• 대한기계학회:학술대회논문집
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• 대한기계학회 2000년도 춘계학술대회논문집A
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• pp.188-193
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• 2000

A more accurate life prediction for gas turbine blade takes into account the material behavior under the complex thermo-mechanical fatigue(TMF) cycles normally encountered in turbine operation. An experimental program has been carried out to address the thermo-mechanical fatigue life of the IN738LC nickel-base superalloy. In the first phase of the study, out-of-phase and in-phase TMF experiments have been performed on uncoated and coated materials. In the temperature range investigated. the deposition of NiCrAlY air plasma sprayed coating did not affect the fatigue resistance. In the second phase of the study, a physically-base life prediction model that takes into account of the contribution of different damage mechanisms has been applied. This model was able to reflect the temperature and strain rate dependences of isothermal cycling fatigue lives, and the strain-temperature history effect on the thermo-mechanical fatigue lives.

• 비파괴검사학회지
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• 제33권1호
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• pp.46-53
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• 2013

Impedance spectroscopy is a non-destructive evaluation (NDE) method first proposed and developed for evaluating TGO layers with compressive stress inside thermally degraded plasma-sprayed thermal barrier coatings (PS TBCs). A bode plot (phase angle (h) vs. frequency (f)) was used to investigate the TGO layer on electrical responses. In our experimental study, the phase angle of Bode plots is sensitive for detecting TGO layers while applying compressive stress on thermal barrier coatings. It is difficult to detect TGO layers in samples isothermally aged for 100 hrs and 200 hrs without compressive stress, and substantial change of phase was observed these samples with compressive stress. Also, the frequency shift of the phase angle and change of the phase angle are observed in samples isothermally aged for more than 400 hrs.

• 한국융합학회논문지
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• 제12권12호
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• pp.145-151
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• 2021

Ti Gr4에 TPS 법을 이용하여 HA 코팅을 수행하여 코팅층에 대한 물리적특성 및 생체적합성을 판단하여 의료용 부품으로서의 활용성에 대한 평가를 하였다. 직경 25mm Ti Gr4 합금 시험편을 기계가공 후 #120, #400, #1,000 샌드페이퍼 및 바렐 연마로 표면을 연마를 하여 ASTM F1185-88로 HA 코팅은 한 후 HA 코팅층의 두께, 표면조도, 강도 및 접착력 측정 시험과 세포독성 시험을 하였다. Ti Gr4에 대한 HA 코팅 결정도는 75.51%, Ca/P 비는 1.67의 값을 얻을 수 있었다. HA 코팅층의 두께는 Ti 소재의 표면거칠기가 거칠수록 증가하고, 코팅의 강도 및 접착력은 시험장치의 지그 형상, 에폭시 성분, 크로스헤드 속도 등에 따라 변화가 있을 것으로 예측된다. 세포독성 시험은 Grade 3의 반응성으로 적합한 것으로 나타났다. 본 실험 결과 TPS에 의한 Ti Gr4 소재의 HA 코팅 두께 향상과 골융합을 촉진이 가능할 것으로 확인되어 인체삽입용으로 상용화가 가능할 것으로 판단된다.

• 한국표면공학회지
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• 제30권4호
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• pp.272-280
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• 1997

The Thermal Barrier Coation(TBC) to improve the that barrier and wear resistant propenrty in high temperature ofthe aircraftength between the accumlation of the aircraft engine and the automobile engine has usually the two layer structure. One is a creamic top layer for heat insulation and the other is a metal bond layer to facilitate the bond strength between the top ceramic layer and the substrate. But, the coated layers should be peeled off because of the accumulation of the thermal stress by the differance of the thermal expantion coefficient between metal and ceramics in a hrat cyclic environment. In this study, the intermediate layer by plasm spray process was introduced to reduce the thermal stress. The powders of plasm spray coating were the Yttria Stabilized Zirconia (YSZ), the Magnesia Stabillized Zirconia(MSZ) and NiCrAlY. the intermediate layer was sprayed with the powders of the bond cast for the purpose of test were executed. The high temperature wear resistance tends to decreasnceee wear and thermal shock test were exeucuted. The high temperature were resistance of the YSZ TBC is better that of the MSZ TBC. The wearrsistance tends to decrease accoring to incresing the temperature between $400^{\circ}C$to $600^{\circ}C$. The thermal shock life of the 3 layer TBC with YSZ top casting was the most outstanding thermal shock rsisstasnce. This means that the intermediate layer should play an importnat roll to alleviate the diffrerence of the thermal expansion coef frcients between metallic layer and cermics layer.

