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Bonding composites : from performance to fashion / Laurie Gibbons in ADHESIVES & SEALANTS INDUSTRY (ASI), Vol. 20, N° 8 (08/2013)
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Titre : Bonding composites : from performance to fashion Type de document : texte imprimé Auteurs : Laurie Gibbons, Auteur Année de publication : 2013 Article en page(s) : p. 30-32 Langues : Américain (ame) Catégories : Adhésifs -- Séchage sous rayonnement ultraviolet
Automobiles -- Matériaux
Avions -- Matériaux
Bateaux -- Matériaux
Colles:Adhésifs
Composites -- Collage
Entretien et réparations
Epoxydes
Méthacrylate de méthyle
Réticulation (polymérisation)
UrethanesIndex. décimale : 668.3 Adhésifs et produits semblables Résumé : Composite materials, including carbon fiber, are often preferred over conventional materials such as metal because they are lightweight, versatile and resilient. Carbon fiber is increasingly preferred for its traditional composite features and benefits and—as the latest fashion trends show — its fantastic finished appearance. Composite materials can be used to make not only a catwalk, but designer accessories as well.
The use of composite materials is particularly prevalent in the aerospace and transportation market sector because composites offer high-strength performance while keeping component weight down, thereby enabling better fuel efficiency and improved performance. Adhesive bonding of these composites offers many benefits and is widely accepted.
Unlike mechanical fasteners, adhesives maintain the composite material’s structure by eliminating the need to drill holes or puncture the composite. An adhesive bond can unitize the two pieces so they will not rattle or vibrate independently, which leads to fatigue. Adhesives further contribute to weight reduction because they simply weigh less than mechanical fasteners. In addition, adhesives provide a seam-free, perfect aesthetic finish, so products can be color-matched to the substrate material.Note de contenu : - BONDING SYSTEMS : Methyl methacrylates - Surface-activated methyl methacrylates - Modified epoxies/MS polymers - Two-component urethanes
- COMPOSITES ADVANCEMENTS : Cyanoacrylates - Two-component, no-mix systems - Epoxies
- COMPOSITES IN FASHIONEn ligne : http://www.adhesivesmag.com/articles/92176-bonding-composites-from-performance-t [...] Format de la ressource électronique : Web Permalink : https://e-campus.itech.fr/pmb/opac_css/index.php?lvl=notice_display&id=19260
in ADHESIVES & SEALANTS INDUSTRY (ASI) > Vol. 20, N° 8 (08/2013) . - p. 30-32[article]Réservation
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Code-barres Cote Support Localisation Section Disponibilité 15389 - Périodique Bibliothèque principale Documentaires Disponible
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Titre : Bonding the friendly skies : United airlines bonds torlon inserts in aircraft floor panels with vantico polyurethane Type de document : texte imprimé Année de publication : 2002 Article en page(s) : p. 51 Langues : Américain (ame) Catégories : Avions -- Matériaux
Colles:Adhésifs
Composites -- Collage
PolyuréthanesIndex. décimale : 668.3 Adhésifs et produits semblables Note de contenu : Bonding history
Insert pottingEn ligne : https://drive.google.com/file/d/1TYlODy1BdC7-xy1CLaylddGUnXxQE8IX/view?usp=drive [...] Format de la ressource électronique : Permalink : https://e-campus.itech.fr/pmb/opac_css/index.php?lvl=notice_display&id=19990
in ADHESIVES AGE > Vol. 45, N° 2 (02/2002) . - p. 51[article]Réservation
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Code-barres Cote Support Localisation Section Disponibilité 001468 - Périodique Bibliothèque principale Documentaires Disponible Butt-joined, thermoplastic stiffened-skin concept development / A. Offringa in SAMPE JOURNAL, Vol. 48, N° 2 (03-04/2012)
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Titre : Butt-joined, thermoplastic stiffened-skin concept development Type de document : texte imprimé Auteurs : A. Offringa, Auteur ; J. W. van Ingen, Auteur ; A. Buitenhuis, Auteur Année de publication : 2012 Article en page(s) : p. 7-15 Note générale : Bibliogr. Langues : Américain (ame) Catégories : Avions -- Fuselage
Avions -- Matériaux
Composites à fibres de carbone
Composites thermoplastiques
