• 제목/요약/키워드: Thermal design

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단열재가 극저온 용기의 내부지지대 구조설계에 미치는 영향 (A Study on Thermal Insulator Effect for Structure Design of Internal Support on Cryogenic Vessel)

  • 김두호;지현진;김기열;조성백
    • 한국군사과학기술학회지
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    • 제14권3호
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    • pp.524-531
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    • 2011
  • The cryogenic vessel, storing a liquified solutions as LOX and $LN_2$, consists of a external vessel, internal vessel, thermal insulator and internal support. The internal support should be satisfied with mechanical strength not only to support weight of internal tank but also to maintain uniform space between external and internal tank in spite of external mechanical shock. However, excessive structure design of internal supports is able to increase the amount of heat conduction and the rate of vaporization. The thermal insulator, filled with space between a external and internal vessel, reduces the rate of heat transfer and guarantees the standing time of cryogenic vessel. Especially powder type of insulator has low thermal conductivity and reduce the specification of structure design. In order to evaluate the effect of insulator on structure design, the experiment set-up simulated cryogenic vessel was tested in shock environment according to thermal insulator. As a result, the behavior of internal support under external shock was understood and the design criteria was able to be suggested.

ASCENT THERMAL ANALYSIS OF FAIRING OF SPACE LAUNCH VEHICLE

  • Choi Sang-Ho;Kim Seong-Lyong;Kim Insun
    • 한국우주과학회:학술대회논문집(한국우주과학회보)
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    • 한국우주과학회 2004년도 한국우주과학회보 제13권2호
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    • pp.239-242
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    • 2004
  • The fairing of the launch vehicles has a role of protecting the spacecraft from outer thermal, acoustical, and mechanical loads during flight. Among them, the thermal load is analyzed in the present study. The ascent thermal analyses include aerodynamic heating rate on every point of the fairing, heat transfer through the fairing and spacecraft, and the final temperature during ascent flight phase. A design code based on theoretical/experimental database is applied to calculate the aerodynamic heating rate, and a thermal math program, SINDA/Fluint, is considered for conductive heat transfer of the fairing. The results show that the present design satisfies the allowing temperature of the structure. Another important thermal problem, pyro explosive fairing separation device, is calculated because the pyro system is very sensitive to the temperature. The results also satisfies the pyro thermal condition.

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합성형교량의 설계온도하중 (Design Thermal Loads In Composite Box Girder Bridges)

  • 장승필;임창균
    • 한국강구조학회 논문집
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    • 제10권3호통권36호
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    • pp.537-551
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    • 1998
  • 본 논문에서는 장기온도측정자료의 통계해석에 바탕을 두고, 합성박스형교량에 작용하는 설계온도하중의 적절한 값을 제안하고자 한다. 이를 위해, 최근에 건설된 합성박스형교량에서 약 20개월간 온도측정을 수행하였다. 극치해석에 앞서, 온도분포특성을 나타내는 주요 매개변수를 정의하고, 이의 계절별변화에 대해 상세히 검토하였다. 이 온도하중매개변수의 극치분포를 Tail-Equivalence법에 의해 결정하고, 주어진 재현기간에 해당되는 온도하중매개변수의 극치값을 계산하였다. 끝으로, 이 결과들을 현 시방서에서 온도하중에 대해 제안하고있는 규정들과 비교하였다. 비교결과로부터, 현 시방서는 합성박스형교량의 온도응력을 나타내는데 불충분하며, 특별한 경우에 있어서 현 설계규정에 포함되지않은 수평방향온도변화를 고려해야만 된다는 결론에 도달하였다.

