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Surface toughening - An industrial approach to increase the robustness of pure adhesive joints with film adhesives

Schollerer, Martin und Kosmann, Jens und Holzhüter, Dirk und Bello-Larroche, Carlos und Hühne, Christian (2020) Surface toughening - An industrial approach to increase the robustness of pure adhesive joints with film adhesives. Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, 234 (13), Seiten 1980-1987. Sage Publications. doi: 10.1177/0954410020950071. ISSN 0954-4100.

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Offizielle URL: https://journals.sagepub.com/doi/full/10.1177/0954410020950071

Kurzfassung

Bonding is known for its wide range of advantages over bolted joints when joining different materials together. However, the advantages e.g. of homogeneous load distribution can quickly be lost in case of overload. For this reason, the load occurring in the adhesive is reduced by constructive measures far below the yield stress of the adhesive, which leads to a conservative joint design. And to be on the safe side, a few “chicken rivets” are then placed again. This problem is particularly well known in aviation. Highly loaded components are structurally bonded by a combination of rivets and adhesive in order to underline the advantages of structural adhesive bonding with the safety of the well-known bolted joints. Known as fail-safe design, this concept is damage tolerant and more robust against manufacturing defects through a secured double load path.  Especially when joining fiber-reinforced composites, bolts weaken the adherends of the joint and only contribute to load transfer when the brittle adhesive fails. With the help of Surface Toughening, a boltless technique for reducing stress concentrations and arresting cracks in adhesive bonded joints is available. This work describes the industrial application of this technique. Starting with coupon tests and a small scale demonstrator to ensure the compatibility with industrial manufacturing processes, such as infusion and prepreg manufacturing, a large scale demonstrator of a 2 m carbon fiber reinforced plastic (CFRP) - HTP leading edge with hybrid laminar flow control is manufactured by the industrial partner AERnnova. Verifying a simple and cost-effective application of the technology, Surface Toughening enables robust bonded joints with a minimum impact on today's process of adhesive bonding.

elib-URL des Eintrags:https://elib.dlr.de/136681/
Dokumentart:Zeitschriftenbeitrag
Titel:Surface toughening - An industrial approach to increase the robustness of pure adhesive joints with film adhesives
Autoren:
AutorenInstitution oder E-Mail-AdresseAutoren-ORCID-iDORCID Put Code
Schollerer, Martinmartin.schollerer (at) dlr.dehttps://orcid.org/0000-0001-7015-9461145175972
Kosmann, JensJens.Kosmann (at) dlr.dehttps://orcid.org/0000-0002-2225-4832NICHT SPEZIFIZIERT
Holzhüter, Dirkdirk.holzhueter (at) dlr.dehttps://orcid.org/0000-0003-1001-2366NICHT SPEZIFIZIERT
Bello-Larroche, CarlosNICHT SPEZIFIZIERTNICHT SPEZIFIZIERTNICHT SPEZIFIZIERT
Hühne, ChristianChristian.Huehne (at) dlr.dehttps://orcid.org/0000-0002-2218-1223145175977
Datum:13 August 2020
Erschienen in:Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering
Referierte Publikation:Ja
Open Access:Ja
Gold Open Access:Nein
In SCOPUS:Ja
In ISI Web of Science:Ja
Band:234
DOI:10.1177/0954410020950071
Seitenbereich:Seiten 1980-1987
Verlag:Sage Publications
Name der Reihe:Part G: Journal of Aerospace Engineering
ISSN:0954-4100
Status:veröffentlicht
Stichwörter:Adhesive bonding, surface toughening, peak stress reduction, strength increasing
HGF - Forschungsbereich:Luftfahrt, Raumfahrt und Verkehr
HGF - Programm:Luftfahrt
HGF - Programmthema:Flugzeuge
DLR - Schwerpunkt:Luftfahrt
DLR - Forschungsgebiet:L AR - Aircraft Research
DLR - Teilgebiet (Projekt, Vorhaben):L - Strukturen und Werkstoffe (alt)
Standort: Braunschweig
Institute & Einrichtungen:Institut für Faserverbundleichtbau und Adaptronik > Funktionsleichtbau
Hinterlegt von: Schollerer, Martin
Hinterlegt am:19 Okt 2020 06:41
Letzte Änderung:24 Okt 2023 14:28

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