Numerical investigation of a layered hybrid load introduction element for thin-walled CFRP structures

Publikation: Beitrag in Buch/Bericht/Sammelwerk/KonferenzbandAufsatz in KonferenzbandForschungPeer-Review

Autorschaft

  • Alexander Herwig
  • Carsten Schmidt
  • Peter Horst

Externe Organisationen

  • Technische Universität Braunschweig
Forschungs-netzwerk anzeigen

Details

OriginalspracheEnglisch
Titel des SammelwerksECCM 2018 - 18th European Conference on Composite Materials
ISBN (elektronisch)9781510896932
PublikationsstatusVeröffentlicht - 2020
Veranstaltung18th European Conference on Composite Materials, ECCM 2018 - Athens, Griechenland
Dauer: 24 Juni 201828 Juni 2018

Abstract

The project “Multi-Layer Inserts” (MLI) proposes a new design for inserts used in thin-walled structures made of carbon fiber reinforced plastic (CFRP). The proposed insert consists of multiple thin metal sheets and is build up simultaneously with the laminate in a fully automated intrinsic hybridization process, eliminating time-consuming post-processing steps. Furthermore, such inserts significantly increase the bonding area between metal and CFRP in comparison to conventional inserts at equal weight. This results in a significant increase of the loads that can be transmitted into the CFRP. The individual material layers of the local CFRP-metal-hybrid (CFRP, metal, adhesive) are very thin and form a multitude of adhesive connections. Prior investigations have shown advantages of octagonal shaped metal inserts in reducing strain concentrations. The present work discusses a simplification methodology to investigate the MLI's dependence on and sensitivity to design parameters by dividing the model of the complex adhesive connection into combinations of common lap joints. After proving the transferability of the lap joint approach for very thin laminates, a comparison of the experimentally measured surface strain distribution near an octagonal MLI is used to assess the quality of the approximation.

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Numerical investigation of a layered hybrid load introduction element for thin-walled CFRP structures. / Herwig, Alexander; Schmidt, Carsten; Horst, Peter.
ECCM 2018 - 18th European Conference on Composite Materials. 2020.

Publikation: Beitrag in Buch/Bericht/Sammelwerk/KonferenzbandAufsatz in KonferenzbandForschungPeer-Review

Herwig, A, Schmidt, C & Horst, P 2020, Numerical investigation of a layered hybrid load introduction element for thin-walled CFRP structures. in ECCM 2018 - 18th European Conference on Composite Materials. 18th European Conference on Composite Materials, ECCM 2018, Athens, Griechenland, 24 Juni 2018.
Herwig, A., Schmidt, C., & Horst, P. (2020). Numerical investigation of a layered hybrid load introduction element for thin-walled CFRP structures. In ECCM 2018 - 18th European Conference on Composite Materials
Herwig A, Schmidt C, Horst P. Numerical investigation of a layered hybrid load introduction element for thin-walled CFRP structures. in ECCM 2018 - 18th European Conference on Composite Materials. 2020
Herwig, Alexander ; Schmidt, Carsten ; Horst, Peter. / Numerical investigation of a layered hybrid load introduction element for thin-walled CFRP structures. ECCM 2018 - 18th European Conference on Composite Materials. 2020.
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abstract = "The project “Multi-Layer Inserts” (MLI) proposes a new design for inserts used in thin-walled structures made of carbon fiber reinforced plastic (CFRP). The proposed insert consists of multiple thin metal sheets and is build up simultaneously with the laminate in a fully automated intrinsic hybridization process, eliminating time-consuming post-processing steps. Furthermore, such inserts significantly increase the bonding area between metal and CFRP in comparison to conventional inserts at equal weight. This results in a significant increase of the loads that can be transmitted into the CFRP. The individual material layers of the local CFRP-metal-hybrid (CFRP, metal, adhesive) are very thin and form a multitude of adhesive connections. Prior investigations have shown advantages of octagonal shaped metal inserts in reducing strain concentrations. The present work discusses a simplification methodology to investigate the MLI's dependence on and sensitivity to design parameters by dividing the model of the complex adhesive connection into combinations of common lap joints. After proving the transferability of the lap joint approach for very thin laminates, a comparison of the experimentally measured surface strain distribution near an octagonal MLI is used to assess the quality of the approximation.",
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AU - Herwig, Alexander

AU - Schmidt, Carsten

AU - Horst, Peter

N1 - Funding Information: This paper is based on investigations of the subproject 1 – ‘Multilayer Inserts – intrinsic hybrid compounds for load introduction into thin walled high-performance CFRP-Structures’ of the priority program 1712 ‘Intrinsic hybrid composites for lightweight load-bearings’, which is kindly supported by the German Research Foundation (DFG).

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N2 - The project “Multi-Layer Inserts” (MLI) proposes a new design for inserts used in thin-walled structures made of carbon fiber reinforced plastic (CFRP). The proposed insert consists of multiple thin metal sheets and is build up simultaneously with the laminate in a fully automated intrinsic hybridization process, eliminating time-consuming post-processing steps. Furthermore, such inserts significantly increase the bonding area between metal and CFRP in comparison to conventional inserts at equal weight. This results in a significant increase of the loads that can be transmitted into the CFRP. The individual material layers of the local CFRP-metal-hybrid (CFRP, metal, adhesive) are very thin and form a multitude of adhesive connections. Prior investigations have shown advantages of octagonal shaped metal inserts in reducing strain concentrations. The present work discusses a simplification methodology to investigate the MLI's dependence on and sensitivity to design parameters by dividing the model of the complex adhesive connection into combinations of common lap joints. After proving the transferability of the lap joint approach for very thin laminates, a comparison of the experimentally measured surface strain distribution near an octagonal MLI is used to assess the quality of the approximation.

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