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Naji, M. |
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Motta, Antonella |
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Aletan, Dirar |
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Mohamed, Tarek |
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Ertürk, Emre |
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Taccardi, Nicola |
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Kononenko, Denys |
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Petrov, R. H. | Madrid |
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Alshaaer, Mazen | Brussels |
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Bih, L. |
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Casati, R. |
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Muller, Hermance |
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Kočí, Jan | Prague |
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Šuljagić, Marija |
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Kalteremidou, Kalliopi-Artemi | Brussels |
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Azam, Siraj |
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Ospanova, Alyiya |
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Blanpain, Bart |
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Ali, M. A. |
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Popa, V. |
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Rančić, M. |
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Ollier, Nadège |
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Azevedo, Nuno Monteiro |
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Landes, Michael |
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Rignanese, Gian-Marco |
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Wolfahrt, Markus
Polymer Competence Center Leoben (Austria)
in Cooperation with on an Cooperation-Score of 37%
Topics
Publications (9/9 displayed)
- 2024Redox cationic frontal polymerization: a rapid curing approach for carbon fiber-reinforced composites with high fiber contentcitations
- 2024Design of Reversible Adhesives by Using a Triple Function of Ionic Liquidscitations
- 2023Redox cationic frontal polymerizationcitations
- 2023Tensile properties of flexible composites with knitted reinforcements from various yarn materialscitations
- 2022Testing mechanical performance of adhesively bonded composite joints in engineering applications: an overviewcitations
- 2021Testing mechanical performance of adhesively bonded composite joints in engineering applicationscitations
- 2019Analysis of the Macroscopic Behaviour of PMI Foamcitations
- 2019Bonded aerospace repairs under tensile loading: Wet chemical surface treatment and selected environmental conditionscitations
- 2016Thiol-Ene versus Binary Thiol–Acrylate Chemistrycitations
Places of action
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article
Bonded aerospace repairs under tensile loading: Wet chemical surface treatment and selected environmental conditions
Abstract
<p>Repair of composite structures and the impact of demanding environmental conditions is a crucial issue for the aircraft industry because of the increasing use of composites in modern aircraft. Consequently, the impact of environmental conditions common for aircraft applications on repair specimens in comparison to nonrepaired specimens is studied. All specimens are produced from a woven carbon fiber-reinforced epoxy-based prepreg. For the repair-specimens, an epoxy-based film adhesive is used for the soft patch repair approach. During the repair process, the surface of the precured prepreg is prepared by a mechanical method (sanding) and an additional chemical functionalization, respectively. Moisture absorption of the repair specimens is independent of the surface preparation method and higher for the repaired than for the nonrepaired specimens. The key influencing environmental conditions for the tensile strength and the failure mode of the repair specimens are elevated temperature testing as well as hot/wet conditioning and conditioning in deionized water.</p>