Fatigue and failure mechanism in carbon fiber reinforced plastics/aluminum alloy single lap joint produced by electromagnetic riveting technique
Source abstract
Abstract
Abstract Electromagnetic riveting (EMR) process is suitable for composite joining due to small damage. In this paper, the EMR experiments were conducted to obtain the fatigue samples. Specimens with normalized driven head dimensions were tested to obtain the fatigue behaviors. The experimental results showed that the driven head dimensions had a remarkable effect on fatigue property. The fatigue life increased first and then decreased with the increasing of D/D 0 ( D and D 0 are the diameters of rivet driven head and original shaft, respectively). The electromagnetic riveted specimens with D/D 0 = 1.5 had the best fatigue properties. The fatigue failure analysis showed that the specimens had three typical fatigue failure modes: failure in the rivet, failure in the Al sheet and failure in the CFRP and Al sheets as influenced by driven head dimensions and stress levels.
Source: openaire · Quality: candidate unverified · Source record ↗
Research context
OpenAlex topics: Advanced Welding Techniques Analysis · Mechanical Behavior of Composites · Fatigue and fracture mechanics
SciVX discovery tags are terminology-based. OpenAlex topics are source-provided classifications.
References (23)
Show source-provided references
1. Static and fatigue testing thin riveted, bonded and hybrid carbon fiber double lap joints used in aircraft structures10.1016/j.compstruct.2014.11.004 ↗
2. Carbon nanotube-based health monitoring of mechanically fastened composite joints10.1016/j.compscitech.2008.05.016 ↗
3. Mechanics of mechanically fastened joints in polymer-matrix composite structures-A review10.1016/j.compscitech.2008.09.037 ↗
4. Interference-fit riveting technique in fiber composite laminates10.1016/j.ast.2005.11.003 ↗
5. Electromagnetic forming-A review10.1016/j.jmatprotec.2010.12.012 ↗
6. An analysis of rivet die design in electromagnetic riveting10.1115/1.3269482 ↗
7. Integration and qualification of the HH500 hand operated electromagnetic riveting system on the 747 Section 11
8. A finite element study of electromagnetic riveting10.1115/1.2830576 ↗
9. Experimental evaluation on mechanical properties of a riveted structure with electromagnetic riveting10.1007/s00170-014-6688-4 ↗
10. Mechanical properties and fatigue behavior of electromagnetic riveted lap joints influenced by shear loading10.1016/j.jmapro.2017.02.022 ↗
11. Effect of discharge voltage on the deformation of Ti grade 1 rivet in electromagnetic riveting10.1016/j.msea.2013.10.084 ↗
12. QJ 782A-2005 general technical requirements for riveting.
13. The exponential law of endurance tests
14. Fatigue behavior of friction spot welds in lap shear specimens of AA5754 and Ti6Al4V alloys10.1016/j.ijfatigue.2016.06.005 ↗
15. Fatigue life prediction model for riveted lap joints10.1016/j.engfailanal.2015.03.013 ↗
16. Influence of interference-fit size on bearing fatigue response of single-lap carbon fiber reinforced polymer/Ti alloy bolted joints10.1016/j.triboint.2015.08.044 ↗
17. The effect of interference fit size on the fatigue life of bolted joints in composite laminates10.1016/j.compositesb.2013.04.048 ↗
18. Interface damage behavior during interference-fit bolt installation process for CFRP/Ti alloy joining structure10.1111/ffe.12313 ↗
19. The fatigue and final fracture behavior of SiC particle reinforced 7034 aluminum matrix composites10.1016/S1359-8368(02)00025-2 ↗
20. Fatigue properties and fracture analysis of a SiC fiber-reinforced titanium matrix composite10.1016/j.compositesb.2014.09.005 ↗
21. Three-dimensional finite element analysis of tensile-shear spot-welded joints in tensile and compressive loading conditions10.1023/B:STOM.0000041536.03924.d4 ↗
22. Delamination in adhesively bonded CFRP joints: standard fatigue, impact-fatigue and intermittent impact10.1016/j.compscitech.2007.11.006 ↗
23. Analytical modeling for stress distribution around interference fit holes on pinned composite plates under tensile load10.1016/j.compositesb.2016.06.011 ↗