<?xml version="1.0" encoding="UTF-8"?><xml><records><record><source-app name="Biblio" version="6.x">Drupal-Biblio</source-app><ref-type>47</ref-type><contributors><authors><author><style face="normal" font="default" size="100%">Wilson, M L</style></author><author><style face="normal" font="default" size="100%">MacConochie, Ian O.</style></author><author><style face="normal" font="default" size="100%">Johnson, G S</style></author></authors></contributors><titles><title><style face="normal" font="default" size="100%">1741. The Pultrusion Process for Structures on Advanced Aerospace Transportation Systems</style></title><secondary-title><style face="normal" font="default" size="100%">45th Annual Conference, Williamsburg, Virginia, May 12-14</style></secondary-title></titles><keywords><keyword><style  face="normal" font="default" size="100%">22. Weight Engineering - Structural Design</style></keyword></keywords><dates><year><style  face="normal" font="default" size="100%">1986</style></year><pub-dates><date><style  face="normal" font="default" size="100%">5/12/86</style></date></pub-dates></dates><urls><web-urls><url><style face="normal" font="default" size="100%">http://www.sawe.org/store/product_info.php?products_id=39976</style></url></web-urls></urls><publisher><style face="normal" font="default" size="100%">Society of Allied Weight Engineers, Inc.</style></publisher><pub-location><style face="normal" font="default" size="100%">Williamsburg, Virginia</style></pub-location><pages><style face="normal" font="default" size="100%">12</style></pages><language><style face="normal" font="default" size="100%">eng</style></language><abstract><style face="normal" font="default" size="100%">The pultrusion process, which has the potential for use in the manufacture of structures for aerospace hardware, is described.  In this process, reinforcing fibers are pulled continuously through a resin system for wetting and subsequently through a heated die for polymerization.  By using this process, fabrication of very long lengths of high strength, lightweight structures with consistently high quality for aerospace applications is possible.  The more conventional processes involve hand lay-up, vacuum bagging, autoclaving or even oven curing techniques such that length of structural elements produced are limited by the lengths of autoclaves or curing ovens.  Several types of developmental structural elements are described in which fiberglass, aramid, graphite, and hybrid fiber systems have been used as reinforcements in an epoxy matrix and their flexural properties compared.  Reinforcement fibers having tailor-made orientations which achieve tailor-made strength in the pultrusions are described.  The potential aerospace applications for the pultruded products are described with advantages cite over conventional hand lay-up methods.</style></abstract><work-type><style face="normal" font="default" size="100%">22. WEIGHT ENGINEERING - STRUCTURAL DESIGN</style></work-type><accession-num><style face="normal" font="default" size="100%">1741</style></accession-num><custom1><style face="normal" font="default" size="100%">Non-Member Price: $10.00. Members may download this paper for free. &lt;a href=&quot;http://www.sawe.org/dms&quot;&gt;Click here&lt;/a&gt;. (Login Required. See SAWE &lt;a href=&quot;http://www.sawe.org/faq&quot;&gt;Frequently Asked Questions&lt;/a&gt;.)</style></custom1></record></records></xml>