中国航空学报(英文版)2024,Vol.37Issue(1) :345-361.DOI:10.1016/j.cja.2023.10.017

Microstructure,mechanical and fracture properties of friction stir welded 2195 Al-Li alloy joints

Guangda SUN Weizhao SUN Li ZHOU Sanfeng LUO Zili ZHANG Debo LIU Huiqiang WU
中国航空学报(英文版)2024,Vol.37Issue(1) :345-361.DOI:10.1016/j.cja.2023.10.017

Microstructure,mechanical and fracture properties of friction stir welded 2195 Al-Li alloy joints

Guangda SUN 1Weizhao SUN 2Li ZHOU 1Sanfeng LUO 3Zili ZHANG 3Debo LIU 2Huiqiang WU2
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作者信息

  • 1. State Key Laboratory of Advanced Welding and Joining,Harbin Institute of Technology,Harbin 150001,China;Shandong Provincial Key Laboratory of Special Welding Technology,Harbin Institute of Technology(Weihai),Weihai 264209,China
  • 2. Beijing Institute of Astronautical Systems Engineering,Beijing 100076,China
  • 3. Shandong Provincial Key Laboratory of Special Welding Technology,Harbin Institute of Technology(Weihai),Weihai 264209,China
  • 折叠

Abstract

The 8 mm-thick 2195 Al-Li alloy joints were achieved by Friction Stir Welding(FSW).The microstructural evolution,temperature-dependent mechanical properties,and fracture proper-ties were studied.The Ti,δ'/β'and θ'precipitates were observed in the Base Metal(BM)and the Heat Affected Zone(HAZ).Most of the precipitates,except for re-precipitated δ'/β'phases,were dissolved in the Nugget Zone(NZ).The tensile specimens that failed at cryogenic temperatures(-196 ℃)had the maximum Ultimate Tensile Strength(UTS),and the fracture surface showed the inter-granular fracture characteristics.Compared to those at room temperature(25 ℃),the decreasing tensile properties at high temperature(180 ℃)were related to microstructure and strain hardening effects.The NZ presented the optimal fracture toughness,and the Crack Tip Opening Displacement(CTOD)was mutually dominated by microhardness and grain size.Analysis on Fati-gue Crack Growth(FCG)rates indicates that the Thermal-Mechanically Affected Zone(TMAZ)exhibited the most superior fatigue resistance performance at stress intensity range below 17 MPa.m1/2 due to compressive residual stress and the crack closure effect.The fatigue fracture surfaces reveal that the crack propagation zone was characterized by the striations and secondary cracks.Also,inter-granular fracture behavior was responsible for the fastest FCG rates in the NZ.

Key words

Aluminum alloys/Friction stir welding/Microstructural evolution/Mechanical properties/Fracture mechanism

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基金项目

National Key Research and Development Program of China(2020YFA0711101)

National Natural Science Foundation of China(U1837204)

National Natural Science Foundation of China(51974100)

出版年

2024
中国航空学报(英文版)
中国航空学会

中国航空学报(英文版)

CSTPCDEI
影响因子:0.847
ISSN:1000-9361
参考文献量48
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