Gesell, Thomas und Holzhüter, Dirk und Kosmann, Jens und Schollerer, Martin und Makiela, Patrick Adrian und Hühne, Christian (2025) Examination of film and paste adhesive behaviour under cryogenic conditions using a thick adherend shear test. Journal of Adhesion. Taylor & Francis. doi: 10.1080/00218464.2025.2600613. ISSN 0021-8464.
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Offizielle URL: https://www.tandfonline.com/doi/full/10.1080/00218464.2025.2600613?src=&#abstract
Kurzfassung
Carbon fibre reinforced polymers (CFRP) are key enablers for lightweight liquid hydrogen storage in aerospace applications. Adhesive bonding provides a structurally efficient and inherently leak-tight method for joining CFRP and hybrid substrates, offering clear advantages over mechanically fastened joints. While most studies focus on shear stress due to the technica difficulty of measuring strain at cryogenic temperatures, the brittle nature of epoxy adhesives under these conditions makes it crucial to establish clear shear strain limits to ensure both leak-tightness and structural performance. This study introduces a methodology for characterising structural film and paste adhesives using thick adherend shear tests under cryogenic conditions. The approach incorporates the development of a dedicated cryogenic test rig (CryoTAST) and the adaptation of a custom-built capacitive extensometer suitable for use at cryogenic temperatures. Shear properties of four adhesives were determined in accordance with ASTM D5656. Furthermore, the influence of manufacturing variability was assessed by evaluating three bondline thicknesses per adhesive. The results provide essential input data for the robust design and qualification of adhesively bonded joints in CFRP liquid hydrogen tanks, supporting both their mechanical performance and leak-tightness under extreme environmental conditions.
| elib-URL des Eintrags: | https://elib.dlr.de/226514/ | ||||||||||||||||||||||||||||
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| Dokumentart: | Zeitschriftenbeitrag | ||||||||||||||||||||||||||||
| Zusätzliche Informationen: | This research was funded by the German Federal Ministry for Economic Affairs and Climate Action (BMWK) within the framework of the national aviation research programme LuFo VI-2. The project “HYTANK” was supported under grant number 20W2214G | ||||||||||||||||||||||||||||
| Titel: | Examination of film and paste adhesive behaviour under cryogenic conditions using a thick adherend shear test | ||||||||||||||||||||||||||||
| Autoren: |
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| Datum: | 25 Dezember 2025 | ||||||||||||||||||||||||||||
| Erschienen in: | Journal of Adhesion | ||||||||||||||||||||||||||||
| Referierte Publikation: | Ja | ||||||||||||||||||||||||||||
| Open Access: | Ja | ||||||||||||||||||||||||||||
| Gold Open Access: | Nein | ||||||||||||||||||||||||||||
| In SCOPUS: | Ja | ||||||||||||||||||||||||||||
| In ISI Web of Science: | Ja | ||||||||||||||||||||||||||||
| DOI: | 10.1080/00218464.2025.2600613 | ||||||||||||||||||||||||||||
| Verlag: | Taylor & Francis | ||||||||||||||||||||||||||||
| ISSN: | 0021-8464 | ||||||||||||||||||||||||||||
| Status: | veröffentlicht | ||||||||||||||||||||||||||||
| Stichwörter: | Adhesive characterisation, cryogenic applications, strain measurement, CFRP liquid hydrogen tank, aerospace | ||||||||||||||||||||||||||||
| HGF - Forschungsbereich: | Luftfahrt, Raumfahrt und Verkehr | ||||||||||||||||||||||||||||
| HGF - Programm: | Luftfahrt | ||||||||||||||||||||||||||||
| HGF - Programmthema: | Komponenten und Systeme | ||||||||||||||||||||||||||||
| DLR - Schwerpunkt: | Luftfahrt | ||||||||||||||||||||||||||||
| DLR - Forschungsgebiet: | L CS - Komponenten und Systeme | ||||||||||||||||||||||||||||
| DLR - Teilgebiet (Projekt, Vorhaben): | L - Strukturwerkstoffe und Bauweisen | ||||||||||||||||||||||||||||
| Standort: | Braunschweig | ||||||||||||||||||||||||||||
| Institute & Einrichtungen: | Institut für Systemleichtbau > Funktionsleichtbau | ||||||||||||||||||||||||||||
| Hinterlegt von: | Gesell, Thomas | ||||||||||||||||||||||||||||
| Hinterlegt am: | 22 Sep 2026 08:29 | ||||||||||||||||||||||||||||
| Letzte Änderung: | 22 Sep 2026 09:36 |
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