• 제목/요약/키워드: Nano-Fractography

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알루미늄 합금 피로 스트라이에이션의 나노 스케일 관찰 (Nano-Scale Observation of Fatigue Striations for Aluminum Alloy)

  • 최성종;권재도
    • 대한기계학회:학술대회논문집
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    • 대한기계학회 2000년도 춘계학술대회논문집A
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    • pp.153-158
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    • 2000
  • Atomic Force Microscope (AFM) was used to study cross sectional profiles and dimensions of fatigue striations in 2017-T351 aluminum alloy. Their widths (SW) and heights $(SH,\;SH_h)$ were measured from the cross sectional Profiles of three-dimension AFM images. The following results that will be helpful to understand the fatigue crack growth mechanism were obtained. (1) Coincidence of the crack growth rate with the striation width was found down to the growth rate of $10^{-5}$ mm/cycle. (2) The relation of $SH={\alpha}(SW)^{1.2}$ was obtained. (3) The ratio of the striation height to its width SH/SW and did not depend on the stress intensity factor range ${\Delta}K$ and the stress ratio R. From these results, the applicability of the AFM to nano-fractography is discussed.

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원자력 현미경(AFM)에 의한 알루미늄 합금의 피로 스트라이에이션 관찰 (The Observation of Fatigue Striations for Aluminum Alloy by Atomic Force Microscope(AFM))

  • 최성종;권재도
    • 대한기계학회논문집A
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    • 제24권4호
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    • pp.955-962
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    • 2000
  • Scanning Probe Microscope (SPM) such as Scanning Tunneling Microscope (STM) and Atomic Force Microscope (AFM) was shown to be the powerful tool for nano-scale characterization of a fracture surface . AFM was used to study cross sectional profiles and dimensions of fatigue striations in 2017-T351 aluminum alloy. Their widths (SW) and heights (SH) were measured from the cross sectional profiles of three-dimension AFM images. The following results that will be helpful to understand the fatigue crack growth mechanism were obtained. (1) Coincidence of the crack growth rate with the striation width was found down to the growth rate of 10-5 mm/cycle. (2) The relation of SH=0.085(SW)1.2 was obtained. (3) The ratio of the striation height to its width SH/SW did not depend on the stress intensity factor range K and the stress ratio R. (4) Not only the SW but also the SH changed linearly with the crack tip opening displacement (CTOD) when plotted in log-log scale. From these results, the applicability of the AFM to nano-fractography is discussed.

알루미늄 합금 피로 스트라이에이션의 나노 스케일 관찰 (Nano-Scale Observation of Fatigue Striations for Aluminum Alloy)

  • 최성종;권재도
    • 대한기계학회논문집A
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    • 제25권7호
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    • pp.1047-1054
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    • 2001
  • Atomic Force Microscope (AFM) was used to study cross sectional profiles and dimensions of fatigue striations in 2017-T351 aluminum alloy. Their widths(SW) and heights (SH, SH(sub)h, SH(sub)ι) were measured from the cross sectional profiles of three-dimension AFM images. The following results that will be helpful to understand the fatigue crack growth mechanism were obtained. (1) The relation of SH=$\alpha$(SW)(sup)1.2 was obtained. (2) The ratio of the striation height to its width SH/SW, SH(sub)h/SW and SH(sub)ι/SW did not depend on the stress intensity factor range ΔK and the stress ratio R( =P(sub)min/P(sub)max = K(sub)min/K(sub)max). (3) Effect of precipitate on the morphology of striation was changed by the relative dimensional difference between the striation width SW and the precipitates. From these results, the applicability of the AFM to nano-fractography is discussed.

Effects of Tungsten Addition on Tensile Properties of a Refractory Nb-l8Si-l0Ti-l0Mo-χW (χ=0, 5, 10 and 15 mot.%) In-situ Composites at 1670 K

