• 한국세라믹학회지
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• 제53권6호
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• pp.628-634
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• 2016

The 8 wt% yttria($Y_2O_3$) stabilized zirconia ($ZrO_2$), 8YSZ, a typical thermal barrier coating (TBC) for turbine systems, was fabricated under different starting powder conditions and coating parameters by atmospheric plasma spray (APS) coating process. Four different starting powders were prepared by conventional spray dry method with different additive and process parameter conditions. As a result, large- and small-size spherical-type particles and Donut-type particles were obtained. Dense structure of 8YSZ coating was produced when small size spherical-type or Donut-type particles were used. On the other hand, 8YSZ coating with a porous structure was formed from large-size spherical-type particles. Furthermore, a segmented coating structure with vertical cracks was observed after post heat treatment on the surface of dense structured coating by argon plasma flame at an appropriate gun distance and power condition.

• 한국추진공학회:학술대회논문집
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• 한국추진공학회 2017년도 제48회 춘계학술대회논문집
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• pp.392-394
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• 2017

본 연구에서는 가변 추력기 3D 모델에 대해 CFD를 이용하여 고온 고압 환경에서의 추력 조절기 표면 열전달 계수를 예측하였다. 추력 조절기 표면에 열차폐코팅(TBC)을 모델링하였고, TBC 코팅의 두께가 추력조절기 내부 온도 분포에 미치는 영향을 연구하였다. TBC층의 두께는 $100{\mu}m{\sim}500{\mu}m$로 변화시켰다. 해석 결과, TBC층의 두께가 증가함에 따라 추력 조절기 표면과 내부 온도는 감소하는 경향을 보였다.

• 한국세라믹학회지
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• 제43권8호
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• pp.479-485
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• 2006

The residual stress changes on thermo-mechanical loading in the interface region of the Thermal Barrier Coating (TBC)/Thermally Grown Oxide (TGO)/Bond Coat (BC) were calculated on the TBC-coated superalloys using a Finite Element Method (FEM). It was found that the residual stress of the interface boundary was dependent upon mainly the oxide formation and the swelling rate of the oxide by creep relaxation. During an oxide swelling, the relaxation of residual stress which is due to creep deformation increased the TBC's life. In the case of the fine grain size of TGO scale, the TBC stresses piled up by oxide swelling could be relaxed by diffusional creep effect of TGO.

• 한국추진공학회지
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• 제13권6호
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• pp.17-23
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• 2009

정확한 추력 및 비추력 특성을 파악하기 위하여 액체로켓엔진용 연소기에 추가적으로 임시 노즐확장부를 장착함에 있어, 그 열/구조적 건전성을 파악하였다. 이 열/구조적 건전성은 재질 및 차폐막(TBC)의 두께 효과를 살펴봄으로써 검토하였다. TBC가 없는 경우에는 열/구조적 건전성을 유지할 수 없음을 파악할 수 있었다. TBC의 두께에 따라서 노즐확장부 벽면에서의 최대온도는 많이 감소하였다. 노즐확장부를 steel로 제작하는 경우에는 TBC를 적용해야만 연소시험동안 확장부의 열/구조적 건전성이 보장될 것으로 예상된다.

• 대한용접접합학회:학술대회논문집
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• 대한용접접합학회 2000년도 특별강연 및 춘계학술발표대회 개요집
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• pp.228-231
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• 2000

Based on the principle of complementary energy an analytical method is developed for determining thermal stress distribution in an thermal barrier coating. This method gives the stress distributions which satisfy the stress-free boundary conditions at the edge. Numerical examples are given in order to verify the method and to investigate the thickness effects of the ZrO$_2$-8wt％Y$_2$O$_3$ top coat on the integrity of thermal barrier coating consisted of IN738LC substrate and MCrAlY bond coat.

• 한국표면공학회지
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• 제45권2호
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• pp.70-74
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• 2012

In thermal barrier coating (TBC) systems, the life of the coating depends on thermally grown oxide (TGO) layer because most of the failure of TBCs occurs when TGO growth increases. In order to inhibit TGO growth, process was additionally carried out before the heat treatment of the TBC coating layer at $1200^{\circ}C$ in air. In the additional process, heat treatment in vacuum furnace of < $10^{-5}$ torr was conducted for 7 h and 14 h before the heat treatment. The area and length of TGO, as well as the crack length in the TBC were characterized using a scanning electron microscope (SEM). The TGO thickness and crack of specimens pre-heat treated in vacuum furnace were reduced by 45% compare to those heat treated in furnace. Consequently, pre-heat treatment in a vacuum furnace process lead to effective inhibition of growth of the TGO.

