• 제목/요약/키워드: Barrier coat

검색결과 53건 처리시간 0.019초

Failure Mechanisms of Thermal Barrier Coatings Deposited on Hot Components in Gas Turbine Engines

  • Lee E. Y.;Kim J. H.;Chung S. I.
    • 한국추진공학회:학술대회논문집
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    • 한국추진공학회 2005년도 제24회 춘계학술대회논문집
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    • pp.106-111
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    • 2005
  • Failure mechanisms were investigated for the two layer thermal barrier coatings consisting of NiCrAlY bond coat and $ZrO_2-8wt.\% Y_{2}O_3$ ceramic coating during cyclic oxidation. $Al_{2}O_3$ developed at the ceramic coating/bond coat interface first, followed by the Cr/Ni rich oxides such as $NiCr_{2}O_4 and Ni(Al,Cr)_{2}O_4$ during cyclic oxidation It was observed that the spalling of ceramic coatings took place primarily within the NiCrAlY bond coat oxidation products or at the interface between the bond coat oxidation products and zirconia based ceramic coating or the bond coat. It was also observed that the fracture within these oxidation products occurred with the formation of $Ni(Cr,Al)_{2}O_4$ spinel or Cr/Ni rich oxides. It was therefore concluded that the formation of these oxides was a life-limiting event for the thermal barrier coatings.

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Failure Mechanisms for Zirconia Based Thermal Barrier Coatings

  • Lee, Eui Y.;Kim, Jong H.
    • The Korean Journal of Ceramics
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    • 제4권4호
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    • pp.340-344
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    • 1998
  • Failure mechanisms were investigated for the two layer thermal barrier coatings consisting of NiCrAlY bond coat and $ZrO_2$-8wt.% $Y_2O_3$ ceramic coating during cyclic oxidation. $Al_2O_3$ developed at the ceramic coating/bond coat interface first, followed by the Cr/Ni rich oxides such as $NiCr_2O_4$ and $Ni(Al, Cr)_2O_4$ during cyclic oxidation. It was observed that the spalling of ceramic coatings took place primarily within the NiCrAlY bond coat oxidation products or at the interface between the bond coat oxidation products and zirconia based ceramic coating or the bond coat. It was also observed that the fracture within these oxidation products occurred with the formation of $Ni(Cr, Al)_2O_4$ spinel or Cr/Ni rich oxides. It was therefore concluded that the formation of these oxides was a life-limiting event for the thermal barrier coatings.

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대기플라즈마 용사법으로 제조된 열차폐코팅의 열피로특성 평가 (Thermal Fatigue Behavior of Thermal Barrier Coatings by Air Plasma Spray)

  • 이한상;김의현;이정혁
    • 대한금속재료학회지
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    • 제46권6호
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    • pp.363-369
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    • 2008
  • Effects of top coat morphology and thickness on thermal fatigue behavior of thermal barrier coatings (TBC) were investigated in this study. Thermal fatigue tests were conducted on three coating specimens with different top coat morphology and thickness, and then the test data were compared via microstructures, cycles to failure, and fracture surfaces. In the air plasma spray specimens (APS1, APS2), top coat were 200 and $300{\mu}m$ respectively. The thickness of top coat was about $700{\mu}m$ in the perpendicular cracked specimen (PCS). Under thermal fatigue condition at $1,100^{\circ}C$, the cycles to top coat failure of APS1, APS2, and PCS were 350, 560 and 480 cycles, respectively. The cracks were initiated at the interface of top coat and thermally grown oxide (TGO) and propagated into TGO or top coat as the number of thermal fatigue cycles increased. For the PCS specimen, additive cracks were initiated and propagated at the starting points of perpendicular cracks in the top coat. Also, the thickness of TGO and the decrease of aluminium concentration in bond coat do not affect the cycles to failure.

용사 열차폐 코팅층의 두께가 열응력에 미치는 영향 (A Study on the Effects of the Thickness of Top Coat on the Thermal Stresses of a Sprayed Thermal Barrier Coating)

  • 김형남;양승한
    • 대한용접접합학회:학술대회논문집
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    • 대한용접접합학회 2004년도 춘계 학술발표대회 개요집
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    • pp.223-225
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    • 2004
  • 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.

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NiCoCrAlY 및 NiAl bond coat를 사용한 Thermal Barrier Coating의 고온안정성에 미치는 Pt의 영향 (Effect of Pt on the High Temperature Stability of NiCoCrAlY or NiAl Bond Coat in the Thermal Barrier Coating System)

  • 구성모;김길무
    • 한국재료학회지
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    • 제15권6호
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    • pp.375-381
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    • 2005
  • High temperature oxidation behavior of thermal barrier coating (TBC) system (IN738 substrate + NiCoCrAlY or NiAl bond coat with or without Pt + yttria stabilized zirconia) prepared by air plasma spray (APS) process has been studied in order to understand the effect of Pt addition to bond coat on the stability of TBC system. Specimens were oxidized in thermal cycling and isothermal oxidation test at $1100^{\circ}C$. The Pt addition in TBC system with NiCoCrAlY bond coat showed a longer life time compared to that without addition of Pt. Pt addition to TBC system is believed to help the formation of more stable thermally grown oxide, $Al_2O_3$, at the TBC/bond coat interface, leading to a longer lifetime of TBC system.

