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钛合金焊接件疲劳特性评估的当量Kt法
引用本文:王向明,刘文珽,王忠波.钛合金焊接件疲劳特性评估的当量Kt法[J].北京航空航天大学学报,2002,28(1):102-104.
作者姓名:王向明  刘文珽  王忠波
作者单位:北京航空航天大学 飞行器设计与应用力学系
摘    要:针对先进飞机结构广泛采用的钛合金焊接结构,提出了描述焊接件疲劳特性的当量理论应力集中系数Kt(Kte)的概念;建立了以钛合金材料疲劳性能为基础,通过一组谱载下钛合金焊接件疲劳试验来确定Kte的技术途径.以TC4钛合金氧弧焊试件为例给出了确定Kte的具体方法和结果.

关 键 词:钛合金  疲劳  应力集中  焊接件
文章编号:1001-5965(2002)01-0102-03
收稿时间:2000-07-11
修稿时间:2000年7月11日

Equivalent Kt Method for Evaluating Fatigue Properties of Titanium Alloy Welding Specimens
WANG Xiang,ming,LIU Wen,ting,WANG Zhong,bo.Equivalent Kt Method for Evaluating Fatigue Properties of Titanium Alloy Welding Specimens[J].Journal of Beijing University of Aeronautics and Astronautics,2002,28(1):102-104.
Authors:WANG Xiang  ming  LIU Wen  ting  WANG Zhong  bo
Institution:Beijing University of Aeronautics and Astronautics, Dept. of Flight Vehicle Design and Applied Mechanics
Abstract:With regard to the Titanium alloy welding structures generally used in advanced aircraft structures,an equivalent theoretical stress concentration coefficient K t (K te ) was introduced to describe the fatigue property of welding specimen. On the basis of the fatigue properties of Titanium alloy specimens,a technological approach used to determine K te is established through fatigue testing for the Titanium alloy welding specimen under a spectrum load. The detailed process determining K te and some useful results are given by taking the TC4 titanium alloy oxy arc welding specimen for example.
Keywords:Titanium alloys  fatigue  stresses  welding specimenfficient  
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