金属学报
金屬學報
금속학보
ACTA METALLURGICA SINICA
2009年
10期
1211-1216
,共6页
林三宝%宋建岭%杨春利%马广超
林三寶%宋建嶺%楊春利%馬廣超
림삼보%송건령%양춘리%마엄초
铝合金%不锈钢%钨极氩弧熔-钎焊%界面层%金属间化合物
鋁閤金%不鏽鋼%鎢極氬弧鎔-釬銲%界麵層%金屬間化閤物
려합금%불수강%오겁아호용-천한%계면층%금속간화합물
aluminum alloy%stainless steel%tungsten inert gas welding-brazing%interfacial layer%intermetallic compound
运用OM,SEM和EDS分析了铝合金/不锈钢TIG熔-钎焊接头界面层的结构特征,并通过微压痕和SEM原位拉伸实验测试了其力学性能.研究结果表明:界面处形成了厚度不均一的锯齿状金属间化合物层,厚度为4-9 μm,满足界面层的要求(≤10 μm);界面反应层包括两类化合物层,即焊缝一侧的τ_5层和钢基体一侧θ+η+τ_5层,在界面处首先形成τ_5相,抑制了粗大枝晶状θ+η二元相的生长.微压痕测试得出:τ_5层平均硬度值为HV1025,θ+η+τ_5层硬度值为HV835.τ_5层压痕处产生裂纹,表明τ_5相是一种硬脆相.SEM原位拉伸实验显示,界面层起裂于θ+η相,在外力作用下沿θ+η+τ_5层迅速开裂,界面层抗拉强度达到120 MPa.
運用OM,SEM和EDS分析瞭鋁閤金/不鏽鋼TIG鎔-釬銲接頭界麵層的結構特徵,併通過微壓痕和SEM原位拉伸實驗測試瞭其力學性能.研究結果錶明:界麵處形成瞭厚度不均一的鋸齒狀金屬間化閤物層,厚度為4-9 μm,滿足界麵層的要求(≤10 μm);界麵反應層包括兩類化閤物層,即銲縫一側的τ_5層和鋼基體一側θ+η+τ_5層,在界麵處首先形成τ_5相,抑製瞭粗大枝晶狀θ+η二元相的生長.微壓痕測試得齣:τ_5層平均硬度值為HV1025,θ+η+τ_5層硬度值為HV835.τ_5層壓痕處產生裂紋,錶明τ_5相是一種硬脆相.SEM原位拉伸實驗顯示,界麵層起裂于θ+η相,在外力作用下沿θ+η+τ_5層迅速開裂,界麵層抗拉彊度達到120 MPa.
운용OM,SEM화EDS분석료려합금/불수강TIG용-천한접두계면층적결구특정,병통과미압흔화SEM원위랍신실험측시료기역학성능.연구결과표명:계면처형성료후도불균일적거치상금속간화합물층,후도위4-9 μm,만족계면층적요구(≤10 μm);계면반응층포괄량류화합물층,즉한봉일측적τ_5층화강기체일측θ+η+τ_5층,재계면처수선형성τ_5상,억제료조대지정상θ+η이원상적생장.미압흔측시득출:τ_5층평균경도치위HV1025,θ+η+τ_5층경도치위HV835.τ_5층압흔처산생렬문,표명τ_5상시일충경취상.SEM원위랍신실험현시,계면층기렬우θ+η상,재외력작용하연θ+η+τ_5층신속개렬,계면층항랍강도체도120 MPa.
Against the background of the required weight reduction in transportation through lightweight construction, the application of hybrid structures, where aluminum alloy and steel are jointed together, has a high technical and economical potential. But jointing of material combinations of aluminum alloy and steel is problematic by fusion welding since brittle intermetallic compounds (IMCs) are formed between aluminum alloy and steel. Nowadays, tungsten inert gas (TIG) welding-brazing offers a great potential for aluminum alloy and steel jointing. In this process, the sheet and filler metal are heated or melted by TIG heat, and the joint has a dual characteristic: in aluminum alloy side it is a welding joint, while in steel side it is a brazing joint. However, in the dynamic heating process, the heating temperature changes so quickly and the reaction time between the liquid filler metal and solid steel is so short that it is more difficult to control the IMC layer's growth, predominantly its thickness and microstructures. Most of past reports about the brazing of aluminum alloy and steel indicate Al-Fe binary IMC layers, e.g., Fe_2Al_5 and FeAl_3, formed in the brazing joint, which are detrimental to the mechanical properties of the joint. Si additions are used to limit the growth of the brittle Al-Fe IMC layer between aluminum alloy and steel by replacing Al-Fe phases with less detrimental Al-Fe-Si phases in aluminizing and furnace brazing of aluminum alloy and steel. By now, there have been few reports of investigating the interfacial layer of TIG welding-brazing joint of aluminum alloy and stainless steel. In this paper, a butt TIG welding-brazing joint of aluminum alloy/stainless steel was formed using Al-Si eutectic filler wire with modified Noclock flux precoated on a steel surface. The microstructure characteristics of the welded seam-steel interfacial layer were analyzed by OM, SEM and EDS and its mechanical properties were measured by dynamic ultra-microhardness tester and SEM in situ tensile tester. The results show that a nonuniform and sawtooth IMC layer forms at the seam-steel interface and its thickness changes from 4 to 9 μm, less than the maximum permissible value (about 10 μm). The interfacial layer is composed of two types of IMC layers, which are τ_5 IMC layer on the seam side and θ+η+τ_5 IMC layer on the steel side.τ_5 phase forms preceding θ+η+τ_5 due to its lower growth energy than Al-Fe phases and the primary τ_5 layer inhibits the growth of rough dendritic θ+η phases. The ultra-microhardness test results show the microhardnesses of τ_5 and θ+η+τ_5 layers reach HV1025 and HV835, respectively. Indentation cracking of τ_5 layer at higher loads indicates that τ_5 is a type of hard brittle phase. SEM in situ tensile test results confirm that cracking initiates from θ+η phases and then fracture rapidly generates along θ+η+τ_5 layer while suffering external force. The tensile strength of IMC layer reaches 120 MPa.