전자빔 증착법에 의한 열차폐코팅의 고온 내산화성 평가 (An Evaluation on High Temperature Oxidation Resistance of EB-PVD Thermal Barrier Coatings)

  • 김종하;정세일;이구현;이의열
    • 한국표면공학회지
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    • 제39권4호
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    • pp.147-152
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    • 2006
  • Failure mechanisms of electron beam physical vapor deposited thermal barrier coatings(EB-PVD TBCs) that occur during thermal cyclic oxidation were investigated. The investigations include microstructural degradation of NiCrAIY bond coat, thermally grown oxides(TGOs) along the ceramic top coat-substrate interface and fracture path within TBCs. The microstructural degradation of the bond coat during cyclic oxidation created Al depleted zones, resulting in reduction of NiAl and ${\gamma}$-Ni solid solution phase. It was observed that the fracture took placed primarily within the TGOs or at the interfaces between TGOs and bond coat.

접착 보조제 종류에 따른 고체 추진제 접착 특성 분석 (Analysis of Adhesion Characteristics of Solid Propellants by Kind of Barrier Coat)

  • 장명욱;구명준;윤재호;이덕범
    • 한국추진공학회지
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    • 제24권4호
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    • pp.33-40
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    • 2020
  • 접착 보조제 종류에 따른 고체 추진제, 라이너 그리고 내열재의 접착 특성에 대한 연구를 수행하였다. 추진제/라이너/내열재 간의 가소제 또는 경화제의 이동을 막기 위하여 접착 보조제를 사용하였다. 접착 보조제의 종류는 Isocyanate계를 사용하였으며, 한 분자 내에 Isocyanate의 개수, 분자량에 대하여 접착 특성을 확인하였다. 시험 결과, -NCO기가 많을수록, 접착 보조제의 분자량이 클수록 접착력이 증가하는 것으로 확인하였다. 또한 접착 보조제를 도포한 후 가사시간에 따른 접착력을 비교한 결과, 가사시간이 짧을수록 접착력이 증가하는 것으로 확인되었다.

Bond Coat의 산화가 Thermal Barrier Coating의 파괴에 미치는 영향 (Effect of Oxidation of Bond Coat on Failure of Thermal Barrier Coating)

  • 최동구;최함메;강병성;최원경;최시경;김재철;박영규;김길무
    • 한국세라믹학회지
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    • 제34권1호
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    • pp.88-94
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    • 1997
  • 플라즈마 용사법(plasma spray method)으로 제작된 상용 가스 터빈 연소기의 finned segment의 열차폐용 코팅계, ZrO2-8wt%Y2O3 top coat/Ni-26Cr-5Al-0.5Y bond coat/Hastelloy X superalloy 기판에서 NiCrAlY bond coat의 산화 거동과 열피로 파괴에 대하여 조사하였다. 생성된 bond coat의 주산화물은 NiO, CrO2, Al2O3였다. ZrO2/bond coat계면에서 생성된 산화물의 분포는 고온에서의 사용 전에 이 계면 아래에 얇은 층의 Al2O3가없는 곳에서는 NiO 산화층 및에 Cr2O3와 Al2O3가 혼합된 형태를 나타내었다. 열피로에 의해 박리된 시편의 파면을 관찰한 결과, 파괴는 주로 ZrO2/산화층 계면보다 세라믹층내로 약간 치우쳐서 일어나지만, 산화층 내에서도 약간 일어남을 알 수 있었다.

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Evaluation of Degradation Characteristics of Thermal Barrier Coating on Gas Turbine Blades

  • Jung, Yongchan;Kim, Mintae;Lee, Juhyeung;Ahn, Jamin;Kim, Kihong
    • KEPCO Journal on Electric Power and Energy
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    • 제2권2호
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    • pp.273-278
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    • 2016
  • In order to evaluate the lifespan of high-temperature parts with thermal barrier coating in gas turbines used for power generation, this study was performed on an 80 MW-class gas turbine exceeding 24 k equivalent operating hours. Degradation characteristics were evaluated by analyzing the YSZ (Yttria Stabilized Zirconia) top coat, which serves as the thermal barrier coating layer, the NiCrAlY bond coat, and interface layers. Microstructural analysis of the top, middle, and bottom sections showed that Thermal Growth Oxide (TGO) growth, Cr precipitate growth within the bond coat layer, and formation of diffusion layer occur actively in high-temperature sections. These microstructural changes were consistent with damaged areas of the thermal barrier coating layer observed at the surface of the used blade. The distribution of Cr precipitates within the bond coat layer, in addition to the thickness of TGO, is regarded as a key indicator in the evaluation of degradation characteristics.

Growth Behavior of Thermally Grown Oxide Layer with Bond Coat Species in Thermal Barrier Coatings

  • Jung, Sung Hoon;Jeon, Soo Hyeok;Park, Hyeon-Myeong;Jung, Yeon Gil;Myoung, Sang Won;Yang, Byung Il
    • 한국세라믹학회지
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    • 제55권4호
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    • pp.344-351
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    • 2018
  • The effects of bond coat species on the growth behavior of thermally grown oxide (TGO) layer in thermal barrier coatings (TBCs) was investigated through furnace cyclic test (FCT). Two types of feedstock powder with different particle sizes and distributions, AMDRY 962 and AMDRY 386-4, were used to prepare the bond coat, and were formed using air plasma spray (APS) process. The top coat was prepared by APS process using zirconia based powder containing 8 wt% yttria. The thicknesses of the top and bond coats were designed and controlled at 800 and $200{\mu}m$, respectively. Phase analysis was conducted for TBC specimens with and without heat treatment. FCTs were performed for TBC specimens at $1121^{\circ}C$ with a dwell time of 25 h, followed by natural air cooling for 1 h at room temperature. TBC specimens with and without heat treatment showed sound conditions for the AMDRY 962 bond coat and AMDRY 386-4 bond coat in FCTs, respectively. The growth behavior of TGO layer followed a parabolic mode as the time increased in FCTs, independent of bond coat species. The influences of bond coat species and heat treatment on the microstructural evolution, interfacial stability, and TGO growth behavior in TBCs are discussed.