304不锈钢钎焊板翅结构疲劳断裂机理分析  

Analysis of fatigue fracture mechanism for brazed 304 stainless steel plate-fin structure

作　　者：蒋文春[1,2] 巩建鸣[2] 涂善东[2] 

机构地区：[1]中国石油大学(华东)机电工程学院,山东东营257061 [2]南京工业大学机械与动力工程学院,南京210009

出　　处：《焊接学报》2010年第4期45-48,96,共5页Transactions of The China Welding Institution

基　　金：国家自然科学基金资助项目(10472043);江苏省普通高校研究生科研创新计划(2007);中国石油大学(华东)引进人才(博士)科研基金(2009)

摘　　要：对304不锈钢板翅结构进行疲劳试验,分析疲劳断裂机理.疲劳裂纹从上钎角萌生,然后向翅片扩展,最终导致失效.在钎焊过程中,钎角处生成了较多的脆性化合物,且钎角处应力高度集中,使得裂纹从钎角萌生.疲劳裂纹的扩展经历了4个阶段:(1)裂纹在循环载荷作用下,在钎角脆性化合物启裂;(2)裂纹启裂后,在循环载荷作用下,沿钎角扩展;(3)裂纹跨越钎角和固溶体组织的界面,沿固溶体组织扩展;(4)裂纹跨越翅片和固溶体的界面,进入翅片区域扩展,直至完全断裂.The fatigue tests were carried out to a 304 stainless steel plate-fin structure,and the fatigue fracture mechanism was analyzed.The crack is initiated at the top fillet,and then it propagates to the fin until failure.During the brazing,some brittle phases are generated in the fillet where the stresses are concentrated,which result in the initiation of crack at the fillet.The fatigue crack propagation is composed of four stages.The first stage is the crack initiation around the brittle phases at the fillet under the cyclic loading.The second stage is the crack propagation in the fillet metal.The third stage is that the crack crosses the interface between filler metal and solid solution and then propagates along the solid solution.The fourth stage is that the crack crosses the interface between solid solution and fin,and then it propagates along the fin until the failure.

关 键 词：不锈钢板翅结构 疲劳 失效机理 

分 类 号：TG405[金属学及工艺—焊接]