<?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%">Zenas, Robert</style></author></authors></contributors><titles><title><style face="normal" font="default" size="100%">3026. Electron Beam Welding of F-22 Aft Fuselage Primary Structures</style></title><secondary-title><style face="normal" font="default" size="100%">59th Annual Conference, St. Louis, Missouri, June 5-7</style></secondary-title></titles><keywords><keyword><style  face="normal" font="default" size="100%">27. Weight Reduction - Materials</style></keyword></keywords><dates><year><style  face="normal" font="default" size="100%">2000</style></year><pub-dates><date><style  face="normal" font="default" size="100%">6/5/00</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=43464</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%">St. Louis, Missouri</style></pub-location><pages><style face="normal" font="default" size="100%">21</style></pages><language><style face="normal" font="default" size="100%">eng</style></language><abstract><style face="normal" font="default" size="100%">Two major components of the rear fuselage of the F-22 Raptor fighter, the forward and aft boom assemblies, were designed and fabricated as monolithic weldments in order to achieve a significant weight savings. This was a challenging task, as these components are fracture/durability critical, load bearing structures that attach the wings and vertical stabilizers to the fuselage and support the horizontal stabilizers. They also form part of the engine bay compartment, have aerodynamic surfaces/contours, and provide internal fuel storage. These highly efficient structures are made from over 90 separate pieces of 6Al-4V titanium alloy. Over 3,600 inches of full penetration electron beam welding are required to fabricate the four assemblies for each ship set. </style></abstract><work-type><style face="normal" font="default" size="100%">27. WEIGHT REDUCTION - MATERIALS</style></work-type><accession-num><style face="normal" font="default" size="100%">3026</style></accession-num><custom1><style face="normal" font="default" size="100%">Non-Member Price: $13.23. 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><custom3><style face="normal" font="default" size="100%">13.23</style></custom3></record></records></xml>