Behavior of the High-Temperaturse Titanium Alloy IMI 834 Under Thermo-mechanical and Isothermal Fatigue Conditions

P. Pototzky, H. Maier, H. Christ
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引用次数: 2

Abstract

The high-temperature titanium alloy IMI 834 was studied with regard to the stress-strain response under thermo-mechanical fatigue conditions, the evolution of the microstructure, the relevant damage mechanisms and their implications for fatigue life. For this purpose isothermal and thermo-mechanical fatigue tests were performed in the temperature range from 350°C to 650°C in vacuum and air, respectively, and changes in the microstructure were determined by means of transmission electron microscopy. It was found that planar dislocation slip prevails in all tests in which the temperature does not exceed 600°C. Hence, in this temperature range the stress-strain response under thermo-mechanical conditions can be predicted solely based on the isothermal behavior. By contrast, a transition to wavy slip takes place at higher temperatures, affecting significantly the stresses in the low-temperature part of the corresponding thermo-mechanical fatigue tests. Fatigue life was generally observed to be lower in out-of-phase tests as compared to in-phase loading. Furthermore, the tests performed in high vacuum demonstrated that oxidation strongly affects fatigue life, but does not basically change the influence of testing mode on cyclic life. This can mainly be attributed to the additional effect of the acting mean stress.
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高温钛合金imi834在热-机械和等温疲劳条件下的行为
研究了高温钛合金imi834在热机械疲劳条件下的应力应变响应、组织演变、损伤机理及其对疲劳寿命的影响。为此,在真空和空气中分别在350°C至650°C的温度范围内进行等温和热机械疲劳试验,并通过透射电子显微镜确定微观结构的变化。在温度不超过600℃的所有试验中,均以平面位错滑移为主。因此,在此温度范围内,热机械条件下的应力应变响应可以仅根据等温行为来预测。相反,在较高温度下发生向波滑的转变,显著影响相应热机械疲劳试验低温部分的应力。与同相加载相比,通常观察到在非相加载中疲劳寿命较低。此外,在高真空条件下进行的试验表明,氧化对疲劳寿命的影响很大,但试验方式对循环寿命的影响基本没有改变。这主要归因于作用平均应力的附加效应。
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