A Contribution Of Environmental Investigations For Glare Riveted Joint Sizing

Beumler, Thomas; Borgonje, B; Sinke, J.

doi:10.1007/978-90-481-2746-7_42

Cited by 6 publications

(3 citation statements)

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“…It has been reported that such thermal cycling applied to multi layered fiber reinforced polymers would result in damages similar to a mechanical fatigue process [28]. On Glare, reductions of 2% and 10% on tensile strength and ILSS respectively where observed in panels exposed to out of room conditions for 86 months [3], but in this case additional effects like moisture and UV incidence probably have a greater effect that the temperature cycles. Furthermore, under such conditions, corrosion of the aluminum sheet can also account for a reduction of the FML performance [29].…”

Section: Resultsmentioning

confidence: 95%

“…FML are composed by alternate layers of a thin sheet metal and resin impregnate fiber fabrics (prepregs) and the outer layers always correspond to the sheet metal [3]. The manufacturing process commonly includes a surface preparation of the metallic sheets like anodizing and epoxy primer painting for aluminum, and hand layup to build up the parts that are cured in autoclave under controlled temperature and pressure conditions [1,4,5].…”

Section: Introductionmentioning

confidence: 99%

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The effect of thermal cycles on the mechanical properties of fiber–metal laminates

et al. 2012

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Section: Resultsmentioning

confidence: 95%

Section: Introductionmentioning

confidence: 99%

The effect of thermal cycles on the mechanical properties of fiber–metal laminates

et al. 2012

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“…properties to the properties of GLARE [5]. As a result, the MVF approach is useful for the prediction of static strength properties for GLARE as found in the literatures [5,44,45]. The MVF value can be calculated as follows:…”

Section: Metal Volume Fraction (Mvf)mentioning

confidence: 99%

The Guidelines of Material Design and Process Control on Hybrid Fiber Metal Laminate for Aircraft Structures

Park¹,

Choi²

2019

Optimum Composite Structures

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Fiber metal laminate (FML) is a hybrid material system that consists of thin metal sheets bonded into a laminate with intermediate thin fiber reinforced composite layers. The aerospace industry has recently increased their use of FMLs due to the considerable weight reduction and consequent benefits for critical load-carrying locations in commercial aircraft, such as upper fuselage skin panels. All FML materials and their processes should be qualified through enough tests and fabrication trials to demonstrate reproducible and reliable design criteria. In particular, proper surface treatment technologies are prerequisite for achieving long-term service capability through the adhesive bonding process. This chapter introduces a brief overview of design concept, material properties and process control methodologies to provide detailed background information with engineering practices and to help ensure stringent quality controls and substantiation of structure integrity. The guidelines and information found in this chapter are meant to be a documentation of current knowledge and an application of sound engineering principles to the FML part development for aerospace usage.

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