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Thermoplastic composites for the building industry / Justin Jin in JEC COMPOSITES MAGAZINE, N° 120 (04/2018)
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Titre : Thermoplastic composites for the building industry Type de document : texte imprimé Auteurs : Justin Jin, Auteur Année de publication : 2018 Article en page(s) : p. 32-35 Langues : Anglais (eng) Catégories : Composites thermoplastiques
Habitations -- Conception et construction
Impression tridimensionnelle
Matières plastiques dans la construction
StratifiésIndex. décimale : 668.4 Plastiques, vinyles Résumé : The building sector contributes about 30% of the global annual greenhouse gas emissions and consumes up to 40% of all energy. This means the more we build houses, the worse, the environmental situation becomes.
From the beginning, Axia Materials Co., Ltd. has been developing new solutions to meet these conflicting goals with new materials and processes. The Pixel Haus uses the company's innovative LiteTex thermoplastic composite and LitePan laminate panel system, changing the building industry's paradigm from "constructing houses" to "making houses".Note de contenu : - Hybrid house system in Jeju Island
- Energy-efficient project in Kuwait
- Gable roof house
Figures and tables : Litetex and litePreg are produced in a continuous way. LitePan is a product laminated with LiteTex - Smlke fire toxicity (SFT) summary - Products for various applicationsPermalink : https://e-campus.itech.fr/pmb/opac_css/index.php?lvl=notice_display&id=30650
in JEC COMPOSITES MAGAZINE > N° 120 (04/2018) . - p. 32-35[article]Réservation
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Code-barres Cote Support Localisation Section Disponibilité 19778 - Périodique Bibliothèque principale Documentaires Disponible 19779 - Périodique Bibliothèque principale Documentaires Disponible Thermoplastic composites set to fly high in aerospace / Aditya Joshi in JEC COMPOSITES MAGAZINE, N° 128 (05-06/2019)
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Titre : Thermoplastic composites set to fly high in aerospace Type de document : texte imprimé Auteurs : Aditya Joshi, Auteur Année de publication : 2019 Article en page(s) : p. 32-34 Langues : Anglais (eng) Catégories : Aéronautique
Avions -- Matériaux
Composites à fibres de carbone
Composites thermoplastiques
Economies d'énergie
Matériaux -- AllègementIndex. décimale : 668.4 Plastiques, vinyles Résumé : In the aerospace industry, structural performance is becoming synonymous with ecology. Fuel costs represent the highest of all the operating costs of an aircraft. Unsurprisingly, the industry is mustering efforts to reduce the weight of aircraft, which has a direct impact on airline economics and on the environment. In passenger aircraft, every kilogram of weight reduction counts. Estimates suggest that a weight reduction of 100 kg in an average airliner results in a yearly fuel saving of about 19000 litres, thereby reducing CO2 emissions. Therefore, the use of lightweight, high-strength materials has become essential for high-end applications in the aviation industry. Note de contenu : - We are set to witness a new begining
- The aerospace thermoplastic composites market is taking off
- Carbon composites clocking the highest tonnage
- Commercial aviation giants make Europe and North America the go-to markets
- The industry is gearing up for the growing opportunity
- Fig. 1 : Aerospace & defence thermoplastic composites market to reach US$ 636 million in 2023
- Fig. 3 : Penetration of composite materials in different aircraft (% of total structural weight)
- Fig. 2 : Key applications of thermoplastic compositesPermalink : https://e-campus.itech.fr/pmb/opac_css/index.php?lvl=notice_display&id=32534
in JEC COMPOSITES MAGAZINE > N° 128 (05-06/2019) . - p. 32-34[article]Réservation
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Code-barres Cote Support Localisation Section Disponibilité 20914 - Périodique Bibliothèque principale Documentaires Disponible Thermoplastic composites technologies for manufacturing nose fuselage structures / P. Lefebure in SAMPE JOURNAL, Vol. 49, N° 5 (09-10/2013)
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Titre : Thermoplastic composites technologies for manufacturing nose fuselage structures Type de document : texte imprimé Auteurs : P. Lefebure, Auteur ; J.-M. Guimard, Auteur Année de publication : 2013 Article en page(s) : p. 32-41 Note générale : Bibliogr. Langues : Américain (ame) Catégories : Avions -- Fuselage
Avions -- Matériaux
Chauffage laser
Composites thermoplastiques
Composites thermoplastiques -- Propriétés mécaniques
Métallisation
Résistance au chocs
SoudageIndex. décimale : 668.4 Plastiques, vinyles Résumé : In the framework of the French national DPAC COMP TP (Thermoplastic) Program, EADS IW has continued its long term efforts on the development of thermoplastic composites technologies for aeronautics structural applications. Most of the research and development activities were focused on the manufacture of "nase" fuselage parts, such as skin panels and stringers and (or) frames, and on the development of TP welding processes. Aircraft windshield front fairings were estimated as good candidates for thermoplastics technologies among all the aeronautic nase fuselage parts. Therefore this paper will discuss the recent developments led by EADS IW, for manufacturing a technological demonstrator, whose main specifications are:
- Thick part (compared to fuselage skins thicknesses) for potential impact resistance properties
- Geometry with severe double curvatures
- Use of cost-effective manufacturing processes
These specifications led to a development program that encompassed the following activities:
- Determination and validation of process limits for TP parts consolidation in aven.