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Thermal Analysis of TRIO-CINEMA Mission

  • Yoo, Jae-Gun;Jin, Ho;Seon, Jong-Ho;Jeong, Yun-Hwang;Glaser, David;Lee, Dong-Hun;Lin, Robert P.
    • Journal of Astronomy and Space Sciences
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    • 제29권1호
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    • pp.23-31
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    • 2012
  • Thermal analysis and control design are prerequisite essential to design the satellite. In the space environment, it makes satellite survive from extreme hot and cold conditions. In recent years CubeSat mission is developed for many kinds of purpose. Triplet Ionospheric Observatory (TRIO)-CubeSat for Ion, Neutral, Electron, MAgnetic fields (CINEMA) is required to weigh less than 3 kg and operate on minimal 3 W power. In this paper we describe the thermal analysis and control design for TRIO-CINEMA mission. For this thermal analysis, we made a thermal model of the CubeSat with finite element method and NX6.0 TMG software is used to simulate this analysis model. Based on this result, passive thermal control method has been applied to thermal design of CINEMA. In order to get the better conduction between solar panel and chassis, we choose aluminum 6061-T6 for the material property of standoff. We can increase the average temperature of top and bottom solar panels from $-70^{\circ}C$ to $-40^{\circ}C $ and decrease the average temperature of the magnetometer from $+93^{\circ}C$ to $-4^{\circ}C$ using black paint on the surface of the chassis, inside of top & bottom solar panels, and magnetometer.

유한요소해석과 최적설계 기법을 활용한 증착용 산화물타겟 접합공정에서의 열 변형 최소화 연구 (Thermal displacement minimization of an oxide target for bonding process by finite element analysis and optimal design)

  • 차한영;정찬엽
    • 한국결정성장학회지
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    • 제30권5호
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    • pp.208-213
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    • 2020
  • 본 연구에서는 유한요소 해석과 PQRSM 알고리즘 기반의 최적설계 기법을 활용하여 IGZO 산화물 타겟과 구리백플레이트가 서로 접합되어 있는 타겟 모듈에서 IGZO 산화물의 열변형을 최소화할 수 있는 방법에 대해 고찰했다. 3차원 유한요소 해석 결과 고온에서 IGZO와 구리 백플레이트의 접합 이후 냉각될 때 IGZO 산화물의 열변형은 최대 0.161 mm로 예측되었다. 유한요소 해석을 연동한 최적설계기법을 적용하기 위해 타겟 모듈을 냉각할 때 사용하는 하부받침대와 상부고정대의 위치를 설계변수화하여 목적함수인 IGZO의 열변형이 최소화되도록 최적설계를 수행했고, 그 결과 IGZO 산화물의 열변형을 최대 42 % 감소시킬 수 있었다. 이는 타겟을 구성하는 주재료와 구조 변경 없이 공정 중에 사용되는 부재료의 위치 변경만으로도 산화물의 열변형을 감소시킬 수 있어 산업계에 유용할 것으로 사료된다.

모터싸이클 디스크 브레이크의 열 및 응력 해석을 통한 형상 설계 (A Study on Shape Design of Motorcycle Disk using Thermal and Stress Analysis)

  • 강석현;박시형;이성수
    • 한국공작기계학회:학술대회논문집
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    • 한국공작기계학회 2001년도 추계학술대회(한국공작기계학회)
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    • pp.363-368
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    • 2001
  • Studies on brake system recently are focused on braking performance, especially the consideration on safety of braking system in an extreme situation and reduction of vibration and noise during braking operation. The thermal crack and Judder from the friction between brake disc and pad can bring the threaten of passengers' safety in the end. Braking force comes from the change of kinetic energy to friction energy. Since heat energy is developed from here, the analysis on thermal stress and thermal strain can be the good data when selecting the material of brake pad and designing heat radiation holes on the disc and it will also be the data when designing the thickness of the disc. This paper is intended to show a creative design method by suggesting the thermal analysis data through FEM study and using shape design parameters.

