• 제목/요약/키워드: heat shield concept

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Thermal Protection Shield Concept for Diamond Impregnated Tools

  • Tillmann, W.;Gathen, M.;Kronholz, C.
    • 한국분말야금학회:학술대회논문집
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    • 한국분말야금학회 2006년도 Extended Abstracts of 2006 POWDER METALLURGY World Congress Part2
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    • pp.875-876
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    • 2006
  • For dry machining of mineral materials the Institute of Materials Engineering pursues a novel thermal protection shield concept for diamond tools, in which thermal insulating materials in diamond composite structures act as heat shield, which protects diamonds in deeper layers against high temperature and graphitisation. Before the effectiveness of this concept could be investigated suitable composites have to be manufactured. In this paper the powder metallurgical production processes of diamond-alumina-cobalt-composites with varying alumina and cobalt particle sizes, their microstructures and porosities are described. It could be observed that the distribution of small-sized alumina particles ($<70{\mu}m$) in the cobalt matrix is uniform and the porosity of the composite decrease.

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초소형 열광전변환 장치용 열재순환 초소형 이미터 내 연소특성에 관한 연구 (Combustion Characteristics in a Heat-recirculating Microemitter for a Micro Thermophotovoltaic System)

  • 이경호;권오채
    • 대한기계학회:학술대회논문집
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    • 대한기계학회 2007년도 춘계학술대회B
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    • pp.2360-2365
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    • 2007
  • A new microemitter (microcombustor) configuration for a micro thermophotovoltaic system in which thermal energy is directly converted into electrical energy through thermal radiation was investigated experimentally and computationally. The microemitter as a thermal heat source was designed for a few watt power-generating micro thermophotovoltaic system. In order to satisfy the primary requirements for designing the microemitter, i.e., stable burning in the small confinement and maximum heat transfer through the emitting walls but uniform distribution of temperature along the walls, the present microemitter is cylindrical with an annular-type shield for heat recirculation to apply for the excessive enthalpy concept. Results show that the heat recirculation substantially improves the performance of the microemitter: the observed and predicted thermal radiation from the microemitter walls indicated that heat generated in the microemitter is uniformly emitted.

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저온-진공 흑체시스템의 설계 및 성능 평가 (Design and Performance Evaluation of Low-Temperature Vacuum Blackbody System)

  • 김기석;장기수;이상용;김건희;김동익
    • 비파괴검사학회지
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    • 제33권4호
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    • pp.336-341
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    • 2013
  • 본 논문에서는 저온-진공 흑체시스템의 설계 및 구성과 함께 흑체시스템의 수학 모델을 이용한 열해석 평가 방법과 그 결과를 제시하였으며 적외선 카메라를 이용한 흑체시스템의 평가 방안 및 결과를 명시하였다. 개발된 흑체시스템은 기존의 시스템에 비해 상대적으로 규모가 소형이며 273 K이하의 저온에서 수증기가 응결될 수 있는 현상을 방지하기 위하여 흑체시스템 내부를 진공 ($2.67{\times}10^{-2}$ Pa) 상태로 유지되도록 제작되었다. 또한 흑체시스템 내부의 열손실로 인한 성능 저하를 막기 위하여 radiator가 설치되는 부위에는 heat sink, heat shield 및 cold shield를 설계하였다. 흑체시스템의 수학 모델에 대한 열 해석을 위해서 변형된 스테판-볼츠만의 정리를 이용하여 radiator의 성능을 검증하였고 실제 흑체시스템에서 방사되는 적외선 신호에 대해서는 적외선 카메라를 이용하여 신호전달함수 및 온도분해능을 측정, 분석하였다. 제안된 설계와 해석 및 실험 결과에 근거하여, 개발된 저온-진공 흑체시스템은 적용온도범위인 268~333 K 구간에서 적외선 측정장치의 캘리브레이션을 위한 기준장치로서 성능이 안정적이고 적용이 적합한 것으로 확인되었다.

