• Proceedings of the Korean Vacuum Society Conference
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• 2013.08a
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• pp.308.1-308.1
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• 2013

여름철 건축물의 냉방 부하 저감 및 자동차 실내의 온도 상승을 억제하기 위하여 일반적으로 단열필름이 사용되고 있다. 실제 시중에 유통되고 있는 단열필름은 크게 유기물 기반의 제품과 무기물 기반 제품으로 나뉘고 있다. 본 연구에서는 유기물 기판의 단열 필름은 내구성이 거의 없기 때문에 무기물 기반의 제품을 위주로 연구를 진행하였다. 단열 필름의 단열 효과가 어느 정도인지를 정확히 알기 위하여 UV-Vis 스펙트럼 분석을 실시하였다. 항온 항습 장치를 이용하여 고온고습 조건에서 무기물 기반의 단열 필름의 성능 변화를 통하여 내구성 실험을 실시하였다.

• Resources Recycling
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• v.28 no.6
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• pp.64-72
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• 2019

Fly ash has different chemical composition depending on the type and quality of flaming coal. Fly ash is classified according to carbon content and particle size. Waste glass powder is manufactured by crushing glass. Exterior Insulation Finish System (EIFS) is generally applied by using poly-styrene foam which is economical and has excellent thermal insulation performance. However, poly-styrene foam has excellent insulation performance, but it is vulnerable to fire, which is becoming a serious problem. In this study, using a fly ash and waste glass powder to produce a finishing mortar at high temperatures. Also, High temperature strength and flame retardant properties were tested according to the cover thickness. From the test result, finishing mortar prepared using fly ash and waste glass powder is due to the improved heat resistance by alkali-activated bonding. However, since the strength decreases at high temperatures, it is necessary to select an appropriate mixing proportion.

• Proceedings of the Korean Nuclear Society Conference
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• 1996.05b
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• pp.317-322
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• 1996

고온으로 유지되는 원자로에는 열손실을 줄이기 위하여 단열재가 설치되어 있다. 일반직으로 열손실 시험에서 나타난 실제 열손실은 설계상의 열손실보다 크며, 이의 원인은 단열설계의 부적절, 단열재 설치상의 미흡 등에 기인한다. 본 연구에서는 단열재 두께와 간격에 대한 열전달 특성을 분석하여 단열설계변수를 최적화하며, chimney effect에 의한 열손실 증가를 정량적으로 분석하였다. 본 연구의 결과는 원자로용기 뿐아니라 가압기, 증기발생기 등의 큰 규모의 단열재 설계에 적용될 수 있다.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2010.05a
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• pp.165-169
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• 2010

Liquid Rocket Engine is generally composed of extremely low and high temperature field. So that the component works properly including the electric component, the heat insulator should be applied appropriately. There are three steps. First, the heat source components should be defined and temperature field analyzed. Second, the heat transfer of pipes between the heat sources should be analyzed. Third, the components and pipes before and after applying the heat insulator should be analyzed. Finally, the optimized heat insulator depth can be calculated. In this paper, the procedure of this steps is established and investigated.

• KOREAN POULTRY JOURNAL
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• v.46 no.4
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• pp.112-115
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• 2014

국내 계사를 살펴보면 우레탄 또는 스티로폼을 거의 사용하고 있다. 오랜 시간이 지나면서 계사의 부식과 쥐의 영향으로 단열재 내부가 파괴되고 있는 상황이다. 하지만 최근 설립된 위드팜이 뿌리는 단열재를 출시하면서 계사의 신축 및 리모델링시 저비용으로 고효율을 기대할 수 있게 됐다. 질석과 펄라이트로 만든 뿌리는 단열재는 불연기능으로 화재예방, 단열기능으로 여름철 고온스트레스 예방, 쥐의 단열재 파괴 예방이 가능해 계사 환경 개선에 큰 도움을 주고 생산성에도 영향을 끼친다. 이번호에는 당당하게 축산업에 뛰어든 신입 축산업체인 위드팜(대표 김재국)을 소개코자 한다.

• KOREAN POULTRY JOURNAL
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• v.17 no.7 s.189
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• pp.104-109
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• 1985

고온이 닭의 생산성에 미치는 영향은 매우 크다. 따라서 여름철에는 환기를 충분히 시키고 단열재를 사용하거나 물을 뿌려 복사열을 막고 계사내에 직사광선이 비치지 못하게 해야 한다.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2017.05a
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• pp.1057-1059
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• 2017

In development of liquid-propellant rocket engine, engine gimbaling requires various types of bellows movements and cryogenic insulation is applied with movement-based design and material on each axial and circular bellows. Cryogenic insulation of Bellows for high pressure line and recirculation line are necessary to maintain cryogenic temperature for engien efficiency and protect from heat transfer and radiation of high temperature components during engine gimbaling.

• Transactions of the KSME C: Technology and Education
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• v.2 no.1
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• pp.65-72
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• 2014

The purpose of this study is to design a heat insulator for reducing available energy loss in stratified thermal storage tank. Heat insulator is operated by buoyancy effect from density difference between hot and cold water without extra equipment. Analysis model using the Matlab Simulink was developed to estimate the internal temperature distribution in thermal storage tank and also used to select proper material and thickness of the heat insulator. Operational feasibility was confirmed through reduced scale experiment. As a result, heat insulator can effectively delay the formation of thermal boundary layer between hot and cold water. In reduced scale experiment, heat insulator can preserve additional 1540J of available energy. When applied to the real thermal storage tank, increase of 6% thermal storage efficiency can be expected.

• Journal of Hydrogen and New Energy
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• v.30 no.6
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• pp.540-548
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• 2019

This study was conducted to develop insulation for solid oxide fuel cell (SOFC). The developed insulation is based on the lamination technology and the radiation shielding technology of the satellite insulation. The insulation material is consisting of insulation material for conduction resistance, spacer, and radiation shielding material. The experimental apparatus consisting vacuum bell jar, pump, heater and temperature recording device has developed to verify the performance of the insulation. The experimental values were used as reference data for the modeling development. In this paper, heat transfer is assumed to be one- dimensional phenomena for the prediction of insulation performance and internal temperature distribution in high temperature region of SOFC. The developed model was used to compare the performance difference of insulation types according to composition materials. The analysis result shows that the insulation including spacer and radiation shielding has better heat insulation performance than other cases. In this study, the thickness reduction effect of about 20% was shown compared to the insulation including only conductive material. It is noted that the radiant shielding material should be carefully selected for durability, because SOFC insulation should be used for a long time at high temperature.

• Composites Research
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• v.33 no.3
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• pp.101-107
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• 2020

This study investigates the characterization on the thermal insulation properties of silicon carbide coating on the C_f-C composites. The silicon carbide coatings by chemical vapor deposition on the C/C composites are prepared to evaluate thermal resistance. Firstly, we perform the basic insulation test by thermal shock at 1350℃ in air on the C/C composite and SiC-coated C/C composite. We also performed the burner tests on the surface of the composites at high temperatures such as 1700 and 2000℃, and the weight change after burner tests are measured. The damages on the surface of C/C composite and SiC-coated composite are observed. As a result, the SiC coating is beneficial to protect the C/C composite from high temperature even though damages such as defoliation, crack and voids are observed during burner test at 2000℃.