• 제목/요약/키워드: Lead tungsten oxide

검색결과 12건 처리시간 0.019초

$PbWO_{4}:Nb$ 단결정의 성장과 그 광학적 특성 (The $PbWO_{4}:Nb$ single crystal growth and its optical properties)

  • 장경동;김도형;양희선;이상걸;박효열;이진호;이동욱;이상윤
    • 한국결정성장학회지
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    • 제9권2호
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    • pp.141-148
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    • 1999
  • Ir 도가니에서 PbO와 $WO_{3}$를 50 %~50 % 혼합한 시료로 부터 쵸코랄스키 성장방법에 의해 고품질의 순수한 $PbWO_{4}$와 Nb 도핑한 $PbWO_{4}$를 성장 시켰다. 결정은 성분의 선택적 결손에 부합하는 화학양론적 변화는 $PbWO_{4}$의 노란색 형성에 원인이 되었다. X선 회절 실험을 통해서 각 $PbWO_{4}$ 결정의 격자상수 변화를 조사하였으며 광발광, 광흡수 및 라만 스펙트럼에 대한 특성들에 대해 조사를 하였다. 광발광은 10 K~300 K 온도 영역에서 측정 되었으며 낮은 온도 영역에서는 미흡한 온도의존성을 보였으며 200 K 온도 이상에서는 열적소광에 의한 광발광 강도의 감소를 보였다. PL 강도와 반치폭의 온도 의존성으로 부터 각 PWO 시료에 대한 활성화 에너지, Huang-Rhys 결합상수, 비균질선폭계수를 구하였다.

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WELD REPAIR OF GAS TURBINE HOT END COMPONENTS

  • Chaturvedi, M.C.;Yu, X.H.;Richards, N.L.
    • 대한용접접합학회:학술대회논문집
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    • 대한용접접합학회 2002년도 Proceedings of the International Welding/Joining Conference-Korea
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    • pp.235-243
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    • 2002
  • Ni-base superalloys are used extensively in industry, both in aeroengines and land based turbines. About 60% by weight of most modern gas turbine engine structural components are made of Ni-base superalloys. To satisfy practical demands, the efficiency of gas turbine engines has been steadily and systematically increased by design modifications to handle higher turbine inlet or firing temperatures. However, the increase in operating temperatures has lead to a decrease in the life of components and increase in costs of replacement. Moreover, around 80% of the large frame size industrial/utility gas turbines operating in the world today were installed in the mid-sixties to early seventies and are now 25 to 30 years old. Consequently, there are greater opportunities now to repair and refurbish the older models. Basically, there are two major factors influencing the weldability of the cast alloys: strain-age cracking and liquation cracking. Susceptibility to strain-age cracking is due to the total Ti plus AI content of the alloy; Liquation cracking is due either to the presence of low melting constituents or constitutional liquation of constituents. Though Rene 41 superalloy has 4.5wt.% total Ti and Al content and falls just below the safe limit proposed by Prager et al., controlled grain size and special heat treatments are needed to obtain crack-free welds. Varying heat treatments and filler materials were used in a laboratory study, then the actual welding of service parts was carried out to verity the possibility of crack-tree weld of components fabricated from Rene 41 superalloy. The microstructural observations indicated that there were two kinds of carbides in the FCC matrix. MC carbides were located along the grain boundaries, while M$_{23}$C$_{6}$ carbide was located both inter and intra granularly. Two kinds of filler materials, Rene 41 and Hastelloy X were used to gas tungsten arc weld a patch into the sheet metal, along with varying pre-weld heat treatments. The microstructure, hardness and tensile tests were determined. The service distressed parts were categorized into three classes: with large cracks, with medium cracks and with small or no visible cracks. No significant difference in microstructure among the specimens was observed. Specimens were cut from the corner and the straight edge of the patch repair, away from the corner. The only cracks present were found to be associated with inadequate surface preparation to remove oxidation. Guidelines for oxide removal and the welding procedures developed in the research enabled crack-free welds to be produced.d.

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