• Title/Summary/Keyword: 단열 두께

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A Study on the Insulation Design Parameters of the Reactor in the Korean Standard Nuclear Power Plant (한국표준원전 원자로용기의 단열 설계에 관한 연구)

  • 김석범;백세진;임덕재;최해윤;이상섭;박종호
    • Journal of Energy Engineering
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    • v.8 no.2
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    • pp.285-292
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    • 1999
  • The design parameter of the reactor vessel insulation for the Korea Standard Power Plant has been studied numerically. The heat loss from the reactor vessel through the insulation is analysed by using the computational fluid dynamics code, FLUENT. Parametric study has been performed on the air gap width between the reactor vessel wall and the inner surface of the insulation, and on the insulation thickness. Also evaluated is the performance degradation due to the chimney effect caused by gaps between the panels during the installation of the insulation system. From the analysis results, the optimal air gap width and the optimal insulation thickness are obtained.

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A Study on the Insulation Performance of Composite Multilayer Insulation by Applciation of Heat Storage Tank (축열조용 복합 다층 단열재의 단열 성능 연구)

  • Choi, Gyuhong;Hwang, Seung Sik;Shin, Donghoon;Park, Woo Sung;Park, Dae Woong;Son, Seung Kil;Chung, Tae Yong
    • Journal of Energy Engineering
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    • v.23 no.3
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    • pp.82-87
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    • 2014
  • MLI(Multi-layer Insulation) is widely used to get highly insulating on cryogenic system in order to reduce heat loads. MLI for satellites thermal performance is changed by materials and laminated method. In this study, a composite multilayer insulation by application of heat stroage tank performance were compared with materials and laminated to change the way. Experimental methods of the KS C 9805 was used, the composite multilayer insulation and EPS was compared with the insulation performance. A method for analysis of experimental results is the equivalent thickness about CMI and the insulation performance were used to compare thermal conductance. As a results, the equivalnet thickenss and the thermal conductance of the composite multilayer insulation were smaller than the EPS and the thermal performance are more excellent. In addition, the configuration of the composite multilayer insulation materials and laminated method varies depending on the overall heat transfer coefficient was confirmed.

한국표준원전 원자로의 단열 설계에 관한 연구

  • 백세진;김석범;주경인;김영보;정종식
    • 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.

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Optimized Insulation Thickness of the Refrigerated Warehouse with Different Envelope Structures and Insulation Materials by L.C.C. Analysis (생애비용 분석을 통한 외벽 및 단열재료 종류별 냉동냉장창고 외피의 적정 단열두께 산정)

  • 강승희;구보경;황혜주;석호태;안홍섭;송승영
    • Korean Journal of Air-Conditioning and Refrigeration Engineering
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    • v.15 no.5
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    • pp.372-381
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    • 2003
  • This study aims to find out the optimized insulation thickness of refrigerated warehouse with different envelope structures (RC and PC wall) and insulation materials (urethane and icynene). Each of them is compared according to the thickness of insulation (100, 150, 200 mm/50 or 250 mm) and the temperature of cold storage room (0, -6, -15$^{\circ}C$). As results, it is proved to have the best economical efficiency in life cycle cost when PC wall with thickness of 100 mm (0 and -6$^{\circ}C$) and 150 m (-15$^{\circ}C$) urethane, respectively, are applied.

Study on the characteristics of perlite insulation for the storage tank in LNG carrier (LNG선박 화물창의 펄라이트 단열재 적용성에 관한 설계 특성 연구)

  • Yun, Sangkook
    • Journal of Advanced Marine Engineering and Technology
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    • v.37 no.8
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    • pp.843-848
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    • 2013
  • As the LNG demands are growing, the constructions of LNG FPSO (Floating Production Storage and Off-loading) and LNG carriers have been constantly increased, and the various design of storage tank has been tried. This paper propose that the material of inner storage tanks is made of 5~9% Ni steel plate and perlite powder insulation instead of urethane foam block. It needs essentially to obtain the proper design specifications that are the pressure of perlite, the characteristics of resilient blanket as the pressure absorber, optimum thickness of blanket and design pressure of tank wall, etc. to enable the perlite insulation system to LNG carrier, The results show that the design thickness of blanket should be between 1/4 to 1/3 of insulation width and the optimum rate becomes 30%, and the design pressure be applied below 1,500 Pa with blanket thickness.

A Study on the Heat Transfer Characteristics of Surface Radiation-Natural Convection Interactions in an Enclosure for Various Adiabatic Wall Thicknesses (단열벽체두께가 변화되는 밀폐공간에서 복사-자연대류열전달특성에 관한 연구)

  • Kwon, Y.I.;Yoo, J.O.;Kwon, S.S.
    • Solar Energy
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    • v.15 no.3
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    • pp.39-52
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    • 1995
  • This study is investigated numerically on the heat transfer characteristics of surface radiation-natural convection interactions in a two dimensional enclosure assumed Ondol cavity. Mean Nusselt number of the bottom surface with surface radiation is increased by increasing wall emissivity and by decreasing dimensionless thickness of adiabatic wall. and is greater than that without radiation. Mean Nusselt number of the bottom surface for convection only with surface radiation is slightly smaller than that without surface radiation with decrease dimensionless thickness of adiabatic wall.

