• 마이크로전자및패키징학회지
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• 제21권4호
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• pp.57-62
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• 2014

미래형 유연소자 개발 시 비용감소 및 공정적합성 개선을 위해 동박을 잉크젯 프린팅법을 이용해 공중합체 유연기판 상 형성하고, 전기적 특성에 열처리 분위기가 미치는 영향을 확인하기 위해 3 종류의 환원분위기에서 열처리를 진행하여 보았다. 그 결과 200도의 낮은 온도에서 환원 특성이 뛰어난 포름산 분위기에서 전도체 수준의 비저항은 얻을 수 있었으나, 열처리 시 발생하는 응력으로 인해 발생된 표면균열에 기인해 그 값이 기존 동박에 비해 매우 높았다. 이에 비정질재료에서 응용되는 응력해소법을 응용하여 표면균열을 억제한 결과 230도 열처리 시 기존 열처리 방법에서는 $7.4{\mu}{\Omega}cm$의 비저항을 보이나, 응력해소를 통한 표면 균열이 억제된 시편에서는 $3.4{\mu}{\Omega}cm$의 비저항 값을 얻을 수 있었다. 특히 등온열처리에 의한 응력해소 효과를 확인하기 위해 동일 온도에서 등온시간 없이 열처리를 진행한 결과, 표면균열이 억제되지 못함을 확인할 수 있었다.

• Korean Chemical Engineering Research
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• 제46권2호
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• pp.389-396
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• 2008

벤조시클로부텐(benzocyclobutene; BCB)과 플라즈마 화학기상증착(PECVD)된 산화규소막이 코팅된 웨이퍼들 사이의 계면에서, 고온 열순환 공정에 의한 잔류응력 및 본딩 결합력의 효과를 4점 굽힙시험법과 웨이퍼 곡률 측정법에 의해 평가하였다. 이를 위해 웨이퍼들은 사전에 확립된 표준 본딩공정에 의거하여 본딩하였으며 이들 웨이퍼에 대한 열순환 공정은 상온으로부터 최대 순환온도 사이에서 수행하였다. 최대 온도 350 및 $400^{\circ}C$에서 수행한 열순환 공정에서, 본딩 결합력은 첫번째 순환공정 동안 크게 증가하는 데, 이는 순환공정 시 발생하는 산화규소막의 축합 반응에 의한 잔류응력 감소 때문인 것으로 분석되었다. 이러한 산화규소막의 잔류응력이 감소함에 따라 BCB와 산화규소막으로 구성된 다층막의 잔류응력에 의해 변형되는 에너지는 상승하였고 따라서 BCB와 산화규소막 사이 다층막의 의 본딩 결합력은 증가하였다.

• 한국분말야금학회:학술대회논문집
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• 한국분말야금학회 1996년도 추계학술강연 및 발표대회 강연 및 발표논문 초록집
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• pp.17-17
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• 1996

• 대한기계학회논문집A
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• 제22권1호
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• pp.16-22
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• 1998

This paper addresses a method which can be used for analyzing thermal stresses of a functionally graded material(FGM) using semi-analytical approach. FGM is a nonhomogeneous material whose composition is changed continuously from a metal surface to a ceramic surface. An infinite one dimensional FGM plate is considered. The temperature distribution in the FGM is obtained by approximate Green's function solution. To expedite the convergence of the solutions, alternative Green's function solution is derived and shows good agreement with results from finite difference method. Thermal stresses are calculated using temperature distribution of the plate.

• 수산해양기술연구
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• 제28권1호
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• pp.71-78
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• 1992

Zr-4 used for a cladding and an end plug of reactor component has creep deformation under operation at high temperature. Creep is regarded as the time dependent deformation of a material under constant applied stress. Although the major source of the deformation of zirconium component in water-cooled reactors is irradiation creep, the thermal creep may give a rise to significant deformation in reactor component especially at relatively high temperatures and at various constant stresses, and therefore it must be predicted accurately. Stress relaxation is the time dependent change of stress at constant strain and it is a process related intimately to creep. In this paper, the creep behavior and stress relaxation of Zr-4 is examined at the temperature of 50$0^{\circ}C$ that is 40% of the absolute melting temperature of Zr-4 under the stress below yield stress and under the various constant strains. The results obtained are summarized as follows: 1) With an increase of stress, the steady state creep rate increases and the creep rupture time decreases. 2) The steady state creep rate $\varepsilon$(%/s) for the stress $\sigma$sub(c) (kgf/mm super(2)) of Zr-4 increases outstandingly. All the empirical equations computed for Zr-4 increases outstandingly. All the empirical equations computed for Zr-4 are in accord with Norton's model equation($\varepsilon$=K$\sigma$ sub(c) super (n)). The constants of materials computed are as follows: K=3.9881$\times$10 super(-5), n=1.9608 3) The rupture time T sub(r) (hr) decreases linearly with the increase of stress on the log-log scaled graph. The empirical equations computed for Zr-4 are in accord with Bailey's model equation (T sub(r)=K sub(1)$\sigma$sub(c) super(m)). The constants of materials computed are as follows: K sub(1)=1.2875$\times$10 super(16), m=-3.467 4) It seems clear that the strain could be quantitatively dependent on the high temperature creep properties such as creep stress, rupture time, steady state creep rate and total creep rate. It is found that these relationships are linear on the log-log graph. 5) In stress relaxation test, as the critical constant strain that can be allowed to the specimen is larger, stress relaxation becomes more rapid, and as the constant strain is smaller, the stress relaxation becomes slower.