Joint d'about
Polyéthers cétone cétone
Polymères hautes performances
ThermodurcissablesIndex. décimale : 668.4 Plastiques, vinyles Résumé : A novel thermoplastic skin concept, with co-consolidated stringers, is being brought to technology readiness level (TRL) 6. This implies manufacturing and mechanical testing of full scale demonstrator products. The stringers are T-shaped and made of flat preforms that are butt jointed to each other and to the panel skin. An injection molded filler increases strength. The skin is fiber placed over the stringer preforms and the product is co-consolidated at melt temperature. Because of the butt-joints, manufacturing is relatively simple. The result is a tough thermoplastic product that can compete on weight and cost with state-of-the-art thermoset composite panels. Development and testing of the panel concept is being done in a step-by-step process. Consecutive building blocks are: coupons, three-stringer subcomponent panels and finally full scale skin panels. The main panel represents the mid-section of a business jet horizontal tail. The panel will be assembled into a 12 meter span torsion box and tested in the second half of 2011. Note de contenu : - INTRODUCTION : General - Current thermoplastic composite applications - Thermoplastic growth potential
- LARGE THERMOPLASTIC STRUCTURES : Current state-of-the-art thermoset panels - First large thermoplastic structures and discovery of the thermoplastic butt-joint - Butt joint research up to a panel concept - The TAPAS Project and the Road to TRL6 - Design of the torsion box demonstrator
- SKIN PANEL DEVELOPMENT : Stringer design and development - Skin design, development and manufacture - Cost modeling
- FULL SCALE TESTINGPermalink : https://e-campus.itech.fr/pmb/opac_css/index.php?lvl=notice_display&id=13604
in SAMPE JOURNAL > Vol. 48, N° 2 (03-04/2012) . - p. 7-15[article]Réservation
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Code-barres Cote Support Localisation Section Disponibilité 13702 - Périodique Bibliothèque principale Documentaires Disponible Caractérisation a-case et décapage chimique / Yves Marcel in GALVANO ORGANO, N° 785 (06-07/2009)
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Titre : Caractérisation a-case et décapage chimique Type de document : texte imprimé Auteurs : Yves Marcel, Auteur Année de publication : 2009 Article en page(s) : p. 32-33 Langues : Français (fre) Catégories : Avions -- Matériaux
Caractérisation
Composites à fibres de carbone
Titane -- DécapageIndex. décimale : 669.9 Métallurgie physique et chimique Résumé : Les exigences pour construire des avions plus économiques et respectueux de l'environnement ont contribué à la généralisation de matériaux légers et hautes performances comme les composites à fibre de carbone par exemple. Compte tenu de son excellente compatibilité thermique et mécanique avec les structures composites, le titane est de plus en plus utilisé. Permalink : https://e-campus.itech.fr/pmb/opac_css/index.php?lvl=notice_display&id=5995
in GALVANO ORGANO > N° 785 (06-07/2009) . - p. 32-33[article]Réservation
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Code-barres Cote Support Localisation Section Disponibilité 011472 - Périodique Bibliothèque principale Documentaires Disponible Carbon fibers with uniform porous structure using block copolymers in CHEMICAL FIBERS INTERNATIONAL, (10/2019)
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Titre : Carbon fibers with uniform porous structure using block copolymers Type de document : texte imprimé Année de publication : 2019 Article en page(s) : p. 34-35 Note générale : Bibliogr. Langues : Anglais (eng) Catégories : Avions -- Matériaux
Composites à fibres de carbone
Copolymères séquencés
Fibres de carbone
Matériaux -- Allègement
Matériaux poreux
Propulsion par réactionIndex. décimale : 677.4 Textiles artificiels Résumé : Researchers at the Virginia Tech's College of Science, Blacksburg, VA/USA, may have discovered a path toward powering planes and cars using energy stored in their exterior shells using porous carbon fibers made from block copolymers.
Carbon fibers, already known as a high-per-forming engineering material, are widely used in the aerospace and automotive industries. One application is the shells of luxury cars like Mercedes-Benz, BMW, or Lamborghini.
