<?xml version="1.0" encoding="ISO-8859-1"?><article xmlns:mml="http://www.w3.org/1998/Math/MathML" xmlns:xlink="http://www.w3.org/1999/xlink" xmlns:xsi="http://www.w3.org/2001/XMLSchema-instance">
<front>
<journal-meta>
<journal-id>0870-8312</journal-id>
<journal-title><![CDATA[Ciência & Tecnologia dos Materiais]]></journal-title>
<abbrev-journal-title><![CDATA[C.Tecn. Mat.]]></abbrev-journal-title>
<issn>0870-8312</issn>
<publisher>
<publisher-name><![CDATA[Sociedade Portuguesa de Materiais]]></publisher-name>
</publisher>
</journal-meta>
<article-meta>
<article-id>S0870-83122007000100003</article-id>
<title-group>
<article-title xml:lang="en"><![CDATA[Development of a new generation of filament of wound composite pressure cylinders]]></article-title>
</title-group>
<contrib-group>
<contrib contrib-type="author">
<name>
<surname><![CDATA[Velosa]]></surname>
<given-names><![CDATA[J. C.]]></given-names>
</name>
<xref ref-type="aff" rid="A01"/>
</contrib>
<contrib contrib-type="author">
<name>
<surname><![CDATA[Nunes]]></surname>
<given-names><![CDATA[J. P.]]></given-names>
</name>
<xref ref-type="aff" rid="A01"/>
</contrib>
<contrib contrib-type="author">
<name>
<surname><![CDATA[Antunes]]></surname>
<given-names><![CDATA[P. J.]]></given-names>
</name>
<xref ref-type="aff" rid="A01"/>
</contrib>
<contrib contrib-type="author">
<name>
<surname><![CDATA[Silva]]></surname>
<given-names><![CDATA[J. F.]]></given-names>
</name>
<xref ref-type="aff" rid="A02"/>
</contrib>
<contrib contrib-type="author">
<name>
<surname><![CDATA[Marques]]></surname>
<given-names><![CDATA[A. T.]]></given-names>
</name>
<xref ref-type="aff" rid="A03"/>
</contrib>
</contrib-group>
<aff id="A01">
<institution><![CDATA[,Minho University Polymer Engineering Department ]]></institution>
<addr-line><![CDATA[Guimarães ]]></addr-line>
<country>Portugal</country>
</aff>
<aff id="A02">
<institution><![CDATA[,Institito Politécnico do Porto ISEP - Instituto Superior de Engenharia do Porto Departamento de Engenharia Mecânica]]></institution>
<addr-line><![CDATA[Porto ]]></addr-line>
<country>Portugal</country>
</aff>
<aff id="A03">
<institution><![CDATA[,Universidade do Porto FEUP - Faculdade de Engenharia do Porto DEMEGI-INEGI]]></institution>
<addr-line><![CDATA[Leça do Balio ]]></addr-line>
<country>Portugal</country>
</aff>
<pub-date pub-type="pub">
<day>00</day>
<month>01</month>
<year>2007</year>
</pub-date>
<pub-date pub-type="epub">
<day>00</day>
<month>01</month>
<year>2007</year>
</pub-date>
<volume>19</volume>
<numero>1-2</numero>
<fpage>8</fpage>
<lpage>13</lpage>
<copyright-statement/>
<copyright-year/>
<self-uri xlink:href="http://scielo.pt/scielo.php?script=sci_arttext&amp;pid=S0870-83122007000100003&amp;lng=en&amp;nrm=iso"></self-uri><self-uri xlink:href="http://scielo.pt/scielo.php?script=sci_abstract&amp;pid=S0870-83122007000100003&amp;lng=en&amp;nrm=iso"></self-uri><self-uri xlink:href="http://scielo.pt/scielo.php?script=sci_pdf&amp;pid=S0870-83122007000100003&amp;lng=en&amp;nrm=iso"></self-uri><abstract abstract-type="short" xml:lang="en"><p><![CDATA[A new generation of composite pressure vessels for large scale market applications has been studied in this work. The vessels consist on a thermoplastic liner wrapped with a filament winding glass fibre reinforced polymer matrix structure. A high density polyethylene (HDPE) was selected as liner and a thermosetting resin was used as matrices in the glass reinforced filament wound laminate. The Abaqus 6.5.1 FEM package were used to predict the mechanical behaviour of pressure vessels with capacity of approximately of 0,068 m³ (68 l) for a 0.6 MPa (6 bar) pressure service condition according to the requirements of the prEN 13923 standard, namely, the minimum internal burst pressure. The Tsai-Wu and Von Mises criteria were used to predict composite laminate and thermoplastic liner failures, respectively, considering the elasto-plastic behaviour of the HDPE liner and the laminae properties deducted from micromechanical models for composite laminates. Finally, prototype pressure vessels were produced in the defined conditions to be submitted to pressure tests. The comparison between the FEM simulations and experimental results are discussed in the present paper.]]></p></abstract>
</article-meta>
</front><body><![CDATA[ <p align="center"><b>Development of a new generation of filament of wound composite    pressure cylinders</b></p>     <p align="center">&nbsp;</p>     <p align="center">J. C. Velosa<sup>1</sup>, J. P. Nunes<sup>1</sup>, P. J. Antunes<sup>1</sup>,    J. F. Silva<sup>2</sup>, A. T. Marques<sup>3</sup></p>     <p align="center">&nbsp;</p>     <p align="center"><sup>1 </sup>Polymer Engineering Department, Minho University,    Campus de Azurém, 4800-058 Guimarães, Portugal</p>     <p align="center"><sup>2 </sup>Department of Mechanical Engineering, ISEP, 4200-072    Porto, Portugal</p>     <p align="center"><sup>3 </sup>DEMEGI-INEGI-FEUP, Universidade do Porto, 4465-591    Leça do Balio, Portugal</p>     <p align="center">&nbsp;</p>     <p align="center"><sup>1</sup>Email: <a href="mailto:jcvelosa@dep.uminho.pt">jcvelosa@dep.uminho.pt</a></p>      <p>&nbsp;</p>      ]]></body>
