02489nam 2200445 450 991081892030332120230803043537.03-8325-9334-9(CKB)4340000000244336(MiAaPQ)EBC5247085(Au-PeEL)EBL5247085(CaPaEBR)ebr11539814(OCoLC)102180556758a1c693-9e40-499a-8417-3edeb0dd2d03(EXLCZ)99434000000024433620180521d2013 uy 0engurcnu||||||||txtrdacontentcrdamediacrrdacarrierAnalysis of process-induced distortions and residual stresses of composite structures /Christian BraunerBerlin :Logos,[2013]©20131 online resource (x, 155 pages) illustrationsScience Report aus dem Faserinstitut Bremen ;Band 8PublicationDate: 201310293-8325-3528-4 Long description: The increased application of composite materials in lightweight structures leads to new integral design of structural parts, using the example of, an integral composite landing flap of an Airbus A320 aircraft. This offers possibilities to simplify the process chain, to decrease manufacturing costs and to have fibre fair structural design. The critical disadvantage of large integral designs is that process-induced deformations are a risk factor during the design phase of the manufacturing process, because rework is not always possible. Especially, the aircraft industry with its demands on high qualities / tolerances and the application of hot curing resin systems, requires knowledge-based methods for virtual process design to avoid time- and effort-consuming iterations. This thesis contributes to the understanding of the mechanism behind process-induced distortions and stresses related to the Resin Transfer Moulding (RTM) manufacturing process. The aim is to comprehend the phenomena, to identify related parameters and to present compensation strategies.Deformations (Mechanics)Deformations (Mechanics)620.1123Brauner Christian1606491MiAaPQMiAaPQMiAaPQBOOK9910818920303321Analysis of process-induced distortions and residual stresses of composite structures3932294UNINA