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Logo Institut für Flugzeugbau und Leichtbau der TU Braunschweig
Composites
  • Research
    • Structural Design & Optimization
    • Composites
    • Preliminary Aircraft Design
    • Multiphysics
    • Fracture Mechanics
    • Scaled flight tests

Composites

The increasing use of composite materials in automobile, aircraft and wind energy applications, together with the need to stress these structures to a higher level increases the demand to assess the fatigue behaviour.


Current projects

ZIM Projekt: BionicWalker -Development of a new type of prosthetic fitting for patients with partial foot amputations through the introduction of a carbon spring element for the absorption, storage and release of kinetic energy

Funding: Bundesministerium für Wirtschaft und Energie im Zentralen Innovationsprogramm Mittelstand (ZIM)

Duration: 2021 – 2023

Team:  J. Finder, S. Heimbs

The "Bionic Walker" project is a cooperation project funded by the Central Innovation Programme  for SMEs (Zentrale Innovationsprogramm Mittelstand) for the development and research of a new prosthetic fitting for patients with partial foot amputations. The project consortium includes REHA-OT Lüneburg Melchior & Fittkau GmbH from Lüneburg, Zeisberg Carbon GmbH from Hanover, OK Gummiwerk Otto Körting GmbH from Hameln, the Institute for Orthopaedic Movement Diagnostics (OrthoGO) from Hanover and the institutes belonging to the HPCFK research group, the Institute of Aircraft Design and Lightweight Structures at the Technical University of Braunschweig and the Institute of Polymer Materials and Plastics Engineering at the Technical University of Clausthal. The project consortium is administratively supported by the Wirtschaftsförderungs-GmbH für Stadt und Landkreis Lüneburg.

The task of the new prosthetic fitting is to restore a normal, dynamic and symmetrical gait for patients who have undergone partial foot amputations in order to prevent subsequent complaints caused by changes in gait and to enable them to return more quickly to their everyday social and professional lives. The essential function of the product is achieved by a special spring element made of carbon fibre-reinforced plastic that replicates the characteristics of the anatomical structures that are no longer present. Just like in a healthy musculoskeletal system, part of the kinetic energy is stored in the spring element as potential energy when stepping on during walking. When the foot is lifted again, the compressed spring serves to support the patient and reduces the amount of force required.

Based on a gait analysis to determine the medical requirements, the complete development, production and combination of all components into a demonstrator takes place within the cooperation project. Its functionality and effect will be proven through static and cyclic tests in a testing machine, multi-axis tests with an industrial robot and realistic tests in the gait laboratory.

DIWA

CT-Aufnahme eines geschädigten dickwandigen FKV-Geflechts
CT-Aufnahme eines geschädigten dickwandigen FKV-Geflechts

Funding: DFG

Duration: Since 2019

Team: Tim Luplow , P. Horst, S. Heimbs

The goal of the joint research project DIWA is to investigate the basic causes and effects of structural composite imperfections, such as fiber misalignment, undulation, and residual stress, on the behavior of thick-walled, biaxially braided fiber-reinforced plastic composites under uniaxial and multiaxial quasistatic, cyclic, and thermal loading. The IFL will investigate the fatigue behavior of thick-walled glass fiber composites under uniaxial and multiaxial loading. Experiments will be conducted on samples with thicknesses up to 10 mm to quantify the effect of thickness on mechanical properties and damage phenomena under uniaxial loading. In a next step, box-shaped structures will be tested under multiaxial loading (axial compression and shear) on the MPT (Multiaxial Panel-Test facility). Additionally, a Multi-Scale Model using the finite element method will be developed for the simulation of material properties and damage in thick-walled braided structures. This model will predict the influence of various thickness-dependent parameters such as nesting, roving orientation, and fiber volume fraction. The necessary parameters will be obtained from microscopy, ultrasonic and CT images.

