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The effects of severe temperature changes and high humidity on porous CFRP

Wybrane pełne teksty z tego czasopisma
Identyfikatory
Warianty tytułu
Języki publikacji
EN
Abstrakty
EN
Purpose: A route to manufacture porous carbon fiber reinforced plastic (CFRP) for study purposes is described. Design/methodology/approach: The porous CFRP is characterized using standard techniques such as matrix digestion as well as the more sophisticated method of high resolution Microfocus X-Ray Tomography (μCT). A comparison of the results of those methods is presented. The mass gains of specimens with a wide range of porosity have been measured both in constant humidity and in alternating environments. Findings: It could be shown that severe temperature changes can temporarily increase the moisture content of porous CFRP. However, after the return to a constant environment, the moisture content returns back to saturation levels. Furthermore, it could be shown by X-Ray Tomography that even under severe climatic conditions no permanent liquid water condensates inside the pores. Research limitations/implications: Using Microfocus Computed Tomography it could be shown that even after nearly a year under hot-wet conditions and more than 150 severe temperature cycles there is no liquid water detectable inside the pores. Originality/value: In this paper the effects of severe temperature changes and high humidity on porous CFRP.
Rocznik
Strony
14--20
Opis fizyczny
Bibliogr. 11 poz., rys., tab.
Twórcy
autor
  • Wehrwissenschaftliches Institut für Werk- und Betriebsstoffe - WIWeB, Institutsweg 1, D-85435 Erding, Germany
autor
  • Ostbayerische Technische Hochschule Regensburg, Fakultät Maschinenbau, Galgenbergstr. 30, D-93053 Regensburg, Germany
Bibliografia
  • [1] M.L. Costa, M.C. Rezende, S. F. M. de Almeida, Strength of Hygrothermally Conditioned Polymer Composites with Voids, Journal of Composite Materials 39/21 (2005) 1943-1961.
  • [2] M.L. Costa, M.C. Rezende, S. F. M. de Almeida, Effect of Void Content on the Moisture Absorption in Polymeric Composites, Polymer-Plastics Technology and Engineering 45/6 (2006) 691-698.
  • [3] DIN EN 2565: Luft- und Raumfahrt- Herstellung von CFK-Prüflaminaten, Berlin: Normenstelle Luftfahrt (NL) im DIN Deutsches Institut für Normung e.V., Beuth Verlag, 1993.
  • [4] DIN EN 2564: Luft- und Raumfahrt - Kohlenstoffaser- Laminate: Bestimmung der Faser-, Harz- und Porenanteile. Berlin: Normenstelle Luftfahrt (NL) im DIN Deutsches Institut für Normung e.V., Beuth Verlag, 1998.
  • [5] H. Dinnebier, Detection of Various Types of Damage in CFRP using Computed Tomography, Proceedings of the NATO-AVT Workshop on Advanced Non-destructive Evaluation Techniques for Polymer Based Composites in Military Vehicles, Riga, Latvia, 2013.
  • [6] HexPly M18 – Epoxy Matrix – Product Data. Sheet, Hexcel Composites, 2007.
  • [7] L. Lin, M. Luo, H.T. Tian, X.M. Li, G.P. Guo, Experimental investigation on porosity of carbon fiber-reinforced composite using ultrasonic attenuation coefficient, Proceedings of the 17th World Conference on Nondestructive Testing, Shanghai, China, 2008.
  • [8] P. Oliver, J.P. Cottu, B. Ferret, Effects of cure cycle Pressure and voids on some mechanical properties of carbon/epoxy laminates, Composites 26/7 (1995) 509-515.
  • [9] V. Schmid, Untersuchung der künstlichen Herstellung und Analyse von Porositäten und Lufteinschlüssen in Probekörpern aus kohlenstofffaserverstärkten Kunststoffen, Wehrwissenschaftliches Institut für Werk- und Betriebsstoffe - WIWeB, Erding, 2010.
  • [10] C. Winter, Herstellung und Untersuchung poröser CFK-Proben, Wehrwissenschaftliches Institut für Werk- und Betriebsstoffe - WIWeB, Erding, 2010.
  • [11] J. Wolfrum, Long Term Behaviour of Porous Composite Material, WIWeB, 2014.
Typ dokumentu
Bibliografia
Identyfikator YADDA
bwmeta1.element.baztech-61b0b9ec-e18d-4018-aff4-da71187bcaab
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