Tensile and Fracture Properties of Aluminium Alloy AA2219-T87 Friction Stir Weld Joints for Aerospace Applications

2021 ◽  
Author(s):  
P. Manikandan ◽  
T. Antony Prabhu ◽  
Sushant K. Manwatkar ◽  
G. Sudarshan Rao ◽  
S. V. S. Narayana Murty ◽  
...  
Keyword(s):  
Aluminium Alloy ◽  
Friction Stir Weld ◽  
Fracture Properties ◽  
Friction Stir ◽  
Weld Joints ◽  
Aerospace Applications

Influence of heat treatment on the tensile and hardness characteristics of friction stir weld joints of dissimilar aluminium alloys

2022 ◽  
Author(s):  
K. Ramesha ◽  
P. D. Sudersanan ◽  
Prem Kumar Mahto ◽  
Shaikh Mohammed Ismail ◽  
Ashwin C. Gowda ◽  
...  
Keyword(s):  
Heat Treatment ◽  
Aluminium Alloys ◽  
Friction Stir Weld ◽  
Friction Stir ◽  
Weld Joints

Mechanical Properties of JIS-S55C Friction Stir Weld Joints

2016 ◽  
Vol 2016.52 (0) ◽  
pp. 510
Author(s):  
Kohei MAKINO ◽  
Yasuyuki MIYANO ◽  
Osamu KAMIYA ◽  
Rintaro UEJI ◽  
Masanori YASUYAMA ◽  
...  
Keyword(s):  
Mechanical Properties ◽  
Friction Stir Weld ◽  
Friction Stir ◽  
Weld Joints

Damage Tolerance Properties of 2198-T8 Integral Fuselage Panel between Double Friction Stir Weld Joints

2011 ◽  
Vol 138-139 ◽  
pp. 651-656 ◽  
Author(s):  
Yu E Ma ◽  
Bao Qi Liu ◽  
Zhen Qiang Zhao
Keyword(s):  
Crack Growth ◽  
Growth Rates ◽  
Fatigue Tests ◽  
Parent Material ◽  
Friction Stir Weld ◽  
Closure Technique ◽  
Friction Stir ◽  
Weld Joints ◽  
Experimental Findings ◽  
Crack Growth Rates

Al-Li alloy 2198-T8 was used in the fuselage application. Integral fuselage panels were joined by double friction stir welds. Fatigue tests were conducted in the R=0.1. Notch was made between two welds. Residual stresses were measured and analyzed in the test samples with double welds. Cracks grew from the centre of two welds and across the two welds were observed, and crack growth rates were measured and compared with parent material. It is shown that crack growth rates are lower between double welds, and it is close to parent material after cross the two welds. The virtual crack closure technique (VCCT) method was used to calculate stress intensity factor from residual stress (Kres) in aim to explain the experimental findings.

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