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| rdf:type
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| rdfs:seeAlso
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| Description
| - Fibre Reinforced Plastics (FRP) used in aerospace industry successfully replace classic metal materials mainly in the components especially where the require is to save the weight while maintaining strength, but with much higher material – production costs in comparison to metal production. Thus efforts to reduce the manufacturing costs of composite structural parts is one of the major objectives of the current aerospace industry. The desire for increasing of production and increasing of efficiency of aerospace manufacturing processes leads primarily to use of composite materials based on high - tech thermoplastics, which are relatively new in primar aircraft structures. The usage and the contribution of the thermoplastic composites in aircraft structures is growing year by year and also at the expense of thermoset composites. That is the purpose why the forming technologies for manufacturing of these materials are still developing and improving in order to be more efficient with lower costs. Parts for structural applications are nowadays produced from carbon or glass fabrics which are pre-impregnated by the high-tech matrixes such as PPS, PEI and PEEK. Matrixes PPS and PEI are primarily intended like a substitution for thermoset matrixes mainly due to their lower costs in comparison with PEEK matrix. Nevertheless these thermoplastics are not able up to now replace thermoset matrixes in all kinds of applications. Thermoforming technology is one of the most progressive technologies used for manufacturing of structural composite parts which are based generally on thermoplastic matrixes. Research of the influence of release agents on thermoforming technology will be performed entirely with the multiply CF/PPS material which is currently the most widespread material for the manufacturing of structural parts for aerospace applications.
- Fibre Reinforced Plastics (FRP) used in aerospace industry successfully replace classic metal materials mainly in the components especially where the require is to save the weight while maintaining strength, but with much higher material – production costs in comparison to metal production. Thus efforts to reduce the manufacturing costs of composite structural parts is one of the major objectives of the current aerospace industry. The desire for increasing of production and increasing of efficiency of aerospace manufacturing processes leads primarily to use of composite materials based on high - tech thermoplastics, which are relatively new in primar aircraft structures. The usage and the contribution of the thermoplastic composites in aircraft structures is growing year by year and also at the expense of thermoset composites. That is the purpose why the forming technologies for manufacturing of these materials are still developing and improving in order to be more efficient with lower costs. Parts for structural applications are nowadays produced from carbon or glass fabrics which are pre-impregnated by the high-tech matrixes such as PPS, PEI and PEEK. Matrixes PPS and PEI are primarily intended like a substitution for thermoset matrixes mainly due to their lower costs in comparison with PEEK matrix. Nevertheless these thermoplastics are not able up to now replace thermoset matrixes in all kinds of applications. Thermoforming technology is one of the most progressive technologies used for manufacturing of structural composite parts which are based generally on thermoplastic matrixes. Research of the influence of release agents on thermoforming technology will be performed entirely with the multiply CF/PPS material which is currently the most widespread material for the manufacturing of structural parts for aerospace applications. (en)
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| Title
| - Influence of mould surface preparation on C/PPS thermoforming technology
- Influence of mould surface preparation on C/PPS thermoforming technology (en)
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| skos:prefLabel
| - Influence of mould surface preparation on C/PPS thermoforming technology
- Influence of mould surface preparation on C/PPS thermoforming technology (en)
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| skos:notation
| - RIV/68407700:21220/14:00219781!RIV15-MSM-21220___
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| http://linked.open...avai/riv/aktivita
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| http://linked.open...avai/riv/aktivity
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| http://linked.open...vai/riv/dodaniDat
| |
| http://linked.open...aciTvurceVysledku
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| http://linked.open.../riv/druhVysledku
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| http://linked.open...iv/duvernostUdaju
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| http://linked.open...titaPredkladatele
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| http://linked.open...dnocenehoVysledku
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| http://linked.open...ai/riv/idVysledku
| - RIV/68407700:21220/14:00219781
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| http://linked.open...riv/jazykVysledku
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| http://linked.open.../riv/klicovaSlova
| - Tribology; Release Agent; Composite; Thermoforming; PPS; Thermoplastics; Aerospace (en)
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| http://linked.open.../riv/klicoveSlovo
| |
| http://linked.open...ontrolniKodProRIV
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| http://linked.open...v/mistoKonaniAkce
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| http://linked.open...i/riv/mistoVydani
| |
| http://linked.open...i/riv/nazevZdroje
| - Proceedings of International Conference on Innovative Technologies IN-TECH 2014
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| http://linked.open...in/vavai/riv/obor
| |
| http://linked.open...ichTvurcuVysledku
| |
| http://linked.open...cetTvurcuVysledku
| |
| http://linked.open...UplatneniVysledku
| |
| http://linked.open...iv/tvurceVysledku
| - Kudláček, Jan
- Roškanin, Petr
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| http://linked.open...vavai/riv/typAkce
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| http://linked.open.../riv/zahajeniAkce
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| issn
| |
| number of pages
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| http://purl.org/ne...btex#hasPublisher
| - Faculty of Engineering University of Rijeka
|
| http://localhost/t...ganizacniJednotka
| |
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