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激光沉積TC4/TC11梯度材料組織與疲勞性能研究
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作者單位:

1.沈陽航空航天大學(xué) 機(jī)電工程學(xué)院;2.沈陽工程學(xué)院;3.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(yàn)室

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中圖分類號(hào):

TG146.2

基金項(xiàng)目:

國家重點(diǎn)研發(fā)計(jì)劃項(xiàng)目(2017YFB1104002);工信部民用飛機(jī)專項(xiàng)科研項(xiàng)目(MJZ-2016-G-71);遼寧省教育廳科學(xué)研究項(xiàng)目(L201738和LQN201722),航空制造工藝數(shù)字化國防重點(diǎn)學(xué)科實(shí)驗(yàn)室開放基金(SHSYS2017007)


Microstructure and fatigue properties of TC4/TC11 gradient materials by laser deposition
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Affiliation:

1.School of Mechatronics Engineering,Shenyang Aerospace University;2.Key Laboratory of Fundamental Science for National Defense of Aeronautical Digital Manufacturing Process,Shenyang Aerospace University

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    摘要:

    為了研究激光沉積TC4/TC11鈦合金梯度材料的組織與疲勞性能,采用激光沉積制造技術(shù)制備兩種不同過渡方式的TC4/TC11復(fù)合材料。觀察不同過渡方式復(fù)合材料的顯微組織,測(cè)試兩種復(fù)合材料分別在550Mpa和800Mpa下的疲勞性能,并對(duì)疲勞斷口進(jìn)行分析。結(jié)果表明,相比直接過渡的復(fù)合材料,具有3層過渡層梯度材料的顯微組織過渡界面不明顯,過渡區(qū)組織結(jié)合緊密;具有3層過渡層的梯度材料在兩種應(yīng)力下的疲勞壽命均比直接過渡的高,低應(yīng)力下相對(duì)提高了129.3%,高應(yīng)力下相對(duì)提高了81.8%;直接過渡復(fù)合材料在裂紋擴(kuò)展時(shí)沿著α片層集束開裂,滑移面較大,疲勞壽命較低;具有3層過渡層的梯度材料,裂紋擴(kuò)展沿著單個(gè)α片層滑移開裂,滑移面小,裂紋擴(kuò)展路徑比較曲折,疲勞壽命高。

    Abstract:

    In order to study the microstructure and fatigue properties of laser deposited TC4/TC11 gradient materials, directly transited and gradiently transited TC4/TC11 composite materials were prepared by laser deposition manufacturing technology. The microstructures of composite materials by different transition were observed, the fatigue properties of these two composite materials under stresses of 550 MPa and 800 MPa were tested, and fatigue fractures were analyzed. The results show that the interface of the microstructure of the gradient material with 3 transition layers is not obvious, and microstructures of TC4 and TC11 are integrated more tightly in the transition zone than that of the directly transition composite materials. The fatigue life of the gradient material with 3 transition layers under either stress is higher than that of the direct transition, which is relatively increased by 129.3% under low stress and 81.8% under high stress. The direct transition composite material cracks along the bunch of α-sheet during crack propagation, with a large sliding surface and a low fatigue life. The cracks of gradient material with 3 transition layers grow along a single α-sheet, the slip plane is small, and the crack propagation path is more tortuous, which improves the fatigue life.

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引用本文

何波,雷濤,孫長青,楊光.激光沉積TC4/TC11梯度材料組織與疲勞性能研究[J].稀有金屬材料與工程,2019,48(9):3048~3054.[He Bo, Lei Tao, Sun Changqing, Yang Guang. Microstructure and fatigue properties of TC4/TC11 gradient materials by laser deposition[J]. Rare Metal Materials and Engineering,2019,48(9):3048~3054.]
DOI:10.12442/j. issn.1002-185X.20180389

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歷史
  • 收稿日期:2018-04-17
  • 最后修改日期:2018-06-03
  • 錄用日期:2018-07-24
  • 在線發(fā)布日期: 2019-10-09
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