.Multiaxial low cycle fatigue life prediction and test verification for turbine disk[J].Journal of Aerospace Power,2011,26(10):2220-2226.
Authors:YANG Jun  LI Cheng-bin and XIE Shou-sheng
Institution:A Military Representative Office, Airforce Xi'an Bureau, The Chinese People's Liberation Army, Xi'an 710021, China;The Engineering Institute, Air Force Engineering University, Xi'an 710051, China;Xi'an Aero-engine (Group) Corporation Limited, Aviation Industry Corporation of China, Xi'an 710021, China;The Engineering Institute, Air Force Engineering University, Xi'an 710051, China
Abstract:The fatigue life of a two-stage turbine disk transmission arm pin hole was predicted by the models of uniaxial,Von Mises strain and critical plane.A full-scale two-stage turbine disk was fabricated and debugged,and then tested for LCF(low cycle fatigue).The predicted life was compared with the life evaluated by fatigue test of real turbine disk,and the result shows that the predicted errors of the critical plane model are less than those of the uniaxial model and the Von Mises strain model,especially the error of SWT(Smith-Watson-Topper)model is 9.26%.
Keywords:turbine disk  multiaxial low cycle fatigue  critical plane  life prediction  SWT(Smith-Watson-Topper) model  Von Mises strain model
本文献已被 CNKI 万方数据 等数据库收录!
点击此处可从《航空动力学报》浏览原始摘要信息
点击此处可从《航空动力学报》下载免费的PDF全文
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号