- Automated lay down technique for TP multi-tows deposition with a laser heating system.
- Panel metallization, for LSP application, with a laser TP tape deposition machine.
- Press-forming process for manufacture of thick and double curvature stiffeners.
- Specific welding process and understanding the mixing of different high performance thermoplastic materials.
A specific design of a representative Thermoplastic CFRC Panel has been created and the associated technological demonstrator is manufactured for validation of the different related development works. Mechanical performance, detailed structural sizing and actual impact resistance of such a component will be addressed at a later date in another development program.Note de contenu : - AUTOMATED TP FIBRE PLACEMENT PROCESS WITH LASER HEATING SYSTEM
- HARMFUL IMPACT OF THE POROSITY IN THERMOPLASTIC COMPOSITE PARTS
- CONSOLIDATION OF PROUS LAMINATES
- MECHANICAL TESTS : FHC (Filled Hole Compression) tests - After impact compression tests
- METALLIZATION OF LARGE CURVED TP CFRC PANELS
- INFLUENCE OF AN AUTOMATED DEPOSITION PROCESS ON LIGHTNING STRIKE BEHAVIOUR
- TECHNOLOGY ADAPTATION TO A MULTI-TOW PLACEMENT MACHINE WITH LASER HEATING SYSTEM
- EADS IW TECHNOLOGICAL DEMONSTRATOR :Part design - Skin manufacture - Frames manufacture - Skin-frames welding feasibilityPermalink : https://e-campus.itech.fr/pmb/opac_css/index.php?lvl=notice_display&id=19270
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Code-barres Cote Support Localisation Section Disponibilité 15385 - Périodique Bibliothèque principale Documentaires Disponible Thermoplastic material toolbox in JEC COMPOSITES MAGAZINE, N° 102 (01-02/2016)
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Titre : Thermoplastic material toolbox Type de document : texte imprimé Année de publication : 2016 Langues : Anglais (eng) Catégories : Bandes composites
Composites à fibres de carbone
Composites à fibres longues
Composites thermoplastiques
Fibres à orientation unidirectionnelle
Matériaux -- Allègement
Matières plastiques dans les automobilesIndex. décimale : 668.4 Plastiques, vinyles Résumé : In the future, lightweight design will become more important for ecological and sustainable mobility due to the shortage of resources, especially fossil fuels. Therefore, new design concepts and high-performance materials like carbon fibre-reinforced polymers (CFRP) are required. In addition to these ecological challenges, the economic constraints of global of global markets have to be taken into account as well. There is still a high demand on cost-efficient materials, especially when it comes to high-volume production, to enable profitable processes. Note de contenu : - Carbon fibre-reinforced thermoplastics
- Customized sizing technologies
- Unidirectional tapes
- Organic sheets
- Long fibre-reinforced thermoplastics (LFT)
- Application examplePermalink : https://e-campus.itech.fr/pmb/opac_css/index.php?lvl=notice_display&id=25434
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Code-barres Cote Support Localisation Section Disponibilité 17764 - Périodique Bibliothèque principale Documentaires Disponible Thermoplastics in aerospace applications / Stéphanie Patel in JEC COMPOSITES MAGAZINE, N° 151 (06-07/2023)
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Titre : Thermoplastics in aerospace applications : how Daher stays one step ahead with CARAC TP Type de document : texte imprimé Auteurs : Stéphanie Patel, Auteur ; Charles Naejus, Auteur ; Martin Denize, Auteur Année de publication : 2023 Article en page(s) : p. 47-50 Langues : Anglais (eng) Catégories : Avions -- Matériaux