시험용 달 궤도선의 광학탑재체 시스템 열설계에 대한 수치해석적 연구 (Numerical Study on the Thermal Design of Lunar Terrain Imager System Loaded on the Korea Pathfinder Lunar Orbiter)

  • 김택영;장수영;허행팔
    • 한국항공우주학회지
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    • 제47권4호
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    • pp.309-318
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    • 2019
  • 한국형 달 궤도선(Korea Pathfinder Lunar Orbiter, KPLO)에 탑재되는 달 표면지형 광학관측기(Lunar Terrian Imager, LUTI)의 열설계를 수행하고, 열해석을 통하여 열설계의 건전성을 검증하였다. 달 임무궤도의 열환경은 지구궤도와 달리 달 표면의 IR 복사가 중요하므로 이를 열설계에 반영하여야 한다. 위성 외부에 노출되는 부품이나 모듈은 가능한 MLI로 단열시키지만 경통이나 방열판은 기능상 노출되므로 복사형상계수의 개념을 이용한 thermal shield를 전면에 장착함으로써 IR 복사를 완화시킨다. 태양복사를 거의 받지 않는 방열판의 전면부는 IR 방사율이 중요하며, 경통과 같이 열변형에 취약한 부품은 복사히터를 사용하여 온도구배를 최소화시킨다. 열해석 결과분석을 통하여 LUTI의 열설계는 다양한 상황에서 안정적임을 확인하였다.

연료전기용 컴팩트형 개질기의 고성능화를 위한 고온 공기 연소 기술의 적용에 관한 연구 (A Numerical Study on a High-Temperature Air Combustion Burner for a Compact Fuel-Cell Reformer)

  • 이경호;권오채
    • 한국수소및신에너지학회논문집
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    • 제16권3호
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    • pp.229-237
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    • 2005
  • A new burner configuration for a compact fuel-cell reformer with a high-temperature air combustion concept was numerically studied. The burner was designed for a 40 $Nm^3/hr$ hydrogen-generated reformer using natural gas-steam reforming method. In order to satisfy the primary requirements for designing a reformer burner (uniform distribution of temperature along the fuel processor walls and minimum heat losses from the reformer), the features of the present burner configuration included 1) a self-regenerative burner for an exhaust-gas-recirculation to apply for the high-temperature air combustion concept, and 2) an annular-type shield for protecting direct contact of flame with the processor walls. For the injection velocities of the recirculated gas of 0.6-2.4 m/s, the recirculated gas temperature of 1000 K, and the recirculated oxygen mole fraction of 4%, the temperature distributions along the processor walls were found uniform within 100 K variation. Thus, the present burner configuration satisfied the requirement for reducing temperature gradients along the processor walls, and consequently demonstrated that the high-temperature air combustion concept could be applied to the practical fuel reformers for use of fuel cells. The uniformity of temperature distribution is enhanced as the amount of the recirculated gas increases.

Design Considerations of Cryogenic Cooling System for High Field Magnets

  • Choi, Yeon-Suk;Kim, Dong-Lak;Lee, Byoung-Seob;Yang, Hyung-Suk;Yoo Jong-Shin;Painter Thomas A.;Miller John R.
    • 한국초전도ㆍ저온공학회논문지
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    • 제8권4호
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    • pp.30-33
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    • 2006
  • Several crucial issues are discussed in the design of cryogenic cooling system for high field magnets. This study is mainly motivated by our ongoing program to develop a 21 T Fourier Transform Ion Cyclotron Resonance Mass Spectrometer (FT-ICR MS). The magnets of this system will be built horizontally to accomplish the requirement of user friendliness and reliability, and the replenishment of cryogen will not be necessary by a closed-loop cooling concept. The initial cool-down and safety are basically considered in this paper. The effects of the helium II volume and the gap distance of the weight load relief valve (or safety valve) on the cool-down time and temperature rising during an off-normal state are discussed. The total amount of cryogenic cooling loads and the required helium flow rate during cool-down are also estimated by a relevant heat transfer analysis. The temperatures of cryogen-free radiation shield are finally determined from the refrigeration power of a cryocooler and the total cryogenic loads.