DLR-Logo -> http://www.dlr.de
DLR Portal Home | Imprint | Privacy Policy | Contact | Deutsch
Fontsize: [-] Text [+]

As-Built-Simulation based on TFP Manufacturing Data

Kärger, Luise and Kling, Alexander and Wille, Tobias (2010) As-Built-Simulation based on TFP Manufacturing Data. ISCM, 06. - 07. Oktober 2010, Marknesse, Niederlande.

Full text not available from this repository.


The Feedback Method is developed to close the gap in the development chain which still exists between design, manufacturing and certification of TFP structures. Tailored Fibre Placement (TFP) is a textile process for optimized fibre reinforced structures with fibre alignments of almost any de-sired orientation. The TFP process provides an improved load-bearing capacity, but also affects the local material properties. Thus, appropriate material models of the TFP composites are of critical importance for a successful application. For this purpose, the so-called Feedback Method gener-ates as-built finite element models by considering manufactured fibre lay-ups, fibre orientations as well as special fibre features like curved fibres or roving kinks. The development chain of a composite structure typically starts with the design process: Based on the optimization results, an FPM (Fibre Placement Manager) or CAD geometry model is developed, where manufacturing constraints in terms of feasibility and economic efficiency are considered. According to this manual step from as-design to as-built, a certification of the real, “as-built” struc-ture is needed. Hence, the purpose of the Feedback Method is an automatic transformation from FPM/CAD models to suitable high-fidelity “as-built” FE models. In addition to the automatic data transformation from as-design to as-build, a multi-scale analysis is performed, where local fibre particularities (e.g. curved fibres) are considered at mesoscopic level and effective global material properties are automatically computed. According to this developed feedback method also other manufacturing data, e.g. lay-up, spring-in angles or residual stresses, are integrated within the future development chain of fibre reinforced composite structures. Thus, a less conservative design concept is developed by accounting for different types of constraints as well as deterministic and probabilistic manufacturing uncertainties within the early design phase of a concurrent engineering process.

Item URL in elib:https://elib.dlr.de/75334/
Document Type:Conference or Workshop Item (Speech)
Title:As-Built-Simulation based on TFP Manufacturing Data
AuthorsInstitution or Email of AuthorsAuthor's ORCID iD
Date:October 2010
Open Access:No
Gold Open Access:No
In ISI Web of Science:No
Keywords:CFRP, fibre placement, TFP, AFP, process simulation, multiscale analysis, homogenization, feed-back method, process chain, manufacturing uncertainties
Event Title:ISCM
Event Location:Marknesse, Niederlande
Event Type:international Conference
Event Dates:06. - 07. Oktober 2010
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Aeronautics
HGF - Program Themes:Aircraft Research (old)
DLR - Research area:Aeronautics
DLR - Program:L AR - Aircraft Research
DLR - Research theme (Project):L - Simulation & Validation (old)
Location: Braunschweig
Institutes and Institutions:Institute of Composite Structures and Adaptive Systems > Structural Mechanics
Deposited By: Böhringer-Thelen, Isolde
Deposited On:27 Mar 2012 12:41
Last Modified:27 Mar 2012 12:41

Repository Staff Only: item control page

Help & Contact
electronic library is running on EPrints 3.3.12
Copyright © 2008-2017 German Aerospace Center (DLR). All rights reserved.