scholarly journals Effects of laser peening on the fatigue strength and defect tolerance of aluminum alloy

2020 ◽  
Vol 43 (4) ◽  
pp. 845-856 ◽  
Author(s):  
Koji Takahashi ◽  
Yuta Kogishi ◽  
Norihito Shibuya ◽  
Fumiaki Kumeno
2008 ◽  
Vol 2008 (0) ◽  
pp. _OS1507-1_-_OS1507-2_
Author(s):  
Yuji SUZUKI ◽  
Yasuo OCHI ◽  
Takashi MATSUMURA ◽  
Toshihumi KAKIUCHI ◽  
Kiyotaka MASAKI ◽  
...  

2010 ◽  
Vol 59 (12) ◽  
pp. 932-937 ◽  
Author(s):  
Yasuo OCHI ◽  
Takashi MATSUMURA ◽  
Takaaki IKARASHI ◽  
Kiyotaka MASAKI ◽  
Toshifumi KAKIUCHI ◽  
...  

2019 ◽  
Vol 2019 (0) ◽  
pp. J40107P
Author(s):  
Yuta KOGISHI ◽  
Koji TAKAHASHI ◽  
Rie SUMIYA ◽  
Itaru CHIDA

2014 ◽  
Vol 891-892 ◽  
pp. 969-973 ◽  
Author(s):  
Yuji Sano ◽  
Kiyotaka Masaki ◽  
Keiichi Hirota

Plane bending fatigue testing was performed to study the fatigue properties of friction stir welded (FSW) 3 mm thick AA6061-T6 aluminum alloy plates. Fatigue cracks propagated with bends and curves on the specimens, showing large deviation from a linear line. This might be reflecting the material flow and microstructure in the weld zone. The fatigue strength of the unwelded base material (BM) was 110 MPa at 107 cycles and FSW deteriorated it to 90 MPa. However, laser peening (LP) restored the degraded fatigue strength up to 120 MPa which is higher than that of the BM.


2016 ◽  
Vol 109 (21) ◽  
pp. 211902 ◽  
Author(s):  
E. I. Ageev ◽  
V. Yu. Bychenkov ◽  
A. A. Ionin ◽  
S. I. Kudryashov ◽  
A. A. Petrov ◽  
...  

2011 ◽  
Vol 29 (3) ◽  
pp. 146-153 ◽  
Author(s):  
Yoshihiro SAKINO ◽  
Yuji SANO ◽  
Rie SUMIYA ◽  
You-Chul KIM

2013 ◽  
Vol 456 ◽  
pp. 451-455
Author(s):  
Jun Yang ◽  
Bo Li ◽  
Qiang Jia ◽  
Yuan Xing Li ◽  
Ming Yue Zhang ◽  
...  

Fatigue test of the welded joint of 5083 aluminum alloy with smooth and height of specimen and the weld zone than the high test measurement and theoretical stress concentration coefficient calculation, the weld reinforcement effect of stress concentration on the fatigue performance of welded joints. The results show that: Smooth tensile strength of specimens for 264MPa, fatigue strength is 95MPa, the tensile strength of the 36%. Higher tensile strength of specimens for 320MPa, fatigue strength is 70MPa, the tensile strength of the 22%. Higher specimen stress concentration coefficient is 1.64, the stress concentration to the weld toe becomes fatigue initiation source, and reduces the fatigue strength and the fatigue life of welded joints.


2020 ◽  
Vol 1666 ◽  
pp. 012019
Author(s):  
K Zakharchenko ◽  
V Kapustin ◽  
I Zverkov ◽  
M Legan ◽  
A Larichkin ◽  
...  

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