๐”– Bobbio Scriptorium
โœฆ   LIBER   โœฆ

Characterization of carbon/epoxy materials for structural repair of carbon/BMI structures

โœ Scribed by J. Moutier; M. Fois; C. Picard


Publisher
Elsevier Science
Year
2009
Tongue
English
Weight
346 KB
Volume
40
Category
Article
ISSN
1359-8368

No coin nor oath required. For personal study only.

โœฆ Synopsis


Characterization and compatibility of high-performance epoxy resins were investigated for on site repair of carbon/bismaleimide aircraft structures. First, processing of three bi-component resins was studied. Then, physical and mechanical characterizations were carried out on carbon fabric/repair resin composite laminates (materials A, B and C) before and after ageing and results are presented. One composite (material A) was chosen, according to industrial specifications, the main criterion being the glass transition temperature. The compatibility of this material with the carbon/BMI structures to be repaired was checked with lap shear tests. Compatibility between the selected repair material and carbon/epoxy composites, whose repair procedure is already known, was conducted and considered as reference point. The obtained results allowed to validate material A for on site step structural repair of the carbon/BMI structures of our industrial partner.


๐Ÿ“œ SIMILAR VOLUMES


Dynamic mechanical analysis of carbon/ep
โœ W.K. Goertzen; M.R. Kessler ๐Ÿ“‚ Article ๐Ÿ“… 2007 ๐Ÿ› Elsevier Science ๐ŸŒ English โš– 340 KB

The viscoelastic behavior of a carbon fiber/epoxy matrix composite material system used for pipeline repair has been evaluated though dynamic mechanical analysis. The effects of the heating rate, frequency, and measurement method on the glass transition temperature (T g ) were studied. The increase

Structural characterization of carbon ma
โœ T.G Miller; D.B Fischbach ๐Ÿ“‚ Article ๐Ÿ“… 1975 ๐Ÿ› Elsevier Science ๐ŸŒ English โš– 129 KB

Abstr anthracene chars heat treated between 500 and 1200ยฐC is developped and applied to d.c. electrical conductivity, paramagnetic susceptibility and apparent density. An inhomogeneous process for the carbonization is proposed, in agreement with recent results on the structure of these chars. acts 3

Development of carbon/epoxy structural c
โœ Paolo Feraboli; Attilio Masini ๐Ÿ“‚ Article ๐Ÿ“… 2004 ๐Ÿ› Elsevier Science ๐ŸŒ English โš– 511 KB

Development of the carbon/epoxy body panels and structural components of the Lamborghini Murcie `lago is discussed, while use of aerospace grade technology and materials is justified for this particular application. The influence of fiber architecture on the strength of a composite panel for the sam

Characterization of carbon nanotube 3D-s
โœ Celeste M.C. Pereira; Paulo Nรณvoa; Marta Martins; Stefan Forero; Felicitas Hepp; ๐Ÿ“‚ Article ๐Ÿ“… 2010 ๐Ÿ› Elsevier Science ๐ŸŒ English โš– 697 KB

This work presents the use of carbon nanotube (CNT) skeletons and the resin infusion process as a path towards the production of polymer composites with high and well dispersed nanotube content. A general purpose low viscosity epoxy resin was used as matrix in the reported process assessment. Thin C