2004
DOI: 10.2320/matertrans.45.419
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Fatigue of Welded Magnesium Alloy Joints

Abstract: Fatigue tests were carried out on welded joints of commercial AZ31 alloy and AZ61 alloy in air as welded surface condition. Alloys were extruded or rolled to a plate shape. Pairs of the same type of alloy plates were butt-welded by tungsten inert gas (TIG) welding or friction stir welding (FSW). All welded joints except FSW-ed AZ61 have joint efficiency of around 90% for static tensile strength. Extruded AZ31 alloy joints by TIG or FSW showed fatigue joint efficiency of about 80%. However, fatigue joint effici… Show more

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Cited by 32 publications
(8 citation statements)
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“…Similar results were found with various aluminum alloys including 6013, 2014 and 7475 [50,51]. It is noted that other factors also affect sample fatigue life, especially any residual stress, the microstructure, and presence of defects which must also be accounted for when making fatigue life comparisons [53,54].…”
Section: Fatiguesupporting
confidence: 77%
“…Similar results were found with various aluminum alloys including 6013, 2014 and 7475 [50,51]. It is noted that other factors also affect sample fatigue life, especially any residual stress, the microstructure, and presence of defects which must also be accounted for when making fatigue life comparisons [53,54].…”
Section: Fatiguesupporting
confidence: 77%
“…Its specific strength is 175-223 MPa/(g/cm 3 ). These values easily exceed the value 125 of heat treated aluminum alloy A6061-T6, and 150 of conventional magnesium alloy extruded AZ31 (Mg-3 mass%Zn-1 mass%Al alloy), 4) and heat treated aluminum alloy A6061 5) and are almost comparable to the value 235 MPa/(g/cm 3 ) of heat-treated strong aluminum alloy A7075-T6. 6) It is now near at hand that the alloy will be put to practical use.…”
Section: Introductionmentioning
confidence: 90%
“…[5][6][7] Many researchers have investigated the fatigue behavior of wrought magnesium alloys. [8][9][10][11][12][13][14][15][16][17][18][19] The reports show the crack initiation and/or propagation mechanisms [9][10][11][12] and the effect of microstructures such as grain size 12,13) and texture 14,15) on fatigue strength. Fatigue property is often evaluated with a stress ratio of R ¼ 0:1 or À1 during the cyclic-uniaxial test.…”
Section: Introductionmentioning
confidence: 99%