• 제목/요약/키워드: Thermal chamber

검색결과 719건 처리시간 0.026초

A Study on the Operational Status of the Chamber for Testing the Thermal Performance of Curtain Walls

  • No, Sang Tae
    • 국제초고층학회논문집
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    • 제3권2호
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    • pp.147-154
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    • 2014
  • The purposes of this study were to analyze criteria for measurement chamber design dedicated curtain wall, and how to measure of performance configuration and status of the chamber that is currently being used. Main dealing criteria is AAMA 1503-09. Measurement of data is made in curtain wall Mock-up experiment station with thermal imaging camera. Measurement data using thermal imaging cameras at Mock-up curtain was made at the test site. The results of this study were as follows; There is no U-value test method for actual size of curtain wall. The thermal test outdoor chamber showed heat loss in the connection part of indoor and outdoor chamber. And the indoor chamber showed unstable temperature distribution by height.

위성 열평형 시험에서 챔버 벽 영향에 관한 연구 (A Study on Chamber Wall Effect in the Satellite Thermal Balance Test)

  • 김동운;장영근
    • 한국항공우주학회지
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    • 제34권12호
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    • pp.90-95
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    • 2006
  • 위성 열평형 시험에 사용하는 열진공 챔버의 벽은 흑체 거동을 하는 우주공간과는 달리 위성의 복사 에너지를 완벽하게 흡수하지 못하고 일부를 반사한다. 챔버의 크기가 작을수록 이러한 챔버 벽 효과는 커지는 것으로 알려져 있다. 이것은 시험비용을 줄이기 위해 대형 챔버를 사용하기 힘든 소형위성의 개발에 걸림돌이 된다. 본 연구에서는 챔버 벽 효과를 예측하고 이를 보정하기 위한 정량적인 분석을 진행하였다. 그 결과로 챔버 벽 효과에 의한 온도 오차를 계산하여 시험 데이터를 보정할 수 있게 하였다. 또, 최적 면적비를 정의하여 소형위성의 열평형 시험용 열진공 챔버의 크기를 정하는데 기준을 마련하였다. 덧붙여 챔버 벽을 투명한 재질로 코팅하여 챔버 벽 효과를 줄일 수 있는 방안에 대해 이론적인 분석을 수행하였다.

열환경챔버의 냉방 시뮬레이션 프로그램 개발에 관한 연구 (A Study on the Development of Cooling Simulation Program for Thermal Environmental Chamber)

  • 이한홍
    • 한국생산제조학회지
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    • 제8권5호
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    • pp.108-114
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    • 1999
  • The thermal environmental chamber has been using in maintaining weather condition keeping thermal capacity under heating and cooling load fluctuation and for the performance testing of cooling system or air-conditioner on artificial envi-ronment. In ordder to make the various environmental conditions in the thermal environmental chamber the proper cooling system is necessary to eliminate the heating load produced inside the chamber and to maintain the designed environmental condition. For this reason the optimal design of cooling system and the prediction of performance is also required. This paper describes the prediction of performance of cooling system in the thermal environmental chamber with the capacity of 37,000kcal/hr which is developed for the test of performance in heating mode of heat pump system, In the results this paper is trying to develop simulation program on the base of mathematical models and which can be applied effectively to the optimal design of cooling system and prediction of performance to the inside and outside change of envi-ronmetal load.

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재생냉각형 가스발생기 챔버 구조해석 (Structural Analysis of Gas Generator Regenerative Cooling Chamber)

  • 류철성;김홍집;최환석
    • 대한기계학회논문집A
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    • 제31권10호
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    • pp.1046-1052
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    • 2007
  • Elastic-plastic structural analysis for regenerative cooling chamber of gas generator was performed. Uniaxial tension test was conducted for STS316L at room and high temperature conditions to get the material data necessary for the structural analysis of the chamber which was operated under thermal load and high internal pressure. Physical properties including thermal conductivity, specific heat and thermal expansion were also measured. The structural analysis for four different types of regenerative cooling chamber of gas generator revealed that increased cooling performance decreased the thermal load and strain of the cooling channel structure. The results propose that in order for the regenerative cooling gas generator chamber to have high structural stability with endurance to high mechanical and thermal loads, it is important for the chamber to be designed to have high cooling performance.

가스발생기 재생냉각 챔버 구조해석 (Structural Analysis of Gas Generator Regenerative Cooling Chamber)

  • 류철성;최환석
    • 대한기계학회:학술대회논문집
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    • 대한기계학회 2007년도 춘계학술대회A
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    • pp.802-807
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    • 2007
  • Elastic-plastic structural analysis for regenerative cooling chamber of gas generator was performed. Uniaxial tension test was also conducted for STS316L at room and high temperature conditions to get the material data necessary for the structural analysis of the chamber which is operated under thermal load and high internal pressure. Physical properties including thermal conductivity, specific heat and thermal expansion data were also measured. The structural analysis for four different types of regenerative cooling chamber of gas generator revealed that increased cooling performance decreases the thermal load and strain of the cooling channel. The results propose that in order for the regenerative cooling gas generator chamber to have high structural stability with endurance to high mechanical and thermal loads, it is important for the chamber to be designed to have high cooling performance.

