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Autor

  • Fedelich, Bernard (120)
  • Skrotzki, Birgit (16)
  • Link, T. (15)
  • Klingelhöffer, Hellmuth (12)
  • Epishin, A. (11)
  • Portella, Pedro Dolabella (9)
  • Rehmer, Birgit (9)
  • Kühn, Hans-Joachim (8)
  • Kindrachuk, Vitaliy (7)
  • Sievert, Rainer (7)
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Erscheinungsjahr

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  • Creep (16)
  • Superalloy (9)
  • LCF (7)
  • Rafting (7)
  • Nickel-base superalloys (6)
  • Single crystal (6)
  • TMF (6)
  • Constitutive law (5)
  • Creep damage (5)
  • Low cycle fatigue (5)
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Organisationseinheit der BAM

  • 5 Werkstofftechnik (32)
  • 5.2 Experimentelle und modellbasierte Werkstoffmechanik (32)
  • 5.1 Materialographie, Fraktographie und Alterung technischer Werkstoffe (3)

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Constitutive modelling of viscoplastic deformation in single crystal nickel-basis superalloys subjected to cyclic and creep loadings at high-temperatures (2017)
Kindrachuk, Vitaliy ; Fedelich, Bernard ; Becker, M.
Gas turbines are widely used for a variety of purposes including power generation, compression or as jet engines in aircrafts. The critical components of a gas turbine are the high-pressure turbine blades which operate under severe conditions. These include thermo-mechanical loadings over temperatures ranging from room temperature up to 1100°C. While a large number of constitutive models for single crystals have been proposed, most applications are restricted to special loading scenarios, temperature range and deformation mechanisms. In particular, a number of models are focused on pure creep. Only a few papers consider application of both creep and fatigue. Applications of the constitutive models to long-term stress relaxation are even scarcer. The new model assumes deformation-induced softening and can properly reproduce the viscous behavior at different time scales. The model has been calibrated with the uniaxial tests at 800°C and 950°C in [001], [011] and [111] specimens of a nickel-basis superalloy. The predicted creep, short- and long-term relaxation and cyclic tests are in reasonable agreement with the experimental observations.
Zur rechnerischen Bewertung der Lebensdauer von Bauteilen unter TMF mit einer Kombination von kommerziellen FE-Programmen und Anwendersoftware (2017)
Fedelich, Bernard ; Haftaoglu, Cetin ; Kindrachuk, Vitaliy
Die Analyse der Lebensdauer von Bauteilen unter thermomechanischer Ermüdung (TMF) erfordert ein geeignetes Stoffgesetz, welches in der Lage ist, zyklische Plastizität die Abhängigkeit der Spannungsantwort nach der Dehnrate, Kriechen und Spannungsrelaxation temperaturabhängig zu beschreiben und ein Lebensdauermodell, welches in Abhängigkeit von der örtlich aufgelösten Spannungs- und Verformungsgeschichten eine Schätzung der Anzahl der Zyklen bis zum Anriss liefern kann.
Simulation of non-isothermal mechanical tests on a single crystal nickel-basis superalloy (2017)
Fedelich, Bernard
Gas turbines are widely used for a variety of purposes including power generation, compression or as jet engines in aircrafts. The critical components of a gas turbine are the high-pressure turbine blades which operate under severe conditions. These include thermo-mechanical loadings over temperatures ranging from room temperature up to 1100°C. While a large number of constitutive models for single crystals have been proposed, most applications are restricted to special loading scenarios, temperature range and deformation mechanisms. In particular, a number of models are focused on pure creep. Only a few papers consider application of both creep and fatigue. Applications of the constitutive models to long-term stress relaxation are even scarcer. The new model assumes deformation-induced softening and can properly reproduce the viscous behavior at different time scales. The model has been calibrated with the uniaxial tests at 800°C and 950°C in [001], [011] and [111] specimens of a nickel-basis superalloy. The predicted creep, short- and long-term relaxation and cyclic tests are in reasonable agreement with the experimental observations.
Creep behaviour of the single-crystal nickel-base superalloy CMSX-4 at ultra-high homologous temperature (2015)
Epishin, A.I. ; Link, T. ; Nolze, Gert ; Fedelich, Bernard ; Schriever, Sina
Data about the creep behaviour of metals and their alloys at temperatures close to the melting point are very limited. The reason is that most engineering alloys are used at temperatures below 0.6-0.8 of their melting point, so, Investigation of creep at higher temperatures has no practical relevance. For some special applications however it is important, in our case hot isostatic pressing (HIP) of single-crystal turbine blades cast from nickel-base superalloys. In order to remove porosity the blades are HlPed at temperatures between y'-solvus and solidus where superalloy has no strengthening y'-phase and therefore is very soft. For example, the Company Howmet Castings HIPs the superalloy CMSX-4 at the temperature 1288aC, which corresponds to a homologous temperature of about 0.97=1561 K/1612 K (solidus temperature). Therefore knowledge about the creep behaviour of CMSX-4 at this temperature and understanding of the creep mechanisms are necessary to model the kinetics of pore closure during HIP as well as to plan the Parameters of the HIP process.
Die thermomechanische Ermüdung von Hochtemperatur beanspruchten Bauteilen: Überblick der Materialmodelle und Fortschritte in der Bauteilsimulation (2015)
Fedelich, Bernard
Overview about constitutive models for single crystal superalloys (2017)
Fedelich, Bernard
