谭晓明,金平,蔡增杰,王刚,王德.腐蚀损伤对典型铝合金结构疲劳寿命的影响研究[J].装备环境工程,2013,10(6):9-13. TAN Xiao-ming,JIN Ping,CAI Zeng-jie,WANG Gang,WANG De.Relationship between the Corrosion Influencing Factor of Fatigue Life and the Corrosion Damage Size of Aircraft Airframe Critical Structure[J].Equipment Environmental Engineering,2013,10(6):9-13.
腐蚀损伤对典型铝合金结构疲劳寿命的影响研究
Relationship between the Corrosion Influencing Factor of Fatigue Life and the Corrosion Damage Size of Aircraft Airframe Critical Structure
投稿时间:2013-07-11  修订日期:2013-07-28
DOI:10.7643/issn.1672-9242.2013.06.003
中文关键词:  腐蚀影响系数  关键结构  铝合金  疲劳寿命
英文关键词:corrosion influencing factor  critical structure  aluminun alloy  fatigue life
基金项目:
作者单位
谭晓明 海军航空工程学院青岛校区,山东青岛266041 
金平 海军航空工程学院青岛校区,山东青岛266041 
蔡增杰 海军航空工程学院青岛校区,山东青岛266041 
王刚 海军航空工程学院青岛校区,山东青岛266041 
王德 海军航空工程学院青岛校区,山东青岛266041 
AuthorInstitution
TAN Xiao-ming Naval Aeronautical Engineering Academy Qingdao Branch,Qingdao266041,China 
JIN Ping Naval Aeronautical Engineering Academy Qingdao Branch,Qingdao266041,China 
CAI Zeng-jie Naval Aeronautical Engineering Academy Qingdao Branch,Qingdao266041,China 
WANG Gang Naval Aeronautical Engineering Academy Qingdao Branch,Qingdao266041,China 
WANG De Naval Aeronautical Engineering Academy Qingdao Branch,Qingdao266041,China 
摘要点击次数:
全文下载次数:
中文摘要:
      目的 研究严酷服役条件下飞机结构的寿命衰减问题。方法 以飞机关键结构模拟件为研究对象,基于编制的某机场环境加速试验谱进行当量加速腐蚀试验,采用MTS810材料试验系统进行预腐蚀后的疲劳试验。结果通过对试验结果的分析,确定了关键结构疲劳寿命腐蚀影响系数与腐蚀损伤尺寸之间的对应关系。结论 关键结构腐蚀损伤宽度与疲劳寿命腐蚀影响系数相关性最好。
英文摘要:
      Objective To study the effect of service environment on aircraft structure.Methods The critical structure coupons of aircraft airframe were tested, and accelerated corrosion experiment was carried out based on the accelerated corrosion spectrum of a field airport environment. Test of fatigue after pre-corrosion was conducted using MTS810. ResultsThrough analysis of testing results, the relationship was determined, between the corrosion influencing factors of fatigue life and the corrosion damage size of aircraft airframe critical structure. Conclusion The result shows that there is a significant correlation between the corrosion damage width and the corrosion influencing factor of fatigue life of aircraft critical structure.
查看全文  查看/发表评论  下载PDF阅读器
关闭

关于我们 | 联系我们 | 投诉建议 | 隐私保护 | 用户协议

您是第11984041位访问者    渝ICP备15012534号-5

版权所有:《装备环境工程》编辑部 2014 All Rights Reserved

邮编:400039     电话:023-68792835    Email: zbhjgc@163.com

视频号 公众号