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激光沉積TA15鈦合金退火處理工藝及網(wǎng)籃組織變形機(jī)制研究
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沈陽航空航天大學(xué) 航空制造工藝數(shù)字化國防重點(diǎn)學(xué)科實(shí)驗室,沈陽航空航天大學(xué) 航空制造工藝數(shù)字化國防重點(diǎn)學(xué)科實(shí)驗室,沈陽航空航天大學(xué) 航空制造工藝數(shù)字化國防重點(diǎn)學(xué)科實(shí)驗室,沈陽航空航天大學(xué) 航空制造工藝數(shù)字化國防重點(diǎn)學(xué)科實(shí)驗室,沈陽航空航天大學(xué) 航空制造工藝數(shù)字化國防重點(diǎn)學(xué)科實(shí)驗室,沈陽航空航天大學(xué) 航空制造工藝數(shù)字化國防重點(diǎn)學(xué)科實(shí)驗室

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TG146.2 3

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國家自然科學(xué)(51505301,51305280,51375316);國家重點(diǎn)研發(fā)計劃項目(2016YFB1100500-04)


Study on Annealing Treatment and Basketweave Structure Deformation Mechanism of Laser Deposition Manufacturing TA15 Titanium Alloy
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Key Laboratory of Fundamental Science for National Defence of Aeronautical Digital Manufacturing Process,Shenyang Aerospace University,Key Laboratory of Fundamental Science for National Defence of Aeronautical Digital Manufacturing Process,Shenyang Aerospace University,Key Laboratory of Fundamental Science for National Defence of Aeronautical Digital Manufacturing Process,Shenyang Aerospace University,Key Laboratory of Fundamental Science for National Defence of Aeronautical Digital Manufacturing Process,Shenyang Aerospace University,Key Laboratory of Fundamental Science for National Defence of Aeronautical Digital Manufacturing Process,Shenyang Aerospace University,Key Laboratory of Fundamental Science for National Defence of Aeronautical Digital Manufacturing Process,Shenyang Aerospace University

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    摘要:

    以TA15鈦合金球形粉末為原料,采用激光沉積制造技術(shù)制備TA15鈦合金厚壁件。通過光學(xué)顯微鏡(OM)、掃描電子顯微鏡(SEM)等方法研究了α+β兩相區(qū)退火處理對TA15鈦合金室溫拉伸性能和顯微組織的影響,并對網(wǎng)籃組織在拉伸過程中的變形機(jī)制進(jìn)行討論。結(jié)果表明:經(jīng)α+β兩相區(qū)不同溫度退火后,顯微組織為網(wǎng)籃組織或近網(wǎng)籃組織,退火溫度對α相的形貌尺寸具有明顯影響;退火后力學(xué)性能仍表現(xiàn)出方向上的各向異性:沉積方向上強(qiáng)度較低,塑性較好,而垂直沉積方向上強(qiáng)度高,塑性較差;粗大的層間區(qū)組織滑移變形具有“開路”作用,而柱狀晶晶界對α相的滑移產(chǎn)生一種“固定”作用;顯微硬度值隨退火溫度升高變化不大,顯微硬度值受α相含量影響;網(wǎng)籃組織中的α片層組織在應(yīng)力的作用下由原來近似正交方向逐漸向近似平行于應(yīng)力方向變形,α片層組織的交錯排列導(dǎo)致滑移變形時互相產(chǎn)生阻力;α+β兩相區(qū)退火處理后的兩種方向上斷口形貌相似,斷裂方式相同,均為韌性斷裂。

    Abstract:

    TA15 titanium alloy bulk specimens were prepared by spherical powder in the way of laser deposition manufacturing. The effect of alpha plus beta phase zone annealing treatment on mechanical properties, microstructure of laser deposition manufacturing TA15 titanium alloy and lamellar deformation mechanism has been studied by optical microstructure (OM) and scanning electron microscopy (SEM). The experimental results showed that microstructure was basketweave structure or near basketweave structure after alpha plus beta phase zone annealing treatment, pattern and size of alpha phase was affected effectively by annealing temperature. The mechanical properties after annealing still showed the anisotropy in the different direction: the strength was low and the plasticity was high in deposition direction and the strength was high and the plasticity was low in vertical deposition direction. The interlayer binding zone slip deformation played a vanguard role and the columnar crystal grain boundary had bound effect on alpha phase slip deformation. Microhardness was effected by the amount of alpha phase while it changed little with the increase of annealing temperature. Alpha lamellar in basketweave structure under the stress changed from near orthogonal to near parallel to the direction of stress, staggered arrangement of alpha lamellar generating resistance each other when it was in the state of slip deformation. Both deposition direction and vertical deposition direction had same tensile fracture modes which was ductile fracture after alpha plus beta phase zone annealing treatment.

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楊 光,王文東,欽蘭云,任宇航,李長富,王 維.激光沉積TA15鈦合金退火處理工藝及網(wǎng)籃組織變形機(jī)制研究[J].稀有金屬材料與工程,2017,46(7):1935~1942.[Yang Guang, Wang Wendong, Qin Lanyun, Ren Yuhang, Li Changfu, Wang Wei. Study on Annealing Treatment and Basketweave Structure Deformation Mechanism of Laser Deposition Manufacturing TA15 Titanium Alloy[J]. Rare Metal Materials and Engineering,2017,46(7):1935~1942.]
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  • 收稿日期:2016-07-26
  • 最后修改日期:2016-11-08
  • 錄用日期:2016-11-10
  • 在線發(fā)布日期: 2017-11-14
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