• Journal of Welding and Joining
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• 제26권4호
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• pp.50-54
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• 2008

In this research, anode for SOFC has been manufactured from two different kinds of feedstock materials through thermal spraying process and the properties of the coatings were characterized and compared. One kind of feedstock was manufactured from spray drying method which includes nano-components of NiO, YSZ (300 nm) and graphite. And the other is manufactured by blending the micron size NiO coated graphite, YSZ and graphite powders as feedstock materials. Microstructure, mechanical properties and electrical conductivity of the coatings as-sprayed, after oxidation and after hydrogen reduction containing nano composite which is prepared from spray-dried powders were evaluated and compared with the same properties of the coatings prepared from blended powder feedstock. The coatings prepared from the spray dried powders has better properties as they provide larger triple phase boundaries for hydrogen oxidation reaction and is expected to have lower polarization loss for SOFC anode applications than that of the coatings prepared from blended feedstock. A maximum electrical conductivity of 651 S/cm at $800^{\circ}C$ was achieved for the coatings from spray dried powders which much more than that of the average value.

• 한국세라믹학회지
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• 제39권6호
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• pp.582-588
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• 2002

Ti 기판에 TiO$_2$ 중간층을 플라즈마 용사법으로 증착 후 IrO$_2$-RuO$_2$ 박막을 졸-겔과 dip coating법으로 제조하였다. 코팅 층의 접착력을 향상시키기 위하여 유기화합물과 glass brit을 첨가하였다. Taguchi법의 망대특성과 Lls(2$^1$$\times$3$^{7}$ )의 직교배열표를 이용하여 IrO$_2$-RuO$_2$ 박막의 최적조건인 인자와 수준 조합의 최적화를 전류밀도를 측정 분산분석하였다. 최적의 코팅조건은 각각 ethyl cellulose의 점도는 100cp, 건조온도 및 시간은 17$0^{\circ}C$ 20분, 열처리온도 및 시간은 75$0^{\circ}C$ 10분, 전도성 분말과 glass frit의 무게비는 99:5, 최종열처리시간은 120분, 주입산소량은 5sccm이었다. 분산분석결과, 유의수준이 $\alpha$=0.1인 통계적으로 90%신뢰공정이었다.

• 방사성폐기물학회지
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• 제8권1호
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• pp.33-39
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• 2010

산화물 사용 후 핵연료를 처리하는 전해환원공정에서는 LiCl 용융염계에서 산소가 생성되는 반응을 수반하게 되며, 생성된 산소로 인해 반응기의 구조재료를 상당히 부식시킬 수 있는, 화학적으로 심각한 반응환경을 조성한다. 따라서, 고온 용융염을 다루는 전해환원 공정장치를 위해서는 최적의 재료를 선택하는 것이 필수적이다. 본 연구에 서는 리튬용융염, $675^{\circ}C$, 216시간동안 산화분위기에서 코팅이 안 된 초합금과 코팅된 초합금 시편의 고온 부식연구를 수행하였다. IN713LC 초합금 시편에 aluminized NiCrAlY bond 코팅 후 $Y_2O_3$ top 코팅을 하였다. 코팅이 안 된 초합금은 부식층의 빠른 성장응력과 열적응력에 의한 부식층의 박리로 명확한 무게손실을 보인다. 탑 코팅의 화학적 및 열적 안정성으로 인해 고온 리튬용융염을 다루는 구조재료의 부식 저항성이 증가함을 확인할 수 있었다.