• 한국기계가공학회지
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• 제6권1호
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• pp.50-56
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• 2007

Exhaust manifold is generally subjected to thermal cycle loadings ; at hot condition, large compressive plastic deformations are generated, and at cold condition, tensile stresses are remained in highly deformed critical zones. These phenomena originate from the fact that thermal expansions of the runners are restricted by inlet flange clamped to the cylinder head, because the former is less stiff than the latter and, the temperature of the inlet flange is lower than that of the runners. Since the failure of an exhaust manifold is mainly caused by geometric constraints between the cylinder head and the manifold, the thermal stress can be controlled by geometric factors. The generic geometric factors include the inter distance (2R), the distance from the head to the outlet (L), the tube diameter(d) and the tube thickness (t). This criteria based on elastic analysis up to onset of yield apparently indicate that the pre-stress also reduces the factor; however, high temperature relaxation may reduce this effect at later operation stage.

• 한국소성가공학회:학술대회논문집
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• 한국소성가공학회 2004년도 춘계학술대회 논문집
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• pp.95-100
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• 2004

An analysis using FEM simulation was conducted to predict residual stresses and birefringence in simple compressed cylindrical glass as a preliminary part of the optimum design determination of optical lenses. The FEM simulation with the Maxwell viscoelastic constitutive model was used to predict thermal induced residual stresses and birefringence during the compression test considering stress relaxation. Also the linear photoelastic theory was introduced to calculate birefringence from the residual stress state. The simulation results were in good agreement with deformation and birefringence distribution in the existing experimental result.

• 소성∙가공
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• 제13권6호
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• pp.509-514
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• 2004

An analysis using FEM simulation was conducted to predict residual stresses and birefringence in simple compressed cylindrical glass as a preliminary part of the optimum design determination of optical lenses. The FEM simulation with the Maxwell viscoelastic constitutive model was used to predict thermal induced residual stresses and birefringence during the compression test considering stress relaxation. Also the linear photoelastic theory was introduced to calculate birefringence from the residual stress state. The error of simulation results between experimental results in the birefringence value at the center of glass specimen is $4.2\%$, and the error in the maximum radius of deformed glass specimen is $1.2\%$. The simulation results were in good agreement with deformation and birefringence distribution in the existing experimental result.

• 대한기계학회논문집A
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• 제26권11호
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• pp.2342-2354
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• 2002

The present study has numerically predicted both the flow -induced and thermally-induced residual stresses and birefringence in injection o. injection/compression molded center -gated disks. Analysis system for entire molding process was developed based on an ap propriate physical modeling including a nonlinear viscoelastic fluid model, stress-optical law, a linear viscoelastic solid model, free volume theory for density relaxation phenomena and a photoviscoelasticity and so on. Part I presents physical modeling a nd typical numerical analysis results of residual stresses and birefringence in the injection molded center-gated disk. Thermal residual stress was found to be extensional near the center, compressive near the surface and tend to become toward tensional at the surface. A double-hump profile was obtained across the thickness in birefringence distribution: nonzero birefringence is found to be thermally induced, the outer peak is due to the shear flow and subsequent stress relaxation during the filling stage a nd the inner peak is due to the additional shear flow and stress relaxation during the packing stage. Predicted birefringence including both the flow -induced and thermally-induced one becomes quite similar to the experimental one.

• 한국결정성장학회지
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• 제8권4호
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• pp.612-618
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• 1998

$SiCl_4/C_3H_8/H_2$계를 사용하여 흑연기판 위에 순수한 SiC층과 SiC/C FGM층을 CVD법에 의해 증착한 후 thermal shock 시험을 통하여 두 시편의 열적 성질을 조사하였다. Thermal shock 시험시 두가지 시편 내부의 이론적인 열응력 차이를 알아보기 위해 상용프로그램을 이용하여 시편내의 온도분포, 열응력 분포를 계산하였다. SiC/C FGM층을 증착한 시편이 순수한 SiC층을 증착한 시편보다 계산상으로 경계면에서 우수한 열응력 완화효과를 나타내는 것으로 판단되었고 실험적으로로 FGM 시편의 경우 $\Delta$T=1600K의 열충격에도 견딜수 있는 것을 확인하여 이론과 실험이 일치하는 것을 입증하였다.