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The Compressive Strength of Thin-Walled Cold-Formed Steel Studs with Slits in the Web (복부에 슬릿이 있는 박판냉간성형형강 스터드의 압축강도)

  • Kwon, Young-Bong;Soe, Eung-Kyu;Lim, Duk-Man;Kim, Gap-Deuk;Kwon, In-Kyu
    • Journal of Korean Society of Steel Construction
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    • v.24 no.2
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    • pp.189-197
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    • 2012
  • The cold-formed steel stud, which has been used as a load-bearing member of wall panels for steel houses, poses a significant problem in insulation due to heat bridging of the web. Therefore, some additional thermal insulating materials are required. In order to solve this problem, the cold-formed steel thermal stud with slits in the web was developed. However, estimating the structural strength of thermal studs is very difficult because of the arrangement of perforations. In this paper, an analytical and experimental research on thermal studs is described. Three types of studs with different length, pitch and arrangement of slits were tested to failure. A simple design approach was proposed based on the test results. The proposed method adopted the direct strength method, based on the elastic local and distortional buckling stress of plain studs with equivalent thickness in the web instead of thermal studs. The predictions using the proposed method were compared with test results for verification and the adequacy of the proposed method was confirmed.

Transient Heat Transfer Analysis of Small Launch Vehicle Common Bulkhead Propellant Tank with Different Insulation Thickness (소형발사체 공통격벽 추진제 탱크의 단열재 두께 변화에 따른 과도 열전달 해석)

  • Ji-Yoon Yang;Gyeong-Han Lee;Sang-Woo Kim;Soo-Yong Lee
    • Journal of Aerospace System Engineering
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    • v.18 no.3
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    • pp.70-75
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    • 2024
  • The insulation performance of a common bulkhead propellant tank for small launch vehicles with variations in insulation thickness was analyzed. The common bulkhead propellant tank composed of a single part allows for lightweight design, as it eliminates the need for tank connections. However, problems such as propellant loss and ignition delay due to heat transfer caused by temperature differences between oxidizer and fuel may arise. Therefore, it is essential to verify the insulation performance of the common bulkhead structure that separates the oxidizer tank and fuel tank. In this study, transient heat transfer analysis was conducted for propellant tanks with insulation thicknesses of (50, 55, 60, 65, and 70) mm to analyze the insulation performance using boil-off mass. Subsequently, the boil-off mass of the oxidizer generated during the first-stage flight time of the propellant tank was determined. The results confirmed that increasing the insulation thickness reduces the boil-off mass, thereby improving the insulation performance.

Tibial Tuberosity Advancement for Partial Rupture of Cranial Cruciate Ligament in Two Dogs (경골조면 전이동술을 이용한 개에서의 부분 전십자인대 단열치료 2례)

  • Heo, Su-Young;Lee, Hae-Beom
    • Journal of Veterinary Clinics
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    • v.31 no.2
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    • pp.141-144
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    • 2014
  • Two dogs (Case 1 weighing 27 kg, Case 2 weighing 42 kg) were referred with hindlimb lameness. On physical examination, there was moderate pain on stifle joint testing and mild cranial translation on cranial drawer testing in Case 1. This translation was obvious when the patient was under general anesthesia. Case 2 showed discomfort during hyperextension of the stifle joint, but no significant cranial translation under general anesthesia. Joint effusion was detected on radiography in both cases. Based on physiologic and radiographic examinations, cranial cruciate deficiency was suspected, so exploratory arthroscopy was performed. Arthroscopy revealed partial rupture of the cranial cruciate ligament (CrCL) in both cases. Case 1 showed unstable partial CrCL rupture, while Case 2 had stable CrCL rupture. Tibial tuberosity advancement (TTA) was carried out as planned. Seroma occurred one week postoperatively in Case 2, and was removed surgically. The patients returned to satisfactory weight-bearing ambulation 5 months after initial surgery. Based on the results of these cases, TTA appears to be a useful procedure in the treatment of CrCL partial rupture.

Research on the Architectural Applications of High-Performance Vacuum Insulation Panel (고성능 진공단열재의 건축적인 적용에 관한 연구)

  • Kwon, Young Cheol;Kim, Suk
    • Land and Housing Review
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    • v.10 no.3
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    • pp.23-32
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    • 2019
  • Vacuum Insulation Panel(VIP) has the lowest thermal conductivity among present insulations. It is composed of envelope, core material and getter. Aluminum film is usually used as the envelope of VIP, and it is important component to decide the useful life of VIP. In this research, the thermophysical properties of incombustible fiber glass core VIP were investigated with the possibility of its architectural applications. The results of this research can be summarized as follows: 1) The thermal conductivity of 20mm-thick fiber glass core VIP is resulted as 0.00177W/m·K, which means that 20mm-thick VIP can meet all the reinforced insulation guideline and it can be used in any envelope of any region in Korea. 2) As a result of the test of incombustion and gas toxicity, fiber glass core VIP was suitable for incombustible material. 3) As the test result for the long term thermal conductivity, fiber glass core VIP was found out that it would keep above 10 times insulating performance than polystyrene foam and glass fiber. 4) To meet the thermal transmittance of 0.12W/㎡K, limited-combustible insulation of expanded polystyrene foam and phenolic foam should be used respectively as thick as above 280mm and 170mm, incombustible VIP can meet the same insulation level with 20mm thickness. 5) The price competitiveness of incombustible VIP to meet the thermal transmittance of 0.12W/㎡·K was about 1,500won/㎡ higher than that of phenolic foam.