[article]
| Titre : |
Repairing instead of replacing : Process for repairing CFRP components without machining |
| Type de document : |
texte imprimé |
| Auteurs : |
David Rabe, Auteur ; Philippa Böhnke, Auteur ; Thi Anh My Huynh, Auteur ; Iris Kruppke, Auteur ; Thomas Gereke, Auteur ; Eric Häntzsche, Auteur ; Chokri Cherif, Auteur |
| Année de publication : |
2021 |
| Article en page(s) : |
p. 34-36 |
| Langues : |
Anglais (eng) |
| Catégories : |
Composites -- Réparation
Composites à fibres de carbone
Coût -- Contrôle
Fibres à orientation unidirectionnelle
Patchs de réparation
Rayonnement ultraviolet
Structures multicouches
Tricot
|
| Index. décimale : |
668.4 Plastiques, vinyles |
| Résumé : |
CFRP components are often in continuous use under harsh environmental conditions, for example in aircraft and motor vehicles. If any damage occurs, the CFRP structures are simply replaced by new components in most cases. This is mainly due to the high cost of established repair methods. With a newly developed process, defective CFRP structures can now be repaired locally much more easily. |
| Note de contenu : |
- Three process steps to the repaired CFRP component
- Simulation as a basis
- UV light instead of manual ablation
- Tests with UD, TFP and MLG patches
- Costs reduced by 80 percent
- Fig. 1 : Overview of the simulation-based repair method for CFRP components: the method enables targeted repair of the damaged area
- Fig. 2 : In the process, the damaged area of the test specimen (1) is treated with a UV LED lamp (see Fig. 3). The fibers are then separated (3) in the repair area (2) thus exposed. The prepared repair area (4) is then cleaned, activated and prepared by an adhesion promoter for the insertion of the patch
- Fig. 3 : Matrix removal in the repair area is carried out with the help of an UV LED lamp. Compared to conventional processes, the manual effort is highly reduced, which ensures higher reproducibility
- Fig. 4 : For the repair, for example, a TFP patch is inserted into the prepared site (A – first patch part inserted, B – second patch part inserted). For the subsequent reinfiltration (C), a method based on the VARI process is used
- Fig. 5 : Rupture force (F max) and elongation at F max for the different patch variants : The UD and MLG patches achieve the best values |
| En ligne : |
https://drive.google.com/file/d/1BHkov2psRWJmmN5IaLr9k_L_tpLUbZcq/view?usp=drive [...] |
| Format de la ressource électronique : |
Pdf |
| Permalink : |
https://e-campus.itech.fr/pmb/opac_css/index.php?lvl=notice_display&id=36176 |
in KUNSTSTOFFE INTERNATIONAL > Vol. 111, N° 6 (2021) . - p. 34-36
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Repairing instead of replacing in KUNSTSTOFFE INTERNATIONAL, Vol. 111, N° 6 (2021)
