Fatigue Life Enhancement of a D16at Aluminum Alloy for Aircraft Components with Fastener Holes

2020 ◽  
Vol 52 (1) ◽  
pp. 1-15
Author(s):  
G. V. Duncheva ◽  
J. T. Maximov ◽  
N. Ganev ◽  
A. P. Anchev
Author(s):  
Zheng Jin ◽  
P. K. Mallick

Self-piercing riveting is receiving attention in the automotive industry as an alternative to spot welding for body panels and structures, especially if they are made of aluminum alloys. In this paper, we explore the possibility of enhancing fatigue life of self-piercing riveted joints in 5754-O aluminum alloy sheets. Different sheet thickness combinations are considered. Coining is found to increase fatigue life significantly for self-piercing riveted joints in thinner sheets. However, the fatigue life enhancement is found to be less significant if the sheet thickness is in the range of 3 mm. The enhancement of fatigue life is attributed to residual compressive stresses around the coined area.


2019 ◽  
Vol 269 ◽  
pp. 06002
Author(s):  
Salina Saidin ◽  
Dahia Andud ◽  
Yupiter H. P. Manurung ◽  
Muhd. Faiz Mat ◽  
Noridzwan Nordin ◽  
...  

This paper deals with a comprehensive investigation of fatigue life enhancement on semiautomated Gas Metal Arc Welding (GTAW) butt weld joint which is found almost everywhere in Malaysia welding structure steel sectors. The selected material in this study was high strength low alloy steel S460G2+M commonly used extremely in steel structure due to its outstanding mechanical properties. In this investigation, the method for joining the butt weld was conducted by unprofessional welder using semi-automated GMAW. At first, suitable welding parameters were identified and formulated into welding procedure specification (WPS) qualification conforming to AWS D1.1 standard. The test specimens were prepared and tested to ensure the welding quality. Further, the HFMI using Pneumatic Impact Treatment (PIT) technique were applied at the weld toe of the butt weld as tool for fatigue life enhancement. To investigate the influence of HFMI/PIT on the fatigue strength, the specimens were undergone fatigue test using universal fatigue machine using a constant amplitude loading. Finally, the comparison of the fatigue strength of as welded and treated specimens to indicate the beneficial influence of the treatment. Yes, the conduction by unprofessional welder using semi-automatic GMAW, the findings showed the improvement of fatigue strength and slope of S-N curves. In addition, the fracture location of test specimen shows physically affected by shifting from critical weld transition to base metal. The tensile test and hardness value also showed a slight difference as compared to untreated specimens.


2015 ◽  
Vol 112 ◽  
pp. 93-107 ◽  
Author(s):  
Galya Duncheva ◽  
Jordan Maximov ◽  
Nikolaj Ganev ◽  
Marieta Ivanova

2007 ◽  
Vol 561-565 ◽  
pp. 2393-2398 ◽  
Author(s):  
Yoshihisa Kaneko ◽  
Y. Nishijima ◽  
T. Sanda ◽  
Satoshi Hashimoto

Effect of Ni/Cu multilayer coating on fatigue durability was investigated. The Ni/Cu multilayered films were coated on cylindrical copper specimens by electroplating technique. Thickness of individual component layers was h=20nm and 100nm and the total thickness was 5μm. The specimens with a conventional nickel coating and uncoated specimens were also prepared. Push-pull fatigue tests were carried out in air at room temperature. It was found that the specimens with the Ni/Cu multilayered coatings exhibited the fatigue lives longer than those of the conventional nickel coating. In particular, the fatigue life with the h=100nm multilayer was at least ten times longer than that with the nickel coating at the stress amplitude of 90MPa. From the electron channelling contrast imaging (ECCI) observation of subsurface areas of the copper specimens, dislocation structures peculiar to fatigue deformation was suppressed by the surface coatings.


2013 ◽  
Author(s):  
Muthuraj R ◽  
Vignesh E ◽  
Kannan C ◽  
Sundararajan Thiyagarajan

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