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The Synergistic Role of Mn and Zr/Ti in Producing Θ'/L12 Co-Precipitates in Al-Cu Alloys Mn和Zr/Ti在Al-Cu合金中产生Θ′/L12共析出相中的协同作用
Pub Date : 2020-03-06 DOI: 10.2139/ssrn.3547686
J. Poplawsky, A. Shyam, L. Allard, Dongwon Shin, P. Shower, M. Chisholm
Microstructural stability is a critical factor to consider when designing new alloys for high-temperature applications. An Al-Cu alloy with Mn and Zr additions has recently been developed to withstand extended exposures of up to 350 °C. The addition of Mn in combination with Zr and their segregation to precipitate interfaces play a significant role in stabilizing the metastable θ' precipitates responsible for the alloy's hardness; however, adding Zr and Mn separately only improves the stability to 200 °C and 300 °C, respectively. To this end, the effect of the synergistic additions on interfacial structure and chemistry was studied in detail using atom probe tomography and scanning transmission electron microscopy for Al-Cu-Mn-Zr/Ti-containing alloys subjected to long-term annealing (up to 2,100 h) in the critical temperature range, 300 °C and 350 °C, to investigate the role of Zr/Ti in increasing the θ'-precipitate stability. The results reveal how the addition of Mn allows Zr to segregate to θ' interfaces and eventually create a θ'/Al3(Zrx,Ti1-x) L12 co-precipitate structure along the interface. The co-precipitate is highly stable, as shown by density functional theory calculations, and is a key factor that governs microstructural stability beyond 300 °C. This study reveals how solute additions with different stabilization mechanisms can work in concert to stabilize a desired microstructure, the results provide insights that can be applied to other high-temperature alloy systems.
显微组织稳定性是设计用于高温应用的新合金时要考虑的一个关键因素。最近开发了一种添加Mn和Zr的Al-Cu合金,可以承受高达350°C的长时间暴露。Mn与Zr的结合及其析出界面的偏析对稳定合金的亚稳θ′析出起重要作用;而单独添加Zr和Mn只能分别提高200°C和300°C的稳定性。为此,利用原子探针层析成像和扫描透射电镜对Al-Cu-Mn-Zr/Ti合金在300℃和350℃的临界温度范围内长期退火(长达2100 h)的界面结构和化学性质进行了详细研究,以探讨Zr/Ti在提高θ′-析出稳定性中的作用。结果揭示了Mn的加入如何使Zr向θ′界面偏析,并最终沿界面形成θ′/Al3(Zrx,Ti1-x) L12共析出结构。密度泛函理论计算表明,共析出物高度稳定,是300°C以上微观结构稳定性的关键因素。该研究揭示了溶质添加与不同稳定机制如何协同工作以稳定所需的微观结构,结果提供了可应用于其他高温合金体系的见解。
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引用次数: 0
Uncoupling the Effects of Strain Rate and Adiabatic Heating on Strain Induced Martensitic Phase Transformations in Steels 应变速率和绝热加热对钢应变诱导马氏体相变的耦合影响
Pub Date : 2018-11-19 DOI: 10.2139/ssrn.3287363
N. V. Fernandez, T. Nyyssönen, M. Isakov, M. Hokka, V. Kuokkala
In this work, the effects of strain rate and adiabatic heating on the strain induced martensitic phase transformation were uncoupled and individually evaluated. Tension tests were performed at different strain rates ranging from 2x10-4 s-1 to 1400 s-1, covering both isothermal and adiabatic conditions. The adiabatic temperature rise of a sample tested at a high strain rate was replicated with heating resistors in a normally isothermal low strain rate test. This test allows studying the mechanical behavior and microstructural evolution of the material at a very low strain rate at thermal conditions similar to that of a high strain rate test. The phase transformation rates from austenite to α'-martensite were measured with the magnetic balance method. The phase transformation rate drops significantly with increasing strain rate, and the effect of adiabatic heating seems to be much smaller than the effect of strain rate. At a higher strain rate, the α'-martensite nucleates primarily on a single habit plane parallel to the primary slip plane of the parent austenite, while at a lower strain rate the α'-martensite nucleation occurs on several habit planes. At the studied plastic strains, the strain rate seems to have a stronger effect on the α'-martensite formation than the adiabatic heating. This is supported by thermodynamic stacking fault calculations, which indicate that the increase in the stacking fault energy due to adiabatic heating at low strains is small and therefore unlikely the only reason for the reduced phase transformation rate. Therefore, the strain rate itself seems to have an important role in the strain induced martensitic phase transformation rate.