  • 김진학;Tatsuo Tabaru;Hisatoshi Hirai
    • 소성∙가공
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    • 제8권3호
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    • pp.233-233
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    • 1999
  • To investigate the effect of tungsten addition on mechanical properties, we prepared refractory (62χ)Nb-18Si-l00Mo-l0Ti-χW (χ=0, 5, 10 and 15 mol.%) in-situ composites by the conventional arc-casting technique, and then explored the microstructure, hardness and elastic modulus at ambient temperature and tensile properties at 1670 K. The microstructure consists of relatively fine (Nb, Mo, W, Ti)/sub 5/Si₃, silicide and a Nb solid solution matrix, and the fine eutectic microstructure becomes predominant at a Si content of around 18 mol.%. The hardness of (Nb, Mo, W, Ti(/sub 5/Si₃, silicide in a W-free sample is 1680 GPa, and goes up to 1980 GPa in a W 15 mol.% sample. The hardness, however, of Nb solid solution does not exhibit a remarkable difference when the nominal W content is increased. The elastic modulus shows a similar tendency to the hardness. The optimum tensile properties of the composites investigated are achieved at W 5 mol.% sample, which exhibits a relatively good ultimate strength of 230 MPa and an excellent balance of yield strength of 215 MPa, and an elongation of 3.7%. The SEM fractography generally indicates a ductile fracture in the W-free sample, and a cleavage rupture in W-impregnated ones.

$Al_2O_3/ZrO_2$복합체의 기계적 물성 및 파괴거동 (Mechanical Properties and Failure Analysis of $Al_2O_3/ZrO_2$ Composites)

  • 홍기곤;한동빈
    • 한국재료학회지
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    • 제2권3호
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    • pp.172-179
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    • 1992
  • $Al_2O_3/ZrO_2$복합분말에 상릉분말을 침가하여 상압소결법으로 $Al_2O_3/ZrO_2$복합체를 제조한 후, 밀도, 강도, 경도 및 파괴인성등의 물성을 측정하였으며 미세구조 및 파괴단면도 관찰하였다. 상용분말의 침가량이 중량비로 50%이하인 경우에는 평균 꺽임 강도가 640 MPa정도로 거의 변화가 없었으며, 50%이상 첨가된 경우에는 강도가 저하되었는데, 이는 미세조직과 관계가 있는 것으로 생각된다. 또한 파괴인성(4.3-5.3 $Mpam^{1/2}$)값은 상용분말 첨가량에 비례하여 증가하였다. 파괴단면 관찰결과 파괴원인으로는 가공에서 생기는 표면 결함, $ZrO_2$ agglomeration에 의한 crack-like void 및 $Al_2O_3/ZrO_2$ nano복합체 분말과 상용분말간의 소결성 차이에서 생기는 계면 분리등이 관찰되었는데, nano 복합 분말만을 사용한 소결체에서는 가공에 의한 표면 결함만이 파괴원으로 작용하였다. 또한, 파괴형태는 주로 transgranular fracture이었다

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고진공 고압 다이캐스팅으로 제조된 AA365 합금의 미세조직과 기계적 특성에 미치는 T6 열처리의 영향 (Effect of T6 heat treatment on the microstructure and mechanical properties of AA365 alloy fabricated by vacuum-assisted high pressure die casting)

  • 전준협;손승배;이석재;정재길
    • 열처리공학회지
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    • 제37권3호
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    • pp.121-127
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    • 2024
  • We investigate the effect of T6 heat treatment on the microstructure and mechanical properties of AA365 (Al-10.3Si-0.37Mg-0.6Mn-0.11Fe, wt.%) alloy fabricated by vacuum-assisted high pressure die casting by means of thermodynamic calculation, X-ray diffraction, scanning and transmission electron microscopy, and tensile tests. The as-cast alloy consists of primary Al (with dendrite arm spacing of 10~15 ㎛), needle-like eutectic Si, and blocky α-AlFeMnSi phases. The solution treatment at 490 ℃ induces the spheroidization of eutectic Si and increase in the fraction of eutectic Si and α-AlFeMnSi phases. While as-cast alloy does not contain nano-sized precipitates, the T6-treated alloy contains fine β' and β' precipitates less than 20 nm that formed during aging at 190℃. T6 heat treatment improves the yield strength from 165 to 186 MPa due to the strengthening effect of β' and β' precipitates. However, the β' and β' precipitates reduce the strain hardening rate and accelerate the necking phenomenon, degrading the tensile strength (from 290 to 244 MPa) and fracture elongation (from 6.6 to 5.0%). Fractography reveals that the coarse α-AlFeMnSi and eutectic Si phases act as crack sites in both the as-cast and T6 treated alloys.