Manufacturing and impact behaviour of aeronautic overmolded grid-stiffened thermoplastic carbon plates

Autor: F. Neveu, C. Cornu, P. Olivier, B. Castanié
Přispěvatelé: Institut Clément Ader (ICA), Institut Supérieur de l'Aéronautique et de l'Espace (ISAE-SUPAERO)-Institut National des Sciences Appliquées - Toulouse (INSA Toulouse), Institut National des Sciences Appliquées (INSA)-Université de Toulouse (UT)-Institut National des Sciences Appliquées (INSA)-Université de Toulouse (UT)-Université Toulouse III - Paul Sabatier (UT3), Université de Toulouse (UT)-Centre National de la Recherche Scientifique (CNRS)-IMT École nationale supérieure des Mines d'Albi-Carmaux (IMT Mines Albi), Institut Mines-Télécom [Paris] (IMT)-Institut Mines-Télécom [Paris] (IMT), CEntre Technique des Industries Mécaniques - Cetim (FRANCE)
Jazyk: angličtina
Rok vydání: 2022
Předmět:
Zdroj: Composite Structures
Composite Structures, 2022, 284, pp.115228. ⟨10.1016/j.compstruct.2022.115228⟩
ISSN: 0263-8223
DOI: 10.1016/j.compstruct.2022.115228⟩
Popis: International audience; Thermoplastic composites offer many opportunities for aeronautics. Among them is the possibility of overmolding composite parts to obtain finished “netshape” parts in medium series. This paper presents the complexity of the manufacturing method and the manufacturing defects that may occur in some grid-stiffened overmolded parts using aeronautic thermoplastics. The results of impact tests up to 15 J carried out at various locations of the plates and the grid show that, due to manufacturing defects at the overmolded grid/plate interface, very significant delaminations can be observed.
Databáze: OpenAIRE
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