EFFECT EVALUATION OF THE ADHESIVE THICKNESS VARIATION IN SINGLE LAP JOINTS BONDED WITH STRUCTURAL ADHESIVE

Author(s):  
Lorena Silva ◽  
RANULFO MARTINS CARNEIRO NETO ◽  
Eduardo Sampaio ◽  
Lucas Vignoli
Materials ◽  
2021 ◽  
Vol 14 (4) ◽  
pp. 1008
Author(s):  
Francesco Musiari ◽  
Fabrizio Moroni

The low quality of adhesion performance on polymeric surfaces has forced the development of specific pretreatments able to toughen the interface between substrate and adhesive. Among these methods, atmospheric pressure plasma treatment (APPT) appears particularly suitable for its environmental compatibility and its effectiveness in altering the chemical state of the surface. In this work, an experimental study on adhesively bonded joints realized using polyamide as substrates and polyurethane as the structural adhesive was carried out with the intent to characterize their fatigue behavior, which represents a key issue of such joints during their working life. The single lap joint (SLJ) geometry was chosen and several surface pretreatments were compared with each other: degreasing, abrasion (alone and followed by APPT) and finally APPT. The results show that the abrasion combined with APPT presents the most promising behavior, which appears consistent with the higher percentage of life spent for crack propagation found by means of DIC on this class of joints with respect to the others. APPT alone confers a good fatigue resistance with respect to the simple abrasion, especially at a low number of cycles to failure.


2018 ◽  
Vol 2018 ◽  
pp. 1-10
Author(s):  
Kai Wei ◽  
Yiwei Chen ◽  
Maojun Li ◽  
Xujing Yang

Carbon fiber-reinforced plastics- (CFRP-) steel single lap joints with regard to tensile loading with two levels of adhesives and four levels of overlap lengths were experimentally analyzed and numerically simulated. Both joint strength and failure mechanism were found to be highly dependent on adhesive type and overlap length. Joints with 7779 structural adhesive were more ductile and produced about 2-3 kN higher failure load than MA830 structural adhesive. Failure load with the two adhesives increased about 147 N and 176 N, respectively, with increasing 1 mm of the overlap length. Cohesion failure was observed in both types of adhesive joints. As the overlap length increased, interface failure appeared solely on the edge of the overlap in 7779 adhesive joints. Finite element analysis (FEA) results revealed that peel and shear stress distributions were nonuniform, which were less severe as overlap length increased. Severe stress concentration was observed on the overlap edge, and shear failure of the adhesive was the main reason for the adhesive failure.


Author(s):  
Lorena M. Fernández-Cañadas ◽  
Ines Ivañez ◽  
Sonia Sanchez-Saez ◽  
Ever J. Barbero

2013 ◽  
Vol 55 (1) ◽  
pp. 35-41 ◽  
Author(s):  
K Mohamed Bak ◽  
K Kalaichelvan ◽  
G K Vijayaraghavan ◽  
M Dinesh ◽  
V Arumugam

2011 ◽  
Vol 101-102 ◽  
pp. 681-684
Author(s):  
Long Li ◽  
Ping Hu ◽  
Wei Dong Li ◽  
Xiao Qiang Han

Adhesive bonded single lap joints are used extensively in the manufacture of automobile structures. However, the joints involve many factors such as the overlap, the adherend thickness, the adherend yield strength etc. Therefore, strength prediction is a controversial issue. In order to quantify the effects of various variables, Latin Hypercube method was used to design the tests of simulation in the present study. The failure load predictive equation involving the factors of the overlap, the adherend thickness, the adherend yield strength, the adhesive thickness, the test speed and the adhesive toughness were achieved. The tests of single lap joints in tension load were carried on; while the results form experiments and formula were compared to verify its validation for strength prediction.


2004 ◽  
Vol 270-273 ◽  
pp. 64-69 ◽  
Author(s):  
Do Won Seo ◽  
Ho Chel Yoon ◽  
Yang Bae Jeon ◽  
Hyo Jin Kim ◽  
Jae Kyoo Lim

Sign in / Sign up

Export Citation Format

Share Document