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预腐蚀典型铆接结构疲劳寿命特性研究
引用本文:任三元,曹鹏钧,刘海涛.预腐蚀典型铆接结构疲劳寿命特性研究[J].装备环境工程,2009,6(1):27-29.
作者姓名:任三元  曹鹏钧  刘海涛
作者单位:1. 中国航空工业第六○五研究所,湖北 荆门,448035
2. 海装航空装备科研订货部,北京,100841
摘    要:通过设计LY12-CZ材料的典型铆接结构试验件与模拟现役飞机的地面停放环境,完成加速试验环境谱下的预腐蚀试验与不同时间预腐蚀后试验件的等幅疲劳试验,最终获得预腐蚀典型铆接结构疲劳寿命特性与疲劳寿命的影响系数C(t)曲线。

关 键 词:预腐蚀  疲劳寿命  C(t)曲线

Research on Fatigue Life Characteristics of Pre-corroded Typical Riveted Structure
REN San-yuan,CAO Peng-jun,LIU Hai-tao.Research on Fatigue Life Characteristics of Pre-corroded Typical Riveted Structure[J].Equipment Environmental Engineering,2009,6(1):27-29.
Authors:REN San-yuan  CAO Peng-jun  LIU Hai-tao
Affiliation:1.No.605 Institute of China Aviation Industry Corporation;Jingmen 448035;China;2.Naval Aviation Scientific Research Equipment Procurement Department;Beijing 1000841;China
Abstract:Typical riveted structure samples were designed and the ground parking environment of aircraft on-service was simulated.Pre-corrosion test under accelerated corrosion test environment spectra and constant-amplitude fatigue test after different corrosion time were carried out.Finally,the fatigue life characteristics on pre-corroded typical riveted structure was obtained,and the effect coefficient C(t) curve of ground parking corrosion to fatigue life was established.
Keywords:fatigue life  pre corrosion  C(t) curve
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