dc.contributor.author | Fojtl, Ladislav | |
dc.contributor.author | Rusnáková, Soňa | |
dc.contributor.author | Žaludek, Milan | |
dc.contributor.author | Rusnák, Vladimír | |
dc.date.accessioned | 2015-09-25T07:09:18Z | |
dc.date.available | 2015-09-25T07:09:18Z | |
dc.date.issued | 2015 | |
dc.identifier.citation | Materiali in Tehnologije. 2015, vol. 49, issue 4, p. 515-519. | cs |
dc.identifier.issn | 1580-2949 | |
dc.identifier.issn | 1580-3414 | |
dc.identifier.uri | http://hdl.handle.net/10084/110483 | |
dc.description | nefunkční DOI | cs |
dc.description.abstract | This research paper deals with an investigation of the flexural properties measured in a three-point bending test depending on
the type and number of the E-glass prepreg layers applied to the facing sides of the resulting sandwich structure used for floor
panels in the transport industry. The values of the low-cycle fatigue were measured according to the values of the flexural
strength obtained from the static test. Cycling was performed at (70, 60 and 50) % values of the ultimate flexural load.
Moreover, a decrease in the flexural strength and stiffness depending on the number of cycles was also studied. For the
production of samples, one type of aluminum honeycomb core and various phenolic prepregs with different numbers of layers
were used. These samples were produced with two, in practice commonly used methods – compression molding and vacuum
bagging. The measured results show that the production technology has a certain influence on the mechanical behavior in
bending and the fatigue life of sandwich structures. The experimental results proved that the type of prepreg (defined by the
reinforcing fabric and the amount of resin) and the number of layers also affect the properties of these structures. All the
obtained results provide useful information for designing the sandwich structures for the transport industry. | cs |
dc.format.extent | 326576 bytes | |
dc.format.mimetype | application/pdf | |
dc.language.iso | en | cs |
dc.publisher | Inštitut za kovinske materiale in tehnologije | cs |
dc.relation.ispartofseries | Materiali in Tehnologije | cs |
dc.relation.uri | http://mit.imt.si/Revija/izvodi/mit154/fojtl.pdf | cs |
dc.title | Influence of the type and number of prepreg layers on the flexural strength and fatigue life of honeycomb sandwich structures | cs |
dc.title.alternative | Vpliv vrste in števila plasti na utrditev upogibne trdnosti in zdržljivosti pri utrujanju satastih
sendvičnih konstrukcij | cs |
dc.type | article | cs |
dc.description.abstract-en | Članek obravnava preiskave lastnosti pri upogibu, izmerjene s trito~kovnim upogibnim preizkusom, v odvisnosti od vrste in
{tevila plasti E-stekla na utrditev, uporabljenih na ~elni strani sendvi~nih konstrukcij, ki se uporabljajo v transportu za talne
plo{~e. Vrednosti malocikli~ne utrujenosti so bile izmerjene skladno z vrednostmi upogibne trdnosti, dobljenimi pri stati~nem
preizkusu. Cikli~no obremenjevanje je bilo izvr{eno pri (70, 60 in 50) % vrednosti upogibne trdnosti. Poleg tega je bilo
preu~evano tudi zmanj{anje upogibne trdnosti in togosti v odvisnosti od {tevila ciklov. Za pripravo vzorcev je bila uporabljena
ena vrsta sataste osnove iz aluminija in razli~ne fenolne plasti za utrjenje z razli~nim {tevilom plasti. Ti vzorci so bili izdelani z
dvema obi~ajnima metodama – s tla~nim litjem in vakuumskim pakiranjem. Izmerjeni rezultati ka`ejo, da ima tehnologija
izdelave dolo~en vpliv na mehansko vedenje pri upogibanju in utrujanju sendvi~nih konstrukcij. Rezultati eksperimentov so
pokazali, da vrsta plasti za utrjanje (dolo~ena s tkanino za utrjanje in koli~ino smole) in {tevilo plasti tudi vplivata na lastnosti
teh konstrukcij. Vsi dobljeni rezultati zagotavljajo koristne informacije za konstruiranje sendvi~nih konstrukcij v transportni
industriji. | cs |
dc.identifier.doi | 10.17222/mit.2014.124 | |
dc.rights.access | openAccess | |
dc.type.version | publishedVersion | |
dc.type.status | Peer-reviewed | cs |
dc.description.source | Web of Science | cs |
dc.description.volume | 49 | cs |
dc.description.issue | 4 | cs |
dc.description.lastpage | 519 | cs |
dc.description.firstpage | 515 | cs |
dc.identifier.wos | 000358560800006 | |