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On the Creep Deformation of a Cast Near Gamma TiAl Alloy Ti-48Al-1Nb

机译:铸造近γTiAl合金Ti-48Al-1Nb的蠕变变形

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摘要

The steady-state creep deformation behavior of a cast two phase gamma TiAl alloy having the composition Ti---48Al---1Nb (at.%) has been studied. Tension creep tests using the stress increment technique (θθ2θ3) were conducted over the temperature range of 704–850°C at constant initial applied stress level of 103.4–241.3 MPa. The activation energy for creep over the temperature and stress regime of this study varied 317.5 kJ/mol (137.8 MPa) up to 341.0 kJ/mol (206.8 MPa) with an average value of 326.4 kJ/mol. This is well within the range of values previously measured for gamma TiAl alloys where creep controlled by volume diffusion has been suggested as rate controlling. The stress exponents meaured were 5.0 at 704°C, 4.9 at 750°C, 4.7 at 800°C and 4.46 at 850°C. Using the activation energy of 326.4 kJ/mol, the temperature compensated steady-state creep rate was plotted against long stress with all temperatures collapsing onto a single line having a slope equal to 4.95. Using conventional creep analysis, this value of the stress exponent can be taken as suggestive of dislocation climb controlled power law creep as the operative deformation mechanism within the stress and temperature regime of the present study. The boundary separating the lamellar grains in two phase gamma TiAl alloys having the duplex microstructure may be a very important aspect of this microstructure with respect to creep deformation resistance. The interlocking γ/α2 laths making up these boundaries are expected to be very resistant to grain boundary sliding which may contribute to creep deformation in the dislocation creep regime. Finally, some previous observations along with a comparison of the creep behavior of the Ti---48Al---1Nb alloy to that of a Tiz.sbnd;50.3Al binary have been discussed in terms of the pre-exponential constant A in the power law creep equation. TiAl alloys having similar stress and temperature dependencies but differing steady-state strain rates over comparable stress-temperature regimes may be rationalized on the basis of differing power law creep constants which may reflect differences in stacking fault energies.
机译:研究了组成为Ti --- 48Al --- 1Nb(at。%)的铸造两相γTiAl合金的稳态蠕变变形行为。在704–850°C的温度范围内,采用恒定的初始施加应力水平103.4–241.3 MPa进行了使用应力增量技术(θθ2θ3)的拉伸蠕变试验。在本研究的温度和应力范围内,蠕变的活化能为317.5 kJ / mol(137.8 MPa),最高为341.0 kJ / mol(206.8 MPa),平均值为326.4 kJ / mol。这恰好在先前针对γTiAl合金测量的值的范围内,其中建议通过体积扩散控制蠕变作为速率控制。测得的应力指数在704°C下为5.0,在750°C下为4.9,在800°C下为4.7,在850°C下为4.46。使用326.4 kJ / mol的活化能,绘制了温度补偿的稳态蠕变速率与长应力的关系图,其中所有温度都塌陷到一条斜率等于4.95的直线上。使用常规蠕变分析,该应力指数的值可以作为位错爬升控制的幂律蠕变的暗示,该蠕变是本研究应力和温度范围内的有效变形机制。就具有抗蠕变变形性而言,在具有双相微观结构的两相γTiAl合金中,将层状晶粒分开的边界可能是该微观结构的一个非常重要的方面。构成这些边界的互锁γ/α2板条有望非常抵抗晶界滑动,这可能会导致位错蠕变状态下的蠕变变形。最后,根据Ti --- 48Al --- 1Nb合金与Tiz.sbnd; 50.3Al二元合金的蠕变行为比较,讨论了先前的一些观察结果。幂律蠕变方程。可以基于不同的幂定律蠕变常数(可能反映堆垛层错能量的差异)合理化具有相似应力和温度依赖性但在可比较应力-温度范围内具有不同稳态应变率的TiAl合金。

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    Hayes, R. W.; London, B.;

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  • 年度 1992
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