• 한국신재생에너지학회:학술대회논문집
• /
• 한국신재생에너지학회 2006년도 춘계학술대회
• /
• pp.576-579
• /
• 2006

This paper describes characteristics and procedure of the basic design of large scale solar thermal power plant system. The evaluation is based on the operating data of CESA-I, solar central receiver plant. In order to evaluate the solar irradiation on the receiver, it is necessary to calculate the amount of thermal energy consumption at steam turbine and storage system in the STPPS. Especially, it is need to take into account of the storage and operating time to design a plant efficiently. In addition, basic design is performed for the CESA-I using the software tool of THERMOFLEX program. Based on the results, It is at lowed to use the program to investigate detail performance of each units of the STPPS by varying the operating conditions.

• Smart Structures and Systems
• /
• 제15권2호
• /
• pp.469-488
• /
• 2015

Thermal loads, especially thermal gradients, have a considerable effect on the behaviors of large-scale bridges throughout their lifecycles. Bridge design specifications provide minimal guidance regarding thermal gradients for simple bridge girders and do not consider transversal thermal gradients in wide girder cross-sections. This paper investigates the three-dimensional thermal gradients of arch bridge girders by integrating long-term field monitoring data recorded by a structural health monitoring system, with emphasis on the vertical and transversal thermal gradients of wide concrete-steel composite girders. Based on field monitoring data for one year, the time-dependent characteristics of temperature and three-dimensional thermal gradients in girder cross-sections are explored. A statistical analysis of thermal gradients is conducted, and the probability density functions of transversal and vertical thermal gradients are estimated. The extreme thermal gradients are predicted with a specific return period by employing an extreme value analysis, and the profiles of the vertical thermal gradient are established for bridge design. The transversal and vertical thermal gradients are developed to help engineers understand the thermal behaviors of concrete-steel composite girders during their service periods.

• 한국항공우주학회지
• /
• 제48권6호
• /
• pp.455-466
• /
• 2020

본 연구에서는 다수의 우주 환경 관측용 탑재체를 장착한 6U급 초소형위성에 대한 열모델을 구축하여 이를 기반으로 수행된 열설계에 대해 기술하였으며, 궤도 열해석을 통해 적용된 열설계의 유효성을 입증하였다. 초소형위성의 특성을 고려하여 표면 처리 및 절연체, 열전도체 등의 수동 열제어 기법 위주로 열설계를 진행하였지만, 배터리 및 추력기 등과 같이 작동 온도의 범위가 좁고 궤도 열환경에 직접적으로 노출되는 부품들에 대해서는 능동 열제어 기법 중 하나인 히터를 적용하였다. 궤도 열해석 조건은 기본적으로 위성의 궤도 조건을 바탕으로 하며, 임무 시나리오에 따른 발열량 및 위성의 자세에 따라 임무 모드, 초기 운용 모드, 비상운용 모드, 편대 비행 모드로 분류하여 궤도 열해석을 수행하였다. 각 모드 별 해석 결과를 통해 모든 부품들이 작동 온도 조건을 만족하는 것을 확인하였고, 비상운용 모드의 해석 결과를 통해 배터리 및 추력기의 히터 용량과 작동 주기를 산출하였다.

• 대한기계학회:학술대회논문집
• /
• 대한기계학회 2005년도 창립60주년 기념 추계 학술대회
• /
• pp.12.2-12.2
• /
• 2005

• 한국전산유체공학회:학술대회논문집
• /
• 한국전산유체공학회 2006년도 PARALLEL CFD 2006
• /
• pp.389-390
• /
• 2006

• 한국항공우주학회지
• /
• 제43권2호
• /
• pp.179-185
• /
• 2015

우주용 고해상도 전자광학카메라의 개발에 있어 초점면 배열 장치(Focal Plane Assembly, FPA)의 열제어 설계는 영상품질을 결정하는 중요한 요소이다. FPA 열제어 설계의 목표는 영상 촬영 기간 중 안정적인 열 환경을 제공하는 것으로, 촬영 기간 동안 운용 온도를 주어진 범위 내로 유지해야 하며 후속 촬영에 문제가 없도록 빠른 시간 내에 온도 초기화를 완료해야 한다. 상기의 두 항목인 온도 유지와 온도 초기화 중에서 FPA 구조 설계에 따른 영향을 가장 많이 받으며, 설계 변경의 자유도가 상대적으로 낮은 온도 유지 항목에 대하여 FPA 구조설계 초기 단계부터 검토 및 반영이 가능한 단순화 된 열 저항 해석 기반의 온도 예측 방안을 정의하였다. 또한 열해석 결과와의 비교를 통해 온도 예측 방안을 검증, FPA 설계를 위한 trade-off에 효과적으로 사용할 수 있음을 확인하였다.

