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XRD线形傅氏分析方法研究TA15合金热压缩变形后的位错 被引量:6

Research on Dislocations for Hot Compressively Deformed TA15 Alloy by X-ray Diffraction Method and a Profile Analysis Theory
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摘要 利用XRD线形傅氏分析方法定量分析TA15合金在750、800和925℃热压缩变形后的位错亚结构。结果表明:利用XRD线性傅氏分析的方法可以比较方便地定量表征位错信息:位错类型主要为基面(0002)、柱面(1010)和锥面(1011)型位错。存750℃、1s^-1变形条件下,随应变量的增加,直到60%变形量时,位错密度仍在增加。而在800℃、1s^-1变形条件下,位错密度先增加后降低。各变形条件下位错密度均在10^10-10^11cm^-2的范围;750℃变形后,各晶面的位错密度随应变量增加而增加,但是基面(0002)和锥面(1011)位错随应变量的增加的速度更快,说明此温度下基面和锥面位错更易滑移;800℃变形后锥面位错密度随着应变量增加稍有增加,而柱面(1010)和基面(0002)的变化很大。 The dislocation sub-structures for TA 15 alloy by hot-compressive deformation were analyzed quantitatively by X-ray diffraction method and a profile analysis theory. The results showed that it is convenient to analyze dislocation by X-ray diffraction method and a profile analysis theory; The primary dislocations constitute of (0002), (1010) and (1011 ) type for deformed TA15 alloy. Dislocation density increases with increasing strain up to 60% at the deformation temperature of 750 ℃ and strain rate of 1s^-1, while increases first followed by decreases under the condition of 800℃ and 1 sl. And the dislocation density falls into the range of 10^10-10^11cm^-2 for all deformation condition. All types of dislocations show an increase in densities, especially (0002) and (10 11 )type dislocation at 750 ℃, suggesting that (0002) and (10 11 ) type dislocations are easy to operate at this temperature. And (1010) and (0002) type dislocations present a sharper change than that of (1011 ) type dislocations at 800 ℃.
机构地区 哈尔滨工业大学
出处 《稀有金属材料与工程》 SCIE EI CAS CSCD 北大核心 2008年第9期1505-1509,共5页 Rare Metal Materials and Engineering
关键词 TA15合金 热压缩变形 XRD线性傅氏分析方法 位错 TA 15 alloy hot-compressive deformation XRD profile analysis theory dislocation
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