Modelling Behaviour of a Carbon Epoxy Composite Exposed to Fire: Part I—Characterisation of Thermophysical Properties

Autor: Pauline Tranchard, Fabienne Samyn, Sophie Duquesne, Bruno Estèbe, Serge Bourbigot

Publikováno v: Materials, Vol 10, Iss 5, p 494 (2017)

Thermophysical properties of a carbon-reinforced epoxy composite laminate (T700/M21 composite for aircraft structures) were evaluated using different innovative characterisation methods. Thermogravimetric Analysis (TGA), Simultaneous Thermal analysis

Externí odkaz: https://doaj.org/article/0074c5859522460784de7c0b9917461a

Tento výsledek nelze pro nepřihlášené uživatele zobrazit.
K zobrazení výsledku je třeba se přihlásit.

LATEST DEVELOPMENTS IN SCALE REDUCTION FOR FIRE TESTING

Autor: Bourbigot, S., Naik, A, Bachelet, P, Sarazin, J, Tranchard, P, Samyn, F., Jimenez, M., Duquesne, S.

Publikováno v: 27th BCC Conference (Flame 2017)-Recent Advances in Flame Retardancy of Polymeric Materials
27th BCC Conference (Flame 2017)-Recent Advances in Flame Retardancy of Polymeric Materials, May 2017, Boston (Massachusetts), United States
Flame 2017
Flame 2017, Jun 2017, Boston, United States

International audience; In this paper, the scaling reduction of fire tests of interest is presented. It deals with vertical fire resistance test (fire protection of steel according to UL 1709 and ISO 834), test for building products (single burning i

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=dedup_wf_001::d945a877fdf016220557079055dc0f53
https://hal.univ-lille.fr/hal-02180309

Tento výsledek nelze pro nepřihlášené uživatele zobrazit.
K zobrazení výsledku je třeba se přihlásit.

Physical modelling of an aeronautical composite in fire

Autor: Tranchard, P., Fabienne Samyn, Duquesne, S., Montes, J-L, Bourbigot, S.

Publikováno v: Foreign Language Association of Maine Annual Conference, FLAME 2016
Foreign Language Association of Maine Annual Conference, FLAME 2016, May 2016, Stamford, CT, United States
Scopus-Elsevier

International audience; The evaluation of fire behaviour of structural composites is done through experimental tests which are time consuming and costly for the aircraft manufacturers (e.g. ISO 2685 and burnthrough test). Concurrently, the amount of

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=dedup_wf_001::024b6e256ff85e8d805f9f86dacf70ce
https://hal.univ-lille.fr/hal-01897598