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带CFRP箍环整体叶盘强度和寿命分析及试验
引用本文:王卫国,古远兴,黄庆东,胡仁高,温卫东.带CFRP箍环整体叶盘强度和寿命分析及试验[J].推进技术,2006,27(5):441-444.
作者姓名:王卫国  古远兴  黄庆东  胡仁高  温卫东
作者单位:1. 南京航空航天大学,能源与动力学院,江苏,南京,210016;中国燃气涡轮研究院,四川,成都,610500
2. 中国燃气涡轮研究院,四川,成都,610500
3. 南京航空航天大学,能源与动力学院,江苏,南京,210016
基金项目:国防科学技术工业委员会国防科学技术三等奖.
摘    要:1引言随着叶轮机叶尖切线速度的日益提高,传统转子材料和结构的使用已经达到了极限。带碳纤维增强复合材料(CFRP)箍环整体叶盘(blisk)结构是上世纪90年代国外在风扇转子设计中采用的一种新型结构形式1,2],其特点是在整体叶盘叶尖位置有金属外环,在外环上带有CFRP箍环,叶片的部

关 键 词:整体叶盘结构~    碳纤维增强复合材料~    强度  疲劳寿命
文章编号:1001-4055(2006)05-0441-04
收稿时间:2005-09-05
修稿时间:2006-05-15

Numerical analysis and experiment on the strength and life of the blisk with CFRP ring
WANG Wei-guo,GU Yuan-xing,HUANG Qing-dong,HU Ren-gao and WEN Wei-dong.Numerical analysis and experiment on the strength and life of the blisk with CFRP ring[J].Journal of Propulsion Technology,2006,27(5):441-444.
Authors:WANG Wei-guo  GU Yuan-xing  HUANG Qing-dong  HU Ren-gao and WEN Wei-dong
Institution:Coll.of Energy and Power,Nanjing Univ.of Aeronautics & Astronautics,Nanjing 210016,China;China Gas Turbine Establishment,Chengdu 610500,China;China Gas Turbine Establishment,Chengdu 610500,China;China Gas Turbine Establishment,Chengdu 610500,China;China Gas Turbine Establishment,Chengdu 610500,China;Coll.of Energy and Power,Nanjing Univ.of Aeronautics & Astronautics,Nanjing 210016,China
Abstract:Numerical analysis and experimental investigation were carried out to study the strength and low cycle fatigue life of the BLISK with carbon fiber reinforced plastics(CFRP) ring.Firstly,based on the mechanical behavior analysis and properties test of CFRP,the numerical analysis on the stress-strain,vibration modal and LCF life of the BLISK with CFRP ring were presented.Secondly,strain measure,modal test and LCF spin test were performed successfully.Finally,the comparison of the numerical results with the experimental data shows good consistency.
Keywords:Blisk structure  Carbon fiber reinforced plastics  Strength  Fatigue life
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