<abstract xmlns="http://www.w3.org/1999/xhtml">

<p>This article studies the pull-through resistance of a titanium carbon fibre-epoxy resin laminate fastener. Coupons with fastener holes made with different methods were compared – drilled, milled on a CNC plotter and special fibre application during laminate production. The tests were conducted according to the ASTM D7332 test standard. The studies showed that the fastener hole preparation method impacts the laminate’s resistance to fastener pull-through. Coupons with holes made with standard (drilling and milling) methods showed fastener pull-through resistance higher, on average, by 6.5% than in coupons with holes placed during plate production. Fastener work to rupture was also higher for coupons with milled and drilled holes. Microscopic observations in UV-light, using a fluorescent penetrant, showed differences in failure mechanisms between individual coupons, especially the lack of fibres in the 0° direction, in immediate vicinity to a hole prepared during laminate application.</p>
</abstract>

This article studies the pull-through resistance of a titanium carbon fibre-epoxy resin laminate fastener. Coupons with fastener holes made with different methods were compared – drilled, milled on a CNC plotter and special fibre application during laminate production. The tests were conducted according to the ASTM D7332 test standard. The studies showed that the fastener hole preparation method impacts the laminate’s resistance to fastener pull-through. Coupons with holes made with standard (drilling and milling) methods showed fastener pull-through resistance higher, on average, by 6.5% than in coupons with holes placed during plate production. Fastener work to rupture was also higher for coupons with milled and drilled holes. Microscopic observations in UV-light, using a fluorescent penetrant, showed differences in failure mechanisms between individual coupons, especially the lack of fibres in the 0° direction, in immediate vicinity to a hole prepared during laminate application.

The Influence of the Fastener Hole Preparation Method on the Fastener Pull-Through Process in a Carbon Composite

Centre for Composite Technologies, Institute of Aviation

Transactions on Aerospace Research

This work is licensed under the Creative Commons Attribution-NonCommercial-NoDerivatives 3.0 License.

This article studies the pull-through resistance of a titanium carbon fibre-epoxy resin laminate fastener. Coupons with fastener holes made with different...

The Influence of the Fastener Hole Preparation Method on the Fastener Pull-Through Process in a Carbon Composite

Online veröffentlicht: 31. Mai 2019

Seitenbereich: 45 - 53

DOI: https://doi.org/10.2478/tar-2017-0005

Schlüsselwörter
composites, fastener pull-through, ASTM D7332 standard, drilling

© 2017 Copyright by Lukasiewicz Research Network – Institute of Aviation

This work is licensed under the Creative Commons Attribution-NonCommercial-NoDerivatives 3.0 License.

The Influence of the Fastener Hole Preparation Method on the Fastener Pull-Through Process in a Carbon Composite

Online veröffentlicht: 31. Mai 2019

Seitenbereich: 45 - 53

DOI: https://doi.org/10.2478/tar-2017-0005

Schlüsselwörtercomposites, fastener pull-through, ASTM D7332 standard, drilling

© 2017 Copyright by Lukasiewicz Research Network – Institute of Aviation

This work is licensed under the Creative Commons Attribution-NonCommercial-NoDerivatives 3.0 License.

Schlüsselwörter
composites, fastener pull-through, ASTM D7332 standard, drilling