Titre : |
Manufacture of nominal-shape composite stiffeners using autoclave injection |
Type de document : |
texte imprimé |
Auteurs : |
Erik Kappel, Auteur ; Manuel Buggisch, Auteur ; V. J. S. Prado, Auteur |
Année de publication : |
2016 |
Article en page(s) : |
p. 37-39 |
Note générale : |
Bibliogr. |
Langues : |
Anglais (eng) |
Catégories : |
Autoclave (technologie) Avions -- Matériaux Composites à fibres de carbone -- Moulage par injection Renforts (matériaux)
|
Index. décimale : |
668.4 Plastiques, vinyles |
Résumé : |
Composites are the material of choice for today's aircraft structures due to their excellent weight-specific performance. Recent dry-fibre technology developments open the door for infusion-based composites to become a serious competitor for the widely adopted prepreg-based structures, which currently dominate aerospace structural applications. |
Note de contenu : |
- Autoclave injection process for high-performance composites
- Straightforward prediction-based tool compensation
- Verification and validation
- FIGURES : 1. Composite stiffener dimensions (left) and the aluminium tool concept used (right) - 2. Manufactured CFRP component, segmented frame and final component - 3. Normalized PID predictions and compensation measures derived through the P-approach - 4. Cross-section evaluation of the four manufactured composite profiles |
Permalink : |
https://e-campus.itech.fr/pmb/opac_css/index.php?lvl=notice_display&id=26864 |
in JEC COMPOSITES MAGAZINE > N° 106 (07/2016) . - p. 37-39