• 한국산업융합학회 논문집
• /
• 제2권2호
• /
• pp.11-21
• /
• 1999

This objective of this paper is to investigate the evaluation and indiction of human thermal comfort in building environment. The issue of defining the boundaries of acceptable thermal comfort conditions in buildings and urban may have significant implication for building design and also may have urban design by climate considerations. And then it is to apply the thermal comfort condition to environmental design by using passive methods in Korea. Since 1920. architects have conducted studies to measure thermal comfort in houses under hot and humid conditions, while industrial hygienists have studied the effects of temperature and humidity on the performance of factory workers. Thermal comfort can be influenced by many variables. This paper conducted to review the previous researches and the human heat balance equation, and to analyse in order to reveal the meaning and usage of the thermal comfort index in two traditional essays, Fanger's PMV and Gagge's ET* Their comfort indexes compared with each other. They were based on human heat balance equation and psychological and physiological responses in the laboratory tests. The researchers and the architectural engineers using thermal comfort index shall be careful in decided the use of indexes and be necessary to recognize the value concept of the design criteria for thermal comfort. Therefore, The opinion of the authors is that different comfort standards have to apply for each building and urban with different climatic conditions.

• 한국초전도ㆍ저온공학회논문지
• /
• 제19권2호
• /
• pp.53-57
• /
• 2017

In superconducting power devices including power cables in which high temperature superconducting (HTS) tapes are utilized, a reliable electrical insulation should be achieved for its maximum performance. For an efficient design of HTS superconducting devices, a comparative evaluation of the mechanical and thermal propperties for various insulation materials at cryogenic temperatures is required. Especially, in the process of the property evaluation of the sheet-shaped insulation materials, anisotropy according to the machining direction should be considered because the mechanical and thermal properties are significantly influenced by the sample orientation. In this study, the cryogenic thermal and mechanical properties of various insulation material sheets such as PPLP, Cryoflex, Teflon, and Kapton were determined considering sample orientation. All samples tested at cryogenic temperature showed significantly higher tensile strength as compared with that of room temperature. The ultimate tensile strength at both temperature conditions significantly depended upon the sample orientation. The thermal properties of the insulation materials exhibited a slight difference among samples depending on the orientation: for the PPLP and Cryoflex, the CD orientation showed larger thermal contraction up to 77 K as compared to the MD one. MD samples in PPLP and Cryoflex showed a lower CTE and thermal contraction which made it more promising as an insulation material due to its comparable CTE with HTS CC tapes.

• 한국전산유체공학회:학술대회논문집
• /
• 한국전산유체공학회 2010년 춘계학술대회논문집
• /
• pp.416-421
• /
• 2010

The north and south panel of a geostationary satellite are used for radiator panels to reject internal heat dissipation of electronics units and utilize several heat pipe networks to control the temperatures of units and the satellite within proper ranges. The design of these panels is very important and essential at the conceptual design and preliminary design stage so several thousands of nodes of more are utilized in order to perform thermal analysis of panel. Generating a large number of nodes(meshes) of the panel takes time and is tedious work because the mesh can be easily changed and updated by locations of units and heat pipes. Also the detailed panel model can not be integrated into spacecraft thermal model due to its node size and limitation of commercial satellite thermal analysis program. Thus development of a program was required in order to generate detailed panel model, to perform thermal analysis and to make a reduced panel model for the integration to the satellite thermal model. This paper describes the development and the verification of panel thermal analysis program with ist main modules and its main functions.

• 한국전산유체공학회지
• /
• 제15권3호
• /
• pp.66-72
• /
• 2010

The north and south panel of a geostationary satellite are used for radiator panels to reject internal heat and utilize several heat pipe networks to control the temperatures of units and the main structures of satellite within proper ranges. The design of these panels is very important and essential at the conceptual design and preliminary satellite design stage, so several thousands of nodes or more are utilized in order to perform detailed thermal analysis of panel. Generating a large number of panel nodes takes time and is tedious work because the nodes can be easily changed and updated by locations of units and heat pipes. Also the detailed panel model can not be integrated into spacecraft thermal model due to its node size and limitation of commercial satellite thermal analysis program. Thus development of a program was required to generate a detailed panel model, to perform thermal analysis and to make a reduced panel model for the integration to the satellite thermal model. This paper describes the development and the verification of the panel thermal analysis program with its main modules and functions.