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Competed

Patent Known References

TypePatent CountryPatent Number
Patent US 20150183505
Patent US 2007114331
Patent US 2005001093
Patent US 20120112004
Patent WO 2000005130
Patent WO 1993014999
Patent US 20130112811
Patent US 20110011978
Patent US 20080210820
Patent US 20070209568
Patent US 8813926
Patent US 6427945
Patent US 6032606
Patent US 5562264
Patent US 5324563
Patent US 3848284
Patent US 2245497
Patent US 20070114331
Patent US 20050001093
Patent US 2012112004
Patent US 8827057
Patent US 6032606
Patent GB 2219257
Patent GB 2150892
Patent GB 922792
Patent GB 351193
Patent GB 137197
Patent FR 2903961
Patent FR 2784961
Patent DE 102006040298
Patent DE 20220600
Patent DE 10352996
Patent JP 06-107290
Patent JP 07-001127
Patent JP 09-086483
Patent JP 2003-053851
Patent JP 2004-182136
Patent JP 2004-324814

Published Known References

TypeTitle of NPL
Other European Search for EP 13400042 Completed by the European Patent Office on June 2 2014 3 Pages
Website COPPINGER. Flight International April 26 2005 Col. 167 No. 4982 Pg. 26 XP-001227208 Composites Soften Impact downloaded from : https://flightglobal.com/news/articles/composites-soften-impact-197140/
Journal A new composite energy absorbing system for aircraft and helicopter Composite Structures 2006 Vol. 75 pgs. 14-23
Conference Crash simulation of composite and aluminum helicopter fuselages using a finite-element program
Conference Multi Terrain impact testing and simulation of a composite energy absorbing fuselage section
Journal Development of a scale model composite fuselage concept for improved crashworthiness Journal of aircraft Vol. 38 No. 1 January-February 2001
Book Structural crashworthiness and failure
Journal Theory and application of finite element analysis to structural crash simulation Computers & Structures Vol. 13 pp. 277-285 1981
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