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Design thermal loading for composite bridges in tropical region

  • Au, F.T.K.;Cheung, S.K.;Tham, L.G.
    • Steel and Composite Structures
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    • 제2권6호
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    • pp.441-460
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    • 2002
  • In the design of bridges, it is important to consider the thermal stresses induced by the non-linear temperature distribution as well as the variation of effective temperature in the bridge deck. To cope with this, design temperature profiles are provided by design codes, which are normally based on extensive research work. This paper presents the results of a comprehensive investigation on the thermal behaviour of bridges in Hong Kong with special emphasis on composite bridges. The temperature distribution in bridges depends primarily on the solar radiation, ambient air temperature and wind speed in the vicinity. Apart from data of the meteorological factors, good estimates of the thermal properties of material and the film coefficients are necessary for the prediction of temperature distribution. The design temperature profiles for various types of composite bridge deck with bituminous surfacing and concrete slab of different thicknesses are proposed. The factors affecting the design effective temperature are also reviewed and suitable values for Hong Kong are proposed. Results are compared with recommendations of the current local code. The method facilitates the development of site-specific temperature profiles for code documents, and it can also be applied to create zoning maps for temperature loading for large countries where there are great climatic differences.

원전 설계기준 사고시 냉각재계통 부분정체로 인한 비대칭 열유동 혼합해석 (Asymmetric Thermal-Mixing Analysis due to Partial Loop Stagnation during Design Basis Accident)

  • 황경모;진태은;김경훈
    • 대한기계학회:학술대회논문집
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    • 대한기계학회 2002년도 학술대회지
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    • pp.51-54
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    • 2002
  • When a cold HPSI (High Pressure Safety Injection) fluid associated with an design basis accident, such as LOCA (Loss of Coolant Accident), enters the cold legs of a stagnated primary coolant loop, thermal stratification phenomena will arise due to incomplete mixing. If the stratified flow enters a reactor pressure vessel downcomer, severe thermal stresses are created in a radiation embrittled vessel wall by local overcooling. Previous thermal-mixing analyses have assumed that the thermal stratification phenomena generated in stagnated loop of a partially stagnated coolant loop are neutralized in the vessel downcomer by strong flow from unstagnated loop. On the basis of these reasons, this paper presents the thermal-mixing analysis results in order to identify the fact that the cold plume generated in the vessel downcomer due to the thermal stratification phenomena of the stagnated loop is affected by the strong flow of the unstagnated loop.

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박판 주조 롤의 최적설계 (Optimal Design of Strip Casting Roll)

  • 박철민;강태욱;박경진
    • 대한기계학회논문집A
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    • 제26권11호
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    • pp.2466-2473
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    • 2002
  • In twin roll strip casting process, the design of casting roll is the most important equipment for producing strip. Analyses of heat transfer and deformation for the casting roll are carried out by using the finite element program, ANSYS. Both the elastic deformation and the elasto-plastic deformation under a thermal load are considered in the analysis. Optimization to minimize the volume of roll is performed under the various thermal loads such as the heat flux and the roll speed. Design variables are defined by diameters and positions of the cooling hole in the roll , Although the thermal load remarkably varies, the design variables and objective function are found to be consistent.

철도차량용 IPMSM의 Water-cooling Jacket 설계 연구 (A Study on the Water-cooling Jacket Design of IPMSM for Railway Vehicles)

  • 박찬배;이준호;이병송
    • 전기학회논문지
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    • 제62권10호
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    • pp.1475-1480
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    • 2013
  • In this paper, the basic design study of a water-cooling jacket, which have reported no cases for applying to railway traction motors so far, were conducted for applying to Interior Permanent Magnet Synchronous Motor (IPMSM) for railway vehicles. The basic thermal characteristics analysis of the 110kW-class IPMSM was performed by using 3-dimentional thermal equivalent network method. The necessary design requirements of the water-cooling jacket were derived by analyzing the results of the basic thermal properties. Next, the thermal characteristics analysis technique was established by using the equivalent model of the solenoid-typed pipe to be installed on the inside of the water-cooling jacket for 110kW-class IPMSM. Finally, a design model of 6kW-class water-cooling jacket was derived through the analysis of various design parameters.