The technological importance, the regularity of the microstructure and the complexity of the mechanical behavior of single crystal superalloys have motivated the development of a large number of mathematical models of the mechanical behavior of these alloys in the last two decades. While crystal viscoplasticity has proven to be an efficient framework to account for their anisotropy, several issues are still challenging. Indeed, most models consider that octahedral and cubic slip systems contribute to the largest part of the plastic deformation. However, the exact nature of cubic slip is still controversial and the precipitates can be sheared by <112> slip systems at intermediate temperatures, which largely influence the dependence of the flow rate on the orientation under creep conditions. Due to the different strengths of the matrix and the precipitates and the large volume fraction of the precipitate phase, a complex distribution of internal stresses exists, which can difficultly be captured by the conventional back stress models of plasticity. In addition, at high temperature, the microstructure degrades and the residual mechanical strength is reduced. The driving force for this microstructure degradation is intimately connected to the distribution of the internal stresses. As a result of this complexity, a large number of tests are usually required to fully characterize the mechanical behavior of single crystal superalloys. This in turn largely impedes the implementation of inelastic modeling in the industrial praxis. The lecture summarizes the principal types of constitutive models for single crystal superalloys and reviews some recent advances in this area. In particular, it is shown how simulations at the microstructure scale level combined with conventional testing and microscopic analysis helped to improve our understanding of the mechanical behavior of single crystal superalloys. Directional coarsening, the importance of internal stresses, orientation dependency and the corresponding modeling issues are discussed. Also open questions are highlighted.
Open aspects in constitutive modeling for single crystal superalloys (2016)
Fedelich, Bernard
Presentation that presents various open aspects in constitutive modelling of superalloys
Zur rechnerischen Bewertung der Lebensdauer von Bauteilen unter tMF mit einer Kombination von kommerziellen FE-Programmen und Anwendersoftware (2017)
Fedelich, Bernard
Die thermomechanische Ermüdung (TMF) von Bauteilen kann heutzutage mit der Finite-Elemente (FE) Methode simuliert werden. Dafür werden komplexe viskoplastische Stoffgesetze benötigt, welche in der Regel in kommerziellen FE Programme nicht zur Verfügung stehen. Im Vortrag wird gezeigt wie solche Stoffgesetze mit Hilfe von benutzerdefinierten Subroutinen in kommerzielle Finite-Elemente Programme implementiert werden können. Es wird auf die Vor- und Nachteile einer expliziten oder impliziten Integration der Entwicklungsgleichungen für die inneren Variablen hingewiesen. Schließlich wird ein Postprozessingstool beschrieben, mit dem die Überlagerung einer niederfrequenten (TMF) und einer hochfrequenten (HCF) Belastung im Bauteil analysiert werden können.
Constitutive modeling and lifetime prediction for a conventionally cast Ni-base superalloy under TMF loading (2016)
Fedelich, Bernard
Under cyclic thermomechanical loading, various effects such as strain accumulation, creep damage, ageing, fatigue etc. may occur in the material of a gas turbine blade. Depending on the loading conditions, all these effects contribute to reduce the lifetime of the component. Subject of the present work is the development of a material model to describe the mechanical effects mentioned above and to subsequently predict lifetimes by using simulated stress strain data. Starting point for deformation modeling is the well known viscoplastic model after Chaboche, which provides descriptions of isotropic and kinematic hardening, as well as dynamic and static recovery. The evolution equation for kinematic hardening model has been modified following the proposal of Ohno/Wang to better predict stress controlled cyclic strain accumulation, i.e. ratchetting. A damage variable has been included to represent tertiary creep according to the concept of Kachanov. Finally, the static recovery has been modified following Kindrachuk to account for strain induced ageing. The models parameters have been calibrated using isothermal test data only. The constitutive model has been validated by comparing experimental with predicted TMF stress-strain hystereses. Lifetime prediction is done with the TMF lifetime model proposed by Riedel. The model assumes that fatigue life is controlled by the propagation of short cracks. Besides pure fatigue, it takes the local creep deformations at the crack tip into account. The model is applied to a broad variety of isothermal and non isothermal tests over temperatures up to 950°C and different loading conditions. The evaluation shows that throughout satisfying results can be achieved using a limited number of model parameters for the whole test data base.
Experimental and analytical investigation of the TMF-HCF lifetime behavior of two cast iron alloys (2016)
Fedelich, Bernard
The superposition of small amplitude, high frequent loading cycles (HCF) to the slow, large amplitude, TMF loading cycles can significantly reduce the TMF life, i.e. the number of TMF blocks until failure. In this work, the combined TMF-HCF loading has been experimentally investigated for two cast iron alloys. Both alloys contain globular graphite nodules but the first one has a ferritic while the second one has an austenitic crystal structure. In particular, the influence of the HCF frequency, of the HCF loading amplitude and of the location of the superposed HCF cycles has been investigated. It was observed that the HCF frequency has a limited impact on the TMF fatigue life. In other words, the number of superposed HCF-cycles has only a slight influence on the TMF fatigue life, which contradicts the linear damage accumulation rule concept. On the other side, the HCF-strain amplitude has a highly non-linear influence on the TMF fatigue life. The experimental results can be understood in terms of a fracture mechanics based damage mechanism [1]: Cracks readily initiate due to the TMF loading and the duration of the growth of the cracks up to a few mm controls the fatigue life. If HCF-loading cycles are superposed, cyclic crack propagation dramatically accelerates at some stage. This stage is related to the existence of a threshold for crack growth under pure HCF-conditions and largely controls the fatigue life of the combined loading. The previous ideas have been expressed in a model that can be very simply applied to provide the fatigue life reduction factor due to the superposed HCF cycles. It only contains two additional adjustable parameters and can be combined with any TMF model.
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