• 한국유체기계학회 논문집
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• 제18권3호
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• pp.38-45
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• 2015

In this study, two computational methodologies were compared to consider an effective conjugate heat transfer analysis technique for the cooled vane with thermal barrier coating. The first one is the physical modeling method of the TBC layer on the vane surface, which means solid volume of the TBC on the vane surface. The second one is the numerical modeling method of the TBC layer by putting the heat resistance interface condition on the surface between the fluid and solid domains, which means no physical layer on the vane surface. For those two methodologies, conjugate heat transfer analyses were conducted for the cooled vane with TBC layer having various thickness from 0.1 mm to 0.3 mm. Static pressure distributions for two cases show quite similar patterns in the overall region while the physical modeling shows quite a little difference around the throat area. Thermal analyses indicated that the metal temperature distributions are quite similar for both methods. The results show that the numerical modeling method can reduce the computational resources significantly and is quite suitable method to evaluate the overall performance of TBC even though it does not reflect the exact geometry and flow field characteristics on the vane surface.

• 비파괴검사학회지
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• 제36권3호
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• pp.202-210
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• 2016

열차폐코팅은 극한의 열환경에서 사용되는 기계요소를 고온으로부터 보호하기 위하여 널리 이용하는 코팅으로, 관련 산업의 경제적 이윤과 사용자 안전에 관련한 중요한 기술이다. 따라서 이런 열차폐코팅의 비파괴적 손상 평가는 그 중요성이 높이 평가되어 왔으나, 코팅 파쇄의 원인이 되는 내부의 미세한 조성 변화를 감지하기 위한 기술적 난제를 안고 있는 연구 주제이다. 본 논문은 열차폐코팅의 비파괴적 손상 평가를 위한 유한요소해석 기반 고감도 와전류 센서 설계 과정을 소개하고, 설계한 센서를 제작하여 진행한 성능 평가를 통해 설계 과정을 검증하였다. 와전류 센서의 성능을 예측하기 위하여 유한요소해석을 수행한 결과, 열차폐코팅의 손상 정도에 따른 센서의 임피던스가 증가와, 마그네틱 쉴드를 적용하였을 때 자속집속에 의한 검출능 향상을 관찰할 수 있었다. 또한 실제 실험결과와 비교를 통해 유한요소해석 결과를 검증하였다.

• 한국세라믹학회지
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• 제54권6호
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• pp.492-498
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• 2017

A thermal barrier coating (TBC) with self-healing property for cracks was proposed to improve reliability during gas turbine operation, including structural design. Effect of healing agent on crack propagation behavior in TBCs with and without buffer layer was investigated through furnace cyclic test (FCT). Molybdenum disilicide ($MoSi_2$) was used as the healing agent; it was encapsulated using a mixture of tetraethyl orthosilicate and sodium methoxide. Buffer layers with composition ratios of 90 : 10 and 80 : 20 wt%, using yttria stabilized zirconia and $MoSi_2$, respectively, were prepared by air plasma spray process. After generating artificial cracks in TBC samples by using Vickers indentation, FCTs were conducted at $1100^{\circ}C$ for a dwell time of 40 min., followed by natural air cooling for 20 min. at room temperature. The cracks were healed in the buffer layer with the healing agent of $MoSi_2$, and it was found that the thermal reliability of TBC can be enhanced by introducing the buffer layer with healing agent in the top coat.

• 한국세라믹학회지
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• 제43권8호
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• pp.498-503
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• 2006

A gas turbine blade with thermal barrier ceramic coating is operated at high temperature to increase engine efficiency. Recently, thermal barrier characteristics have been improved by advanced coating technology through microstructure control and increase of adhesion force of the coating layer. More advanced coating materials, rare earth zircon ate ceramics have been studied for replacing YSZ coatings as thermal barrier coatings. In this study, $La_2O_3,\;HfO_2,\;CeO_2,\;Gd_2O_3$ and pure or yttria stabilized zirconia were prepared. Microstructure analysis and the evaluation of mechanical properties such as Hertzian indentation and hardness test were performed.