Further Information

FASTHER - Numerical and experimental investigation of the fatigue strength of welded thermoplastic FRP structures taking residual stresses into account

Fasther Projekt

Funding: Deutsche Forschungsgemeinschaft (DFG)

Duration: 2022 – 2025

Team:  J. L. Stüven, S. Heimbs

Thermoplastic matrices in fibre composite structures have increasingly become the focus of research in recent years, as they have a decisive advantage over thermoset matrices: their weldability. This offers great potential, e.g. in terms of weight reduction, cycle time reduction and recyclability, which is so important nowadays. Although various welding processes are the subject of research and some of them are already used in industrial applications, the basic operating principle of the processes is very similar. The matrix is melted by applying heat in the area of the intended joining zone. Under the influence of externally applied pressure on the joining partners during cooling, these are then joined to form a component. In our own numerical simulations within the JoinThis project, it has already been shown that residual stresses occur in the joining zone and its surroundings as a result of the cooling process, which cause preliminary damage to the matrix. Particularly for components subjected to cyclic loads, this results in potential pre-damage that reduces the service life and must be taken into account in the dimensioning of components subjected to such loads.

The aim of the FASTHER project is to systematically investigate the damage behaviour of welded thermoplastic fibre composite structures with regard to cyclic loading, taking into account thermal residual stresses. The central research hypothesis is that a procedure for the computational lifetime prediction of welded fibre-reinforced thermoplastics can be created on the basis of the finite element method. With the completion of the project, a detailed modelling of the fatigue damage of welded thermoplastic fibre composite structures is available for the first time, which provides valuable insights with regard to the computational dimensioning in aircraft construction. In addition, the understanding of the numerical modelling of the fatigue of FRP is expanded and a significant contribution is made to the possibilities of experimentally obtaining validation data with the aid of fibre-optic sensors.

Completed projects

EFRE project: AutoBLADE - Automated technology for the production of continuously draped preforms with a high aspect ratio
AutoBlade

Funding: EUROPÄISCHEN FONDS FÜR REGIONALE ENTWICKLUNG (EFRE)

Duration: 2021-2022

Team: J. L. Stüven

Harnessing the energy from tidal currents offers great potential to increase the renewable share in the energy mix of the future. The production of rotor blades for the tidal power plants, like the production of wind power rotor blades, is characterised by a predominantly manual workload. This applies in particular to the preforming process, in which a large-area textile preform is produced and vacuum-infused with a polymer matrix in a subsequent step. While preforming for small and medium-sized components is usually carried out by compression moulding, there is no automated counterpart for large-area components with a high length-to-width ratio (aspect ratio). If the preforming for such FRP components can be automated, both economic and quality-specific production optimisations for sustainable energy generation can be envisaged.

The aim of the research project to be carried out in the innovation network of the LU Hannover, TU Clausthal and TU Braunschweig is the development and research of an automated technology for the production of continuously draped preforms for large-area FRP infusion components with a high aspect ratio. The novel, fully automated manufacturing process, which is being developed using a technology demonstrator in the form of a rotor blade for tidal power plants, involves the layer-by-layer construction of a preform by continuously draping online-bonded textile semi-finished products onto complex curved surfaces.

With the help of the functional demonstrator of a drape laying head for complex structural components developed in the FlexProCFK project, a new technology for the continuous construction of a dry fibre preform is being developed and researched. One focus of the research is the fixation of the fibre textile by means of a sprayed-on binder on the mould or the previously deposited textile layer in order to prevent slipping. The laying process is adapted to the activation behaviour of different binder types and the influence on the quality of the preform is investigated. Furthermore, the infusion behaviour of the preform under the influence of the binder material and quantity is investigated in permeability measurements and modelled for use in infusion simulations. In the technology demonstrator under consideration, production-induced fibre angle deviations and wrinkling in the preform represent one of the most frequent causes of failure. The fibre angles and drape defects in the preform are recorded by the stereoscopic recording of the fibre structure after deposition and serve as a basis for a realistic infusion simulation and structural analysis for the property characterisation of the rotor blade. The influence of local fibre angle deviations on mechanical component properties such as strength and stability is simulated as a function of component geometry parameters and material properties. Through continuous exchange in the innovation network, the findings from the experimental and simulative investigations are efficiently linked and incorporated into process development to increase preform quality.

VHCF-2
Beispiel von Rissen und Delaminationen in einem Kreuzlaminat

Funding: DFG

Duration: 2018 - 2022

Team: M. Bartelt, P. Horst

Das Forschungsprojekt VHCF-2 baut auf dem DFG-Schwerpunktprogramm SPP1466 auf. Im Fokus steht die Untersuchung des Ermüdungsverhaltens von Faserverbundwerkstoffen im Very-high-cycle-fatigue-(VHCF-)Bereich (Bis zu 108 Lastwechsel). Die Basis des Hochfrequenzprüfstands wird weiterentwickelt (automatische Aufnahmen, Temperaturüberwachung) und mit zusätzlichen Prüffähigkeiten wie die Ermüdung unter schwellender Belastung ausgestattet. Untersucht werden die folgenden Einflüsse anhand von Kreuzlaminaten:

  • Material (Faser-Matrix-Anbindung)
  • Schichtdicke
  • Spannungsverhältnis
  • Belastungsart

Die Einflüsse werden anhand von Schadensparametern wie Rissdichten und Delaminationsflächenanteilen charakterisiert.

