Ingenieurwissenschaften und zugeordnete Tätigkeiten
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Vergleichende Bewertung verschiedener Verfahren der E-Modulbestimmung für metallische Werkstoffe
(2017)
Für numerische Beanspruchungs- und Lebensdaueranalysen ist die Kenntnis des E-Moduls der eingesetzten Werkstoffe von zentraler Bedeutung. Für seine experimentelle Bestimmung wurden eine Vielzahl von Verfahren entwickelt, die zum Teil werkstoffspezifisch Eingang in die Normung gefunden haben. Prinzipiell können diese Verfahren in zwei Gruppen eingeteilt werden - die statischen und die dynamischen Prüfverfahren. Während die statischen Verfahren auf der direkten Messung des Spannungs-Dehnungs-Zusammenhangs während einer Belastung im elastischen Verformungsbereich beruhen (Zug-, Biege- bzw. Druckversuch) nutzen die dynamischen Verfahren die Analyse der resultierenden Schwingungen nach einer entsprechenden Anregung eines Prüfkörpers (Resonanz- bzw. Impulsanregungsmethode). Für verschiedene Werkstoffe wurden statische und dynamische Verfahren zur E-Modulbestimmung eingesetzt. Die Unterschiede und Vorteile der verschiedenen Verfahren werden vergleichend diskutiert.
Vergleichende Bewertung verschiedener Verfahren der E-Modulbestimmung für metallische Werkstoffe
(2017)
Für numerische Beanspruchungs- und Lebensdaueranalysen ist die Kenntnis des E-Moduls der eingesetzten Werkstoffe von zentraler Bedeutung. Für seine experimentelle Bestimmung wurden eine Vielzahl von Verfahren entwickelt, die zum Teil werkstoffspezifisch Eingang in die Normung gefunden haben. Prinzipiell können diese Verfahren in zwei Gruppen eingeteilt werden - die statischen und die dynamischen Prüfverfahren. Während die statischen Verfahren auf der direkten Messung des Spannungs-Dehnungs-Zusammenhangs während einer Belastung im elastischen Verformungsbereich beruhen (Zug-, Biege- bzw. Druckversuch) nutzen die dynamischen Verfahren die Analyse der resultierenden Schwingungen nach einer entsprechenden Anregung eines Prüfkörpers (Resonanz- bzw. Impulsanregungsmethode). Für verschiedene Werkstoffe wurden statische und dynamische Verfahren zur E-Modulbestimmung eingesetzt. Die Unterschiede und Vorteile der verschiedenen Verfahren werden vergleichend diskutiert.
TMF tests were carried out on EN-GJSA-XNiSiCr35-5-2 at constant minimum temperature (400 °C) and varying maximum temperatures (Tmax = 700 °C, 800 °C, 900 °C) with hold times of 180 s at Tmax and two phase angles (in-phase (IP), 180° out-of-phase (OP)). The results showed a comparable strength under OP- and IP-TMF loading. At Tmax = 700 °C and 900 °C, the lifetime in IP-tests was slightly longer than that of OP-tests, while it is vice versa at Tmax = 800 °C. The IP-tests at Tmax = 900 °C showed a similar lifetime as OP-tests at Tmax = 700 °C and 800 °C, which was unexpected for such a high testing temperature. All IP-tests at Tmax = 900 °C showed a continuous cyclic softening from the beginning on, which was different from all other testing conditions. Complementary metallographic investigations indicated that under this test condition, intergranular creep damage is present in the volume of the test pieces.
The use of miniaturized specimen geometries in mechanical testing allows extracting the sample material directly from critical components of power plants like e.g. headers and pipes. In this way, both the impacts of the manufacture of the component (including all shaping and tempering influences) and of the complex aging/loading/oxidation conditions during Service can be analyzed and representative mechanical properties are obtained. In the present study, example results of a comparative creep and creep rupture study on P91 tempered martensite ferritic Steel, involving Standard and miniature specimens that were all taken from one batch of material, are presented. Cylindrical creep specimens with a minimum gauge length diameter of 3 mm were used, representing the smallest recommended test geometry of ISO 204. The test results of miniature specimens exhibit all characteristic creep features of tempered martensite ferritic steels, and analysis of the stress and temperature dependence of creep results in values that correspond well to literature data for P91. However, direct comparison with large scale specimen data reveals small but systematic variations in minimum creep rates, elongations at fracture and times to rupture. In our contribution, these differences are discussed in the light of literature findings on specimen size influences in other heat resistant alloys. Size effects need to be considered for a correct interpretation of results from miniature specimen creep tests.
The aluminum alloy 2618A is an Al-Cu-Mg alloy with additions of Fe and Ni, which was designed for long-term operation at elevated temperature in transportation and aerospace industries. Typical applications include aircraft parts and structures (sheet material) or engine components such as turbo charger centrifugal compressor wheels (forged material). Such components are subjected to prolonged aging during service, (e.g. 50 000 h) at temperatures which are close to their age hardening temperature (ca. 190 °C).
The microstructural evolution during creep exposure is studied.
The aluminum alloy 2618A is an Al-Cu-Mg alloy with additions of Fe and Ni, which was designed for long-term operation at elevated temperature in transportation and aerospace industries. Typical applications include aircraft parts and structures (sheet material) or engine components such as turbo charger centrifugal compressor wheels (forged material). Such components are subjected to prolonged aging during service, (e.g. 50 000 h) at temperatures which are close to their age hardening temperature (ca. 190 °C). The microstructural evolution was investigated.
The fatigue behaviour of cast iron is usually investigated on machined specimens. Components of cast iron, however, have a casting skin; therefore the investigation of the influence of the casting skin on the lifetime is of interest. To study this influence isothermal fatigue tests were carried out on heat-resisting spheroidal graphite cast iron EN GJS SiMo 4.05 in 4–point-bending set-up at 400 °C. Specimens with and without casting skin were investigated comparatively. The number of cycles to failure was significantly lower for specimens with casting skin. Metallographic investigations underline the reduction of lifetime caused by casting skin.
It is widely known that the magnetic domain structure of stress-sensitive ferromagnetic materials may be altered by external or internal mechanical stresses due to magnetoelastic effects. In this contribution, localized magnetic domain changes arising from inhomogeneous deformation and multiaxial loading conditions are imaged by the Bitter method for the first time. It is demonstrated that these domain changes provide deformation-related information and thus, allow for the visualization of macroscopic strain gradients in fine-grained polycrystalline steels, while keeping a sufficient spatial resolution.
This approach has been developed within the framework of BAM-MI-project “MICRONET”.
Experimental and analytical investigation of the TMF-HCF lifetime behavior of two cast iron alloys
(2017)
The combined loading Thermomechanical Fatigue (TMF) with High Cycle Fatigue (HCF) has been experimentally investigated for two cast iron alloys. Both alloys contain globular graphite nodules but the first one has a ferritic structure while the second one has an austenitic crystal structure. In particular, the influences of the HCF frequency, of the HCF loading amplitude and of the location of the superposed HCF cycles have been investigated. It was observed that the HCF frequency has a limited impact on the fatigue life. On the other side, the HCF-strain amplitude has a highly non-linear influence on the fatigue life. The experimental results can be understood in terms of a fracture mechanics based damage mechanism: Cracks quickly initiate due to the TMF loading and 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 after a threshold has been reached. This threshold is regarded as controlling the fatigue life reduction. The previous ideas have been expressed in a model that can be very simply applied to estimate the fatigue life reduction ratio due to the superposed HCF cycles. It only contains two adjustable parameters and can be combined with any TMF life assessment model.