Carbon fibers, thin hair-like strands of car-bon, possess multiple prime material properties : they are mechanically strong, chemically resistant, electrically conductive, fire-retardant and perhaps most importantly, lightweight. The weight of carbon fibers improves fuel and energy efficiency, producing faster jets and vehiclesNote de contenu : - Designing materials for structure and function
- Using block copolymers to create porous carbon fibers
- New possibilities in energy storage
- Fig. 1 : Conventional and new methods for synthesizing carbon fibers from various polymer precursors
- Fig. 2 : Images from a scanning electron microscope (SEM) of carbon fibers made from PAN, PAN/PMMA, and PAN-b-PM¬MA. PAN-b-PMMA was used to create carbon fibers with more uniformly sized and spaced poresEn ligne : https://drive.google.com/file/d/1Mfp1ReWauCvITgIuHivo9cTYad1QL994/view?usp=drive [...] Format de la ressource électronique : Permalink : https://e-campus.itech.fr/pmb/opac_css/index.php?lvl=notice_display&id=33079
in CHEMICAL FIBERS INTERNATIONAL > (10/2019) . - p. 34-35[article]Réservation
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Code-barres Cote Support Localisation Section Disponibilité 21255 - Périodique Bibliothèque principale Documentaires Disponible Ceramic matrix composite jet engine exhaust / Yann Richard in JEC COMPOSITES MAGAZINE, N° 89 (05/2014)
PermalinkChallenges for a greener aircraft / Rocio Ruiz Gallardo in JEC COMPOSITES MAGAZINE, N° 124 (10/2018)
PermalinkLa chimie en Région Midi-Pyrénées (dossier) / Société Française de Chimie in L'ACTUALITE CHIMIQUE, N° 392 (01/2015)
PermalinkClosing the loop for the thermoplastic composites / Falk Ansorge in JEC COMPOSITES MAGAZINE, N° 112 (04-05/2017)
PermalinkComposite casing with embedded sensors for aircraft battery applications / Sophie Mahé in JEC COMPOSITES MAGAZINE, N° 149 (01-02/2023)
PermalinkComposite patch repair of sandwich structures with cracked face sheets / M. M. Ratwani in SAMPE JOURNAL, Vol. 49, N° 4 (07-08/2013)
PermalinkPermalinkLes composites creusent leur sillon / Pauline Léna in PLASTIQUES & CAOUTCHOUCS MAGAZINE, N° 847 (04/2007)
PermalinkComputed laminography - production-integrated inspection of large-scale CFRP components / Sébastien Papin in JEC COMPOSITES MAGAZINE, N° 114 (07/2017)
PermalinkComputer-aided engineering (CAE) technology applicable to the aerospace industry / Shan Nageswaran in JEC COMPOSITES MAGAZINE, N° 89 (05/2014)
PermalinkConcurrent processing of lay-up tasks / Axel Rieckmann in JEC COMPOSITES MAGAZINE, N° 52 (10/2009)
PermalinkCost-effective, phase-based thermography method for ultrasonic investigation of defects in CFRP structure in SAMPE JOURNAL, Vol. 47, N° 6 (11-12/2011)
PermalinkCost modelling of composite structure / Mathilda Karlsson Hagnell in JEC COMPOSITES MAGAZINE, N° 96 (04/2015)
PermalinkCustomized solutions for laser-assisted tape placement / Christian Brecher in JEC COMPOSITES MAGAZINE, N° 76 (10-11/2012)
PermalinkCutting, kitting and assembly of composite materials / Yvonne Heinen-Foudeh in JEC COMPOSITES MAGAZINE, N° 47 (03-04/2009)
PermalinkDate Palm fibre composites / Mohamad Midani in JEC COMPOSITES MAGAZINE, N° 112 (04-05/2017)
PermalinkLe défi du fuselage en composites / Bertrand Florentz in PLASTIQUES & CAOUTCHOUCS MAGAZINE, N° 911 (04/2014)
PermalinkA demountable composite wing box for private planes / Nicolas Vetel in JEC COMPOSITES MAGAZINE, N° 119 (03/2018)
PermalinkDesigning for damage tolerance / Andrew T. Rhead in JEC COMPOSITES MAGAZINE, N° 88 (04/2014)
PermalinkDeveloping a carbon fibre hybrid fuselage for multifunctional purposes / Yosif Golfman in JEC COMPOSITES MAGAZINE, N° 97 (05-06/2015)
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