DFG database

DFG-SPP1712: Teilprojekt Multilayer-Inserts - Intrinsische Hybridverbunde zur Krafteinleitung in dünnwandige Hochleistungs-CFK-Strukturen
MLI-Konzept
MLI Concept

Funding: DFG

Duration: 2014 - 2020 

Team: A. Herwig, P. Horst

The aim of this research project is to develop an intrinsic hybrid interface and its manufacturing process. The interface is characterized by a load-optimized pinned structure which allows a uniform transfer of loads at the transition metallic structure into highly stressed, complex fiber-plastic composite structures. For this purpose, an intrinsically produced multilayer insert (MLI) is developed. This insert forms a novel interface for this partial structure attachment. The CFRP considered here can be used, for example, in aircraft construction or automotive engineering in the future.

Further information

DFG database

and regarding SPP1712

DFG-Collaborative Research Center 880: Fundamentals of high lift future commercial aircraft. Project B3 - Contour-variable leading edge
droop_nose

Funding: DFG (Sonderforschungsbereich)

Duration: 2011 - 2019

Team: F. Nolte

A full analysis of today's commercial aircrafts has shown a substantial need for high lift devices, which will not be covered by the predominant technology evolution. This is true in particular in the domains of noise reduction and enhanced scalability of the performance parameters of high lift device during take-off and landing.

Within the Collaborative Research Center 880 the aerodynamic Coanda effect is intented to be utilized for high lift. Therefor a highly deflectable flap and a contour-variable leading edge is needed.

In the project B3 the research is focussed on the contour-variable skin of the leading edge, which is characterized by withstanding large strains in morphing direction as well as providing as much stiffness as possible to transfer the aerodynamic loads to the underlying, supporting structure.

DFG database

schliffbild
Micrograph section of skin sample
DFG SPP1466: Life∞ - Infinite life cycle for cyclically stressed high-performance materials
SPP1466-web-grafik

Funding: DFG

Duration: 2010 - 2017

Team: M. Bartelt, P. Horst

In the context of the DFG priority programme SPP1466, the IFL carries out research on the fatigue behaviour of fibre-reinforced composites subjected to very high numbers of load cycles. This project is realised in collaboration with the DLR (Prof. Sinapius).Given that VHCF (very high cycle fatigue) studies on standard testing machines require lengthy runs (e.g. 232 days for 108 cycles run at 5 Hz), the focus in the first stage of the project is on the construction of suitable test stations.For this purpose, at the IFL, a high frequency test stand is currently devised for fatigue-testing of glass fibre-reinforced bending specimens. In addition to the development of a test stand, priority is given to the integration and testing of various monitoring systems (thermography, microscopy) for the analysis of damage evolution.

DFG database

Photo credits on this page
CT-Aufnahme eines geschädigten dickwandigen FKV-GeflechtsTim Luplow/TU Braunschweig
Fasther ProjektHPCFK/HPCFK @hpcfk.de
AutoBladeHPCFK/HPCFK
Beispiel von Rissen und Delaminationen in einem KreuzlaminatMartin Bartelt/TU Braunschweig
MLI-KonzeptAlexander Herwig/Alle Rechte bei der TU Braunschweig
droop_noseAndre Schmitz/Alle Rechte bei der TU-Braunschweig
schliffbildAndre Schmitz/Alle Rechte bei der TU-Braunschweig
SPP1466-web-grafikTill Julian Adam/Alle Rechte bei der TU-Braunschweig
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CT-Aufnahme eines geschädigten dickwandigen FKV-Geflechts
CT-Aufnahme eines geschädigten dickwandigen FKV-Geflechts
Beispiel von Rissen und Delaminationen in einem Kreuzlaminat
MLI-Konzept
MLI Concept
droop_nose
schliffbild
Micrograph section of skin sample
SPP1466-web-grafik