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EN
One of the major areas of titanium alloys application includes discs and blades of compressors in turbine engines. In titanium alloys, significant strain can accumulate as a function of time, at stresses well below the yield strength at the homologous temperature below 0.25, even at room temperature. Life prediction for elements made of titanium alloys which is based solely on steady state creep parameters is in some cases not adequate due to large primary creep strains. In the case of rotating components of aero-engines small dimensional tolerances can be threatened and transient creep strains must be taken into account in modelling of overall creep deformation. Creep and fatigue properties of two-phase titanium alloys show strong dependence on microstructure, especially morphology of the α and β phases which can be controlled to certain extent by proper selection of hot working and heat treatment conditions. In the paper the primary creep behaviour of Ti–6Al–2Mo–2Cr alloy (VT3–1) at elevated temperature was investigated. The microstructure of the alloy was varied by means of changing conditions of heat-treatment. Creep tests were carried out on the alloy with globular and lamellar microstructure at the temperature of 450°C. Primary stage of the creep process was described using various constitutive laws. Applicability of power-law and logarithmic equations for describing strain evolution was verified. The influence of the initial microstructure on the primary creep strain and strain rate at the onset of steady-state creep stage was analysed.
PL
W pracy podjęto próbę określenia oddziaływania morfologii mikrostruktury dwufazowego stopu tytanu Ti–6Al–2Mo–2Cr na jego właściwości w stadium pełzania nieustalonego w temperaturze 450°C. Istotnym celem badań był dobór równań konstytutywnych opisujących krzywe pełzania stopu, które mogą być zastosowane do ilościowej oceny wpływu morfologii mikrostruktury stopu na wielkości charakteryzujące proces pełzania. Zagadnienie to jest istotne w procesie projektowania elementów konstrukcyjnych, zwłaszcza w przypadku małych tolerancji wymiarów (np. łopatki wirnika sprężarki silnika turbinowego), ze względu na skłonność stopów tytanu do osiągania znacznych odkształceń trwałych, zależnych od czasu, nawet w zakresie temperatury homologicznej poniżej 0,25.
EN
Creep and fatigue properties of two-phase titanium alloys show strong dependence on microstructure, especially morphology of the α and β phases which can be controlled to certain extent by proper selection of hot working and heat treatment conditions. In the paper the creep behaviour of Ti-6Al-2Mo-2Cr alloy (VT3-1) at elevated temperature was modelled. Finite element analyses of primary creep stage were carried out taking into account some microstructural features of the two-phase alloy that were included in the physical model and different properties of α and β phases. In order to verify results of calculations distinct types of microstructure were developed in the alloy by heat treatment and creep tests were carried out at elevated temperature (450°C) at various stress levels. Based on the FEM simulations the effect of changes of some microstructure features on primary creep strain development was estimated.
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