Practice for Classifying Failure Modes in Fiber-Reinforced-Plastic (FRP) Joints

10.1520/d5573 ◽  
2008 ◽  
Author(s):  
Author(s):  
John PT Mo ◽  
Bathmarajah Suparayan

Composite fiber-reinforced plastic products have many failure modes in the manufacturing stage. The cost of rework is high. To ensure a reliable manufacturing process and outcome, this article presents a new method to prioritize assembly process errors according to a risk-based cost of poor quality. The method combines a range of reliability techniques including cause–effect diagram, fault tree, and analytic hierarchy process to achieve multiple failure mode assessment. The outcome of this research provides direct links to develop risk mitigation plans to treat the prioritized risks of production errors in the composite fiber-reinforced plastic assembly process.


2021 ◽  
Vol 9 (7) ◽  
pp. 726
Author(s):  
Dong-Uk Kim ◽  
Hyoung-Seock Seo ◽  
Ho-Yun Jang

With the gradual application of composite materials to ships and offshore structures, the structural strength of composites that can replace steel should be explored. In this study, the mechanical bearing strength and failure modes of a composite-to-metal joining structure connected by mechanically fastened joints were experimentally analyzed. The effects of the fiber tensile strength and stress concentration on the static bearing strength and failure modes of the composite structures were investigated. For the experiment, quasi-isotropic [45°/0°/–45°/90°]2S carbon fiber-reinforced plastic (CFRP) and glass fiber-reinforced plastic (GFRP) specimens were prepared with hole diameters of 5, 6, 8, and 10 mm. The experimental results showed that the average static bearing strength of the CFRP specimen was 30% or higher than that of the GFRP specimen. In terms of the failure mode of the mechanically fastened joint, a cleavage failure mode was observed in the GFRP specimen for hole diameters of 5 mm and 6 mm, whereas a net-tension failure mode was observed for hole diameters of 8 mm and 10 mm. Bearing failure occurred in the CFRP specimens.


2007 ◽  
Vol 44 (01) ◽  
pp. 1-15
Author(s):  
Ömer Eksik ◽  
R. Ajit Shenoi ◽  
Stuart S. J. Moy ◽  
Han Koo Jeong

The paper outlines an experimental procedure devised to assess the strength of top-hat-stiffened panels under uniform pressure load. Structural stiffness issues and their dependence on lay-up have been explored. The nature of the failure, from matrix cracking through the final collapse, is detailed. Included in the discussion is the nature of failure modes and their linkage to lay-up design. Numerous strain and digital dial gauges were used to collect important information.


1994 ◽  
Vol 116 (2) ◽  
pp. 233-237 ◽  
Author(s):  
L. C. Bank ◽  
M. Nadipelli ◽  
T. R. Gentry

An experimental investigation of the local compression flange buckling and failure of commercially produced pultruded fiber-reinforced plastic (FRP) I-shaped beams is described in this paper. Results of tests on pultruded E-glass/polyester and E-glass/vinylester composite material beams are described. The test configuration was designed to cause local buckling and ultimate failure of the compression flange of the beams and to prevent global lateral-torsional buckling. The beams were stiffened to prevent crippling and warping at the supports, and local tensile failure at the load points. All beams were monitored with strain gages and LVDT’s. Buckling loads, failure loads, buckling stresses, deflections, and failure modes are reported. Effective mechanical properties of the beams, obtained from overall flexural and shear strain data, are presented. A discussion of the different failure characteristics of the polyester and the vinylester beams is provided.


Author(s):  
Fernand Ellyin

Fiber reinforced plastic (FRP) composites offer a number of advantages over the conventional industrial materials. The reluctance of adopting composite materials in high pressure applications, is partly due to a limited understanding of their behavior under multiaxial loadings and lack of qualified design methodologies. Design and analysis issues concerning pressurized components made of fiber reinforced plastic composites, are discussed in this paper. Specifically, the optimum placement of reinforcement with respect to the applied loads, failure modes and failure analysis techniques, and a method of design based on long-term leakage envelope, are presented.


2017 ◽  
Vol 37 (4) ◽  
pp. 267-283 ◽  
Author(s):  
Yifeng Gao ◽  
Fei Li ◽  
Qilin Zhao ◽  
Jiangang Gao ◽  
Xiaoqiang Yan ◽  
...  

To assess the failure modes and failure mechanisms of single pre-tightened tooth connection joints, experiments were conducted on the mechanical properties of three different materials―T700/DER-321, T700/EP4221, and E-glass/HCH-8300―under different geometric parameters. During the test, failure processes and details of the fracture surfaces were observed by using a high-speed camera, an optical microscope, and a scanning electron microscope. Then, the failure modes and failure mechanisms of the joints were analyzed by numerical simulation and theoretical methods. The results showed that only two failure modes, shear failure and crushing failure, occurred in the glass fiber-reinforced plastic single joint. However, in addition to these two failure modes, a new failure mode was found to occur in the carbon fiber-reinforced plastic single joint, i.e. compression failure. The glass fiber-reinforced plastic joint had a lower elastic modulus along the fiber direction than the carbon fiber-reinforced plastic joint, which was the fundamental cause for the new failure mode. The carbon fiber-reinforced plastic joint with compression failure had a higher bearing capacity, and a certain ductile failure will occur as a result of the large interlaminar shear strength of the composite, which is an important consideration in joint design. Thus, the material type, the geometrical parameters of the tooth, and the interlaminar shear strength of the composite all influenced the failure modes and the bearing capacity of single pre-tightened tooth connection joints.


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