<body><![CDATA[<p>&nbsp;</p>      <p><b>ABSTRACT</b></p>      <p>A new generation of composite pressure vessels for large scale market applications has been studied in this work. The vessels consist on a thermoplastic liner wrapped with a filament winding glass fibre reinforced polymer matrix structure. A high density polyethylene (HDPE) was selected as liner and a thermosetting resin was used as matrices in the glass reinforced filament wound laminate. </p>      <p>The Abaqus 6.5.1 FEM package were used to predict the mechanical behaviour of pressure vessels with capacity of approximately of 0,068 m<sup>3</sup> <sup> </sup>(68 l) for a 0.6 MPa (6 bar) pressure service condition according to the requirements of the prEN 13923 standard, namely, the minimum internal burst pressure. The Tsai-Wu and Von Mises criteria were used to predict composite laminate and thermoplastic liner failures, respectively, considering the elasto-plastic behaviour of the HDPE liner and the laminae properties deducted from micromechanical models for composite laminates. </p>      <p>Finally, prototype pressure vessels were produced in the defined conditions to be submitted to pressure tests. The comparison between the FEM simulations and experimental results are discussed in the present paper.</p>      <p>&nbsp;</p>     <p>&nbsp;</p>      <p>Texto completo disponível apenas em PDF.</p>     <p>Full text only available in PDF format.</p>      <p>&nbsp;</p>     ]]></body>
<body><![CDATA[<p>&nbsp;</p>      <p><b>REFERENCES</b></p>      <!-- ref --><p>1    Brandt, J., Drechsler, K., Richter, H., “The Use of High-Performance Thermoplastic Composites for Structural Aerospace Applications”, <i>9th Int. Conference on Composite Materials (ICCM-9), </i>Vol. 6, Madrid, Spain (1993) 143-150.&nbsp;&nbsp;&nbsp;&nbsp;&nbsp;&nbsp;&nbsp;&nbsp;[&#160;<a href="javascript:void(0);" onclick="javascript: window.open('/scielo.php?script=sci_nlinks&ref=141234&pid=S0870-8312200700010000300001&lng=','','width=640,height=500,resizable=yes,scrollbars=1,menubar=yes,');">Links</a>&#160;]<!-- end-ref --><p>2    Won-Man, C., Bang-Eop, L., Song-Hoe, K., Young-Shin, L.  “Effects of Geometric    and Material Nonlinearity on The Stresses of Various Pressure Vessel Dome Shapes”    Computers &amp; Structures Vol. 55, No. 6 (1995) 1063-1075.</p>      <p>3    Kang, D.H., Kim, C.U., Kim, C.G. “The embedment of fiber Bragg grating    sensors into filament wound pressure tanks considering multiplexing” NDT&amp;E    Int., 39 (2006); 119-116.</p>      <p>4    Tsai, S.W., “Composites Design, Think Composites”, USA (1987).</p>      <p>5    Jones, R.M., “Mechanics of Composite Materials”, International Student    Edition, MacGraw-Hill Kogakusha Ltd, Tokyo (1975).</p>      <p>6    Saarela, O., “LAMDA-Laminate Design and Analysis”, Helsinki University of Technology”, Otaniemi, Finland (1992)</p>      <p> 7   Nunes, J. P., Bernardo, C. A., Pouzada, A. S. e Edie, D. D.<b>,</b> “Formation    and Characterisation of Carbon/Polycarbonate Towpregs and Composites”, Journal    of Composite Materials, Vol. 31 (17), USA (1997) 1758-1777.</p>      <p>8    Abaqus Documentation, Version 6.5.1, Hibbitt, Karlsson &amp; Sorensen Inc.</p>      ]]></body>
<body><![CDATA[<p>9    Antunes, P. J., Dias, G. R., Nunes, J. P., van Hattum,  F.W.J., Oliveira,    T. “FEM Analysis of Thermoplastic Matrix Composite Gas Cylinders ” Proceedings    of the 15th Int. Conference on Composite Materials- ICCM 15, 27 June-1 July,    Durban/South Africa, (2005).</p>       ]]></body><back>
<ref-list>
<ref id="B1">
<nlm-citation citation-type="">
<person-group person-group-type="author">
<name>
<surname><![CDATA[Brandt]]></surname>
<given-names><![CDATA[J.]]></given-names>
</name>
<name>
<surname><![CDATA[Drechsler]]></surname>
<given-names><![CDATA[K.]]></given-names>
</name>
<name>
<surname><![CDATA[Richter]]></surname>
<given-names><![CDATA[H.]]></given-names>
</name>
</person-group>
<article-title xml:lang="en"><![CDATA[The Use of High-Performance Thermoplastic Composites for Structural Aerospace Applications]]></article-title>
<source><![CDATA[9th Int. Conference on Composite Materials (ICCM-9)]]></source>
<year>1993</year>
<volume>6</volume>
<page-range>143-150</page-range><publisher-loc><![CDATA[Madrid ]]></publisher-loc>
</nlm-citation>
</ref>
</ref-list>
</back>
</article>