本文对应变速率和绝热加热对应变诱导马氏体相变的影响进行了解耦和单独评价。在2 × 10-4 s-1至1400 s-1的不同应变速率下进行拉伸试验,包括等温和绝热条件。高应变速率下试样的绝热温升用加热电阻在正常等温低应变速率试验中复制。该测试允许在类似于高应变率测试的热条件下,在极低应变率下研究材料的力学行为和微观结构演变。用磁天平法测定了从奥氏体到α′-马氏体的相变速率。随着应变速率的增加,相变速率明显下降,绝热加热的影响似乎远小于应变速率的影响。在较高应变速率下,α′-马氏体主要在与母奥氏体初级滑移面平行的单一习惯面上形核,而在较低应变速率下,α′-马氏体在多个习惯面上形核。在研究的塑性应变下,应变速率似乎比绝热加热对α′-马氏体形成的影响更大。热力学层错计算支持了这一点,表明在低应变下绝热加热引起的层错能增加很小,因此不太可能是相变速率降低的唯一原因。因此,应变速率本身似乎对应变诱发马氏体相变速率起着重要的作用。
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引用次数: 0
Critical Thickness of High Temperature Barrier Coatings of Magnesium Oxychloride Sorrel Cement 氯氧镁酸盐水泥高温阻隔涂层的临界厚度
Pub Date : 2003-02-01 DOI: 10.1115/HT2003-47392
K. Sharma
The critical thickness of high temperature barrier coating is derived to avoid cycling of temperature from the finite speed heat conduction equations. When a cylinder is subject to a step change in temperature at the surface of the cylinder the transient temperature profile is obtained by the method of separation of variables. The finite speed of heat propagation is accounted for by using the modified Fourier’s law of conduction with a heat velocity of √α/τr . In order to avoid pulsations of temperature with respect to time the cylinder has to be maintained at a radius no less than 4.8096√ατr . In the asymptotic limit of infinite heat velocity the governing equation becomes parabolic diffusion equation. In the limit of zero velocity of heat and infinite relaxation time the wave equation result and solution can be obtained by a relativistic coordinate transformation. In the asymptote of zero velocity of heat and zero thermal diffusivity the solution for the dimensionless temperature is a decaying exponential in time. The average temperature of the naval warhead as indicated by UL 1709 test was estimated by using a idealized finite slab, and Leibnitz rule and an analytical expression for the average temperature was obtained using convective boundary condition. The solution is: For 1/2 >= Bi, = exp(−τ(1/2 + sqrt(1/4 − Bi*)))For Bi > 1/2, = exp(−τ/2)Cos(τsqrt(−1/4 + Bi*))) The average temperature is damped oscillatory in time domain. Further the transient temperature profile is represented by an infinite series of decaying exponential in time and Bessel function of the first kind and 0th order. The constant can be obtained from the principle of orthogonality. The bifurcated nature of the exact solution gives rise to the lower limit on the radius to avoid cycling of temperature with respect to time. The exact solution is thus, u = Σ0∝ cn J0 (λn X) exp(−τ(1/2 − sqrt(1/4 − λn2))) and when λn > 1/2 u = Σ0∝ cn J0(λn X) exp(−τ/2 Cos(τsqrt(−1/4 + λn2)) where, λn = (2.4048 + (n−1)π)(√α/τr/R) cn is given by equation (53). The term in the infinite series onward where the contribution is oscillatory is identified.Copyright © 2003 by ASME
从有限速度热传导方程出发,导出了避免温度循环的高温屏障涂层临界厚度。当圆柱体表面温度发生阶跃变化时,用分离变量法得到了瞬态温度分布。热传播的有限速度是用修正的傅立叶传导定律来解释的,热速度为√α/τr。为了避免温度随时间的波动,圆柱体必须保持在不小于4.8096√ατr的半径上。在无限热速的渐近极限下,控制方程变为抛物扩散方程。在零热速和无限松弛时间的极限下,波动方程的结果和解可以通过相对论性坐标变换得到。在零热速和零热扩散系数的渐近线上,无量纲温度的解是一个随时间衰减的指数。采用理想有限板法对ul1709试验显示的舰载战斗部平均温度进行了估计,利用对流边界条件得到了莱布尼茨规则和平均温度的解析表达式。解为:对于1/2 >= Bi, = exp(- τ(1/2 + sqrt(1/4 + Bi*))))对于Bi > 1/2, = exp(- τ/2)Cos(τsqrt(- 1/4 + Bi*)))平均温度在时域内是阻尼振荡的。此外,瞬态温度分布由时间衰减指数的无穷级数和第一类和第0阶贝塞尔函数表示。该常数可由正交原理求得。精确解的分叉性质产生了半径的下限,以避免温度相对于时间的循环。因此,精确解为:u = Σ0∝cn J0(λn X) exp(- τ(1/2 - sqrt(1/4 - λn2)),当λn > 1/2 u = Σ0∝cn J0(λn X) exp(- τ/2 Cos(τsqrt(- 1/4 + λn2))时,λn = (2.4048 + (n−1)π)(√α/τ R /R) cn由式(53)给出。在无穷级数中贡献为振荡的项是确定的。ASME版权所有©2003
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引用次数: 0
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MatSciRN: High-Temperature Intermetallic Materials (Topic)
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