Composites à fibres -- Propriétés mécaniques
Composites thermoplastiques
Fibres continues
Hautes températures
Polyaryl éther cétones
Résistance au chocs
Résistance au fluageIndex. décimale : 668.4 Plastiques, vinyles Résumé : CARAC TP project was established to furnish in-depth knowledge on continuous fibre thermoplastic materials, and consolidates the company's lead in the use of these materials for aerospace applications. Results from CARAC TP will be applied to a broad range of uses at high temperature (up to a constant one 170°C), and to better control forming processes. This project was conducted in partnership with specialised composite materials laboratories. The results were partly presented at the 2022 SAMPE France event. Note de contenu : - Defining the process window : Controlling crystallisation - Studying degradation
- Resistance to the environment
- Resistance to creep, fatigue, and impact
- Fig. 1 Daher's CARAC TP project approach
- Fig. 2 : Example of DSC curves with different cooling rates
- Fig. 3 : TTT diagram of isothermal and anisothermal conditions
- Fig. 4 : DSC analysis after exposure to temperatures higher than the melting temperature for different times
- Fig. 5 : Example of analysis of material after time/temperature exposure : mass loss bending modulus evolution
- Fig. 6 : Visual observation and chemical analysis on material after UV exposure
- Fig. 7 : Observation on panels fire exposure, UD thermoplastic family and UD thermoset family
- Fig. 8 : Tensile static test results onf QI stacking at room temperature, 120°C ande 170°C
- Fig. 9 : Example of fatigue diagram, tensile mode, QI stacking at room temperature, 120°C and 170°C
- Fig. 10 : Type of deformation after creeping, soft stacking, maintaining tensile load for 6 hours at 170°C
- Fig. 11 : Picture taken by a thermal camera during impact test at elevated temperature : tomography of a sample after impactEn ligne : https://drive.google.com/file/d/1hGQCQa8e-ZGyuz5vz39Co49sBoL8h2rV/view?usp=drive [...] Format de la ressource électronique : Permalink : https://e-campus.itech.fr/pmb/opac_css/index.php?lvl=notice_display&id=40221
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Code-barres Cote Support Localisation Section Disponibilité 24088 - Périodique Bibliothèque principale Documentaires Disponible Du thermoplastique dans les volants / Ankit Garg in PLASTIQUES & CAOUTCHOUCS MAGAZINE, N° 855 (02-03/2008)
PermalinkThermoset composite resin matrices / Scott W. Beckwith in SAMPE JOURNAL, Vol. 48, N° 6 (11-12/2012)
PermalinkThree-dimensional simulation of capillary rheometry for an estimation of extensional viscosity / Huan-Chang Tseng in INTERNATIONAL POLYMER PROCESSING, Vol. 38, N° 2 (2023)
PermalinkUn triangle de suspension en composite in GALVANO ORGANO, N° 820 (05/2013)
PermalinkTwin-O-Sheet / Dietmar Drummer in JEC COMPOSITES MAGAZINE, N° 89 (05/2014)
PermalinkVariety of lightweight construction processes / Josef Renkl in KUNSTSTOFFE INTERNATIONAL, Vol. 105, N° 9 (09/2015)
PermalinkVol. 21, N° 3 - 09-10-11-12/2011 - Composites haute performance pour applications aéronautiques (Bulletin de REVUE DES COMPOSITES ET DES MATERIAUX AVANCES) / Jacques Renard
PermalinkVol. 9, N° Hors série - 1999 - Les matériaux composites à base de bois (Bulletin de REVUE DES COMPOSITES ET DES MATERIAUX AVANCES) / Pierre Morlier
PermalinkWeight reduction with composites / Karl-Heinz Kalmbach in JEC COMPOSITES MAGAZINE, N° 45 (11-12/2008)
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