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2015
DOI: 10.1016/j.matdes.2015.04.051
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Assessment of alternative joining techniques for Ti–6Al–4V/CFRP hybrid joints regarding tensile and fatigue strength

Abstract: YAG laser riveting of Ti-6Al-4V/CFRP lap joint was successfully realized-Tensile strength is comparable to that of conventional riveted lap joints-Fatigue strength of conventional riveted joint can be increased by adhesive bonding-The effect of adhesive bonding is comparable to surface structuring of Ti-6Al-4V

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Cited by 54 publications
(20 citation statements)
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“…A solution to avoid galvanic corrosion is to use fasteners or shields made of a metal with less difference in the galvanic potential compared to carbon-reinforced composite. Titanium alloys are a good example of such materials [ 122 ], but the fasteners made of them are expensive and heavy compared to fasteners made of aluminum alloys [ 16 , 121 ]. Since thousands of fasteners are usually used to join the aircraft structure, it results also in a severe cost and weight penalty [ 123 ].…”
Section: Fastener Typesmentioning
confidence: 99%
“…A solution to avoid galvanic corrosion is to use fasteners or shields made of a metal with less difference in the galvanic potential compared to carbon-reinforced composite. Titanium alloys are a good example of such materials [ 122 ], but the fasteners made of them are expensive and heavy compared to fasteners made of aluminum alloys [ 16 , 121 ]. Since thousands of fasteners are usually used to join the aircraft structure, it results also in a severe cost and weight penalty [ 123 ].…”
Section: Fastener Typesmentioning
confidence: 99%
“…Due to the high assembly and repair efficiency, low requirements for surface treatment and good compatibility between CFRPI materials and Ti alloys, mechanically fastened CFRPI-Ti alloy joints are more favorable as compared with the corresponding bonded joints in aircraft engine structures. 1 Meanwhile, the screws are often used to tighten the fastener from only accessible one side of the structure with a smoother surface. 2 Thus, the high-temperature performances of the screwed CFRPI-Ti alloy joints are of great concern in the design and repair of aircraft engine structures.…”
Section: Introductionmentioning
confidence: 99%
“…Wang et al [5] studied hybrid joints between carbon fibre reinforced polymers (CFRP) and titanium Ti-6Al-4V, using the Comeld ™ electron beam machining technology [6] to sculpt surface protrusions which enhanced bond strength considerably. Working with a similar material combination, Kashaev et al [7] investigated 'laser rivetted' hybrid joints, observing mechanical properties which were comparable to those of traditional riveted joints. Ko et al [8] characterised hybrid joints made of stainless steel 'z-pins' under fatigue and environmental conditions, with pins being worked mechanically prior to insertion for increased surface roughness and hence improved crack bridging performance.…”
Section: Introductionmentioning
confidence: 99%