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정지궤도 위성의 열평형 시험 모델링 및 예비 예측 (THERMAL BALANCE MODELLING AND PREDICTION FOR A GEOSTATIONARY SATELLITE)

  • 전형열;김정훈
    • 한국전산유체공학회:학술대회논문집
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    • 한국전산유체공학회 2009년 춘계학술대회논문집
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    • pp.142-147
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    • 2009
  • COMS (Communication, Ocean and Meteorological Satellite) is a geostationary satellite and has been developing by KARI for communication, ocean and meteorological observations. It will be tested under vacuum condition and very low temperature in order to verify thermal design of COMS. The test will be performed by using KARI large thermal vacuum chamber, which was developed by KARI, and the COMS will be the first flight satellite tested in this chamber. The purposes of thermal balance test are to correlate analytical model used for design evaluation and predicting temperatures, and to verify and adjust thermal control concept. KARI has plan to use heating plates to simulate space hot condition especially for radiator panels such as north and south panels. They will be controlled from 90K to 273K by circulating GN2 and LN2 alternatively according to the test phases, while the shroud of the vacuum chamber will be under constant temperature, 90K, during all thermal balance test. This paper presents thermal modelling including test chamber, heating plates and the satellite without solar array wing and Ka-band reflectors and discusses temperature prediction during thermal balance test.

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열피로시험중 질화규소 와류실에 발생하는 응력해석 (Stress Analysis of $Si_3N_4$ Swirl Chamber during Thermal Fatigue Test)

  • 김창삼;정덕수
    • 한국세라믹학회지
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    • 제33권3호
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    • pp.321-326
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    • 1996
  • Thermal fatigue test and stress analysis of Si3N4 and metal swirl chamber were carried out to investigate the reliability of the swirl chambers. Conditions of the thermal fatigue test were severer than those in real engine and FEM was used to analize the stress distribution in the swirl chambers. Fatigue cracks of the maximum length 2.4 mm and deformation were occurred at the corner of the jet in metal swirl chamber but not observed in Si3N4 swirl chamber. Maximum tensile stress in Si3N4 swirl chamber calculated by FEM was 300 MPa.

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Thermal Dissipation Performance of a Heat Sink/Vapor Chamber Prepared by Metal Injection Molding Process

  • Chena, Bor-Yuan;Hwang, Kuen-Shyang
    • 한국분말야금학회:학술대회논문집
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    • 한국분말야금학회 2006년도 Extended Abstracts of 2006 POWDER METALLURGY World Congress Part2
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    • pp.767-768
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    • 2006
  • In this study, copper vapor chambers with built-in cooling fins, which eliminated the soldered or brazed joints in the conventional vapor chamber, were fabricated using the metal injection molding process. The results show that with optimized molding parameters, fins with an aspect ratio up to 18 could be produced. After sintering, the densities of the fin and chamber reached 96%. With only 32 cooling fins and a small fan installed, the thermal resistance of the heat sink was $1.156^{\circ}C/W$, and the power dissipation was 40W when the junction temperature was $70^{\circ}C$. When copper powder was sintered onto the chamber to make a vapor chamber, the thermal resistance decreased to $1.046^{\circ}C/W$.

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실시간 플랜트 시뮬레이터를 이용한 우주 열환경 챔버 제어기 개발에 관한 연구 (Study on the application of a realtime simulator to the development of a controller for a space thermal environment chamber)

  • 정무진;신영기;최석원;문귀원;서희준;이상훈;조혁진
    • 대한기계학회:학술대회논문집
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    • 대한기계학회 2003년도 추계학술대회
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    • pp.216-221
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    • 2003
  • A thermal vacuum chamber is mainly used to simulate thermal environments of a test satellite in satellite orbits in which daily temperature variations range from 80K to above 400K depending on solar radiation under the vacuum below $10^{-4}$ torr. The test facility is quite complex and consists of expensive parts. So any modification of control software is discouraged in fear of unexpected system failure. The purpose of this study is to develop a realtime dynamics model of the thermal vacuum chamber in view of controller design and simulate its electrical inputs and outputs for interface with a PLC (programmable logic controller). A PLC program that was used in the thermal vacuum chamber is applied to the realtime simulator. The realized simulator dynamics is found to be quite similar to that of the thermal vacuum chamber and serve to an appropriate plant to verify the control performance of a programmed PLC.

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열환경 챔버 제어를 위한 PID 튜닝기법 연구 (A Study on PID Tuning Technique of a Thermal Environment Chamber)

  • 신영기;양훈철;태춘섭;장철용;조수;김영일
    • 설비공학논문집
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    • 제17권11호
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    • pp.1072-1078
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    • 2005
  • The present study has been conducted to tune a PID controller for large thermal systems such as a thermal environment chamber. In spite of large thermal mass of the thermal chamber under test, its response delay time was found to be negligible mainly due to high air recirculation rate. In general, heating and cooling capacities tend to be small compared the size of a thermal environment chamber, which leads to long transient periods of one hour or so. In the study, a PI tuning method is suggested which makes system responses faster while reducing overshoots and hunting by utilizing efficiently proportional band of actuators.