| Titre : |
Aircraft coating |
| Type de document : |
texte imprimé |
| Auteurs : |
Shashank T. Mhaske, Auteur ; Pravin G. Kadam, Auteur |
| Année de publication : |
2010 |
| Article en page(s) : |
p. 61-68 |
| Note générale : |
Bibliogr. |
| Langues : |
Anglais (eng) |
| Catégories : |
Anticorrosion
Avions -- Revêtements:Avions -- Peinture
|
| Index. décimale : |
667.9 Revêtements et enduits |
| Résumé : |
Corrosion remains a significant threat to aircraft structural integrity ; it can reduce section thicknesses, generate corrosion-related cracks, and create stress concentrations which act as sites for fatigue cracking. The presence of corrosion induced cracking can shorten the overall crack growth life, and perhaps more significantly, lead to fatigue cracking in areas which would not normally be regarded as critical. Current corrosion-damage maintenance procedures are usually based on a policy of fin-and-fix which often involves the complete stripping of an aircraft coating system to permit visual inspection of the outer skin of the aircraft, or the disassembly of structure to assist inspection. All these activities are costly and may significantly aircraft flett readiness. |
| Note de contenu : |
COATING PROPERTIES : 1. Corrosion protective properties - 2. Optical properties - 3. Mechanical properties plus chemical/solvent resistance - 4. Exterior durability and property maintenance in exposure - 5. Film thickness : Interaction of sol-gel network with metal surfaces and with the primer or topcoat. |
| Permalink : |
https://e-campus.itech.fr/pmb/opac_css/index.php?lvl=notice_display&id=10495 |
in PAINTINDIA > Vol. LX, N° 10 (10/2010) . - p. 61-68
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Aircraft coating in PAINTINDIA, Vol. LX, N° 10 (10/2010)
