| Titre : |
Thermoplastics in aerospace applications : how Daher stays one step ahead with CARAC TP |
| Type de document : |
texte imprimé |
| Auteurs : |
Stéphanie Patel, Auteur ; Charles Naejus, Auteur ; Martin Denize, Auteur |
| Année de publication : |
2023 |
| Article en page(s) : |
p. 47-50 |
| Langues : |
Anglais (eng) |
| Catégories : |
Avions -- Matériaux
Composites à fibres -- Propriétés mécaniques
Composites thermoplastiques
Fibres continues
Hautes températures
Polyaryl éther cétones
Résistance au chocs
Résistance au fluage
|
| Index. décimale : |
668.4 Plastiques, vinyles |
| Résumé : |
CARAC TP project was established to furnish in-depth knowledge on continuous fibre thermoplastic materials, and consolidates the company's lead in the use of these materials for aerospace applications. Results from CARAC TP will be applied to a broad range of uses at high temperature (up to a constant one 170°C), and to better control forming processes. This project was conducted in partnership with specialised composite materials laboratories. The results were partly presented at the 2022 SAMPE France event. |
| Note de contenu : |
- Defining the process window : Controlling crystallisation - Studying degradation
- Resistance to the environment
- Resistance to creep, fatigue, and impact
- Fig. 1 Daher's CARAC TP project approach
- Fig. 2 : Example of DSC curves with different cooling rates
- Fig. 3 : TTT diagram of isothermal and anisothermal conditions
- Fig. 4 : DSC analysis after exposure to temperatures higher than the melting temperature for different times
- Fig. 5 : Example of analysis of material after time/temperature exposure : mass loss bending modulus evolution
- Fig. 6 : Visual observation and chemical analysis on material after UV exposure
- Fig. 7 : Observation on panels fire exposure, UD thermoplastic family and UD thermoset family
- Fig. 8 : Tensile static test results onf QI stacking at room temperature, 120°C ande 170°C
- Fig. 9 : Example of fatigue diagram, tensile mode, QI stacking at room temperature, 120°C and 170°C
- Fig. 10 : Type of deformation after creeping, soft stacking, maintaining tensile load for 6 hours at 170°C
- Fig. 11 : Picture taken by a thermal camera during impact test at elevated temperature : tomography of a sample after impact |
| En ligne : |
https://drive.google.com/file/d/1hGQCQa8e-ZGyuz5vz39Co49sBoL8h2rV/view?usp=drive [...] |
| Format de la ressource électronique : |
Pdf |
| Permalink : |
https://e-campus.itech.fr/pmb/opac_css/index.php?lvl=notice_display&id=40221 |
in JEC COMPOSITES MAGAZINE > N° 151 (06-07/2023) . - p. 47-50
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Thermoplastics in aerospace applications in JEC COMPOSITES MAGAZINE, N° 151 (06-07/2023)
