• 제목/요약/키워드: Thermal Design and Analysis

검색결과 2,066건 처리시간 0.037초

액체금속 표적 시스템의 열적, 구조적 건전성 평가 및 설계 (Thermal-Hydraulic, Structural Analysis and Design of Liquid Metal Target System)

  • 이용석;정창현
    • 에너지공학
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    • 제10권3호
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    • pp.294-298
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    • 2001
  • 사용 후 핵연료의 고독성 장수명 핵종을 저독성 단수명 핵종으로 변환시키기 위한 미임계 핵변환로 연구가 진행중이다. 본 논문에서는 이러한 미임계 핵변환로에서 사용될 표적 시스템을 설계하기 위하여 표적시스템에 대한 열적, 구조적 분석을 수행하였다. 표적시스템의 열수력 분석에서는 diffuse plate를 삽입함으로써 빔창의 냉각효과를 증대시킬 수 있었다. 또한, 주요 인자인 빔창두께, 빔출력, 냉각재 유량 변화에 따른 빔창의 열적, 구조적 건전성 분석을 수행하여 표적시스템의 설계치를 설정하였다. 본 설계조건 하에서 빔창의 최대 온도 및 음력은 허용가능한 범위에 있음을 확인하였다.

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Thermal Model of High-Speed Spindle Units

  • Zver, Igor-Alexeevich;Eun, In-Ung;Chung, Won-Jee;Lee, Choon-Man
    • Journal of Mechanical Science and Technology
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    • 제17권5호
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    • pp.668-678
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    • 2003
  • For the purpose to facilitate development of high-speed spindle units (SUs) running on rolling bearings, we have developed a beam element model, algorithms, and software for computer analysis of thermal characteristics of SUs. The thermal model incorporates a model of heat generation in rolling bearings, a model of heat transfer from bearings, and models for estimation of temperature and temperature deformations of SU elements. We have carried out experimental test and made quantitative evaluation of the effect of operation conditions on friction and thermal characteristics of the SUs of grinding and turning machines of typical structures. It is found out that the operation conditions make stronger effect on SU temperatures when rpm increases. A comparison between the results of analysis and experiment proves their good mutual correspondence and allows us to recommend application of the models and software developed for design and research of high-speed SUs running on rolling bearings.

제동 패턴을 고려한 드럼 브레이크의 열적 거동 특성에 대한 연구 (A Study on the Thermal Behavior Characteristic of Drum Brake considering Braking Patterns)

  • 이계섭;손성수;양기현
    • 한국자동차공학회논문집
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    • 제14권5호
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    • pp.145-154
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    • 2006
  • Each part of drum brake system is loaded by continual mechanical force and thermal force every time of braking, so enough strength and stability are required. Thermal characteristic is one of the important factors in drum brake systems design. This paper presents the thermal performance such as temperature distribution and thermal contact stress of drum brake system considering several braking patterns; 80th heat braking test mode, heat fade braking test mode, general road mode, steep slope road mode and off road mode. Transient heat transfer analysis and Thermo elastic contact analysis is executed to obtain the temperature distribution, and to evaluate thermal stress of drum brake by using ABAQUS/Standard code. This procedure of analysis can effectively be used to improve the quality problem of brake system and to get design guideline of the new product.

매스콘크리트 구조물의 수화열 저감을 위한 매개변수 연구 (Parametric Study for Reduction of Heat of Hydration in Mass Concrete)

  • 심종성;문도영;최광민
    • 한국콘크리트학회:학술대회논문집
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    • 한국콘크리트학회 2002년도 봄 학술발표회 논문집
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    • pp.29-34
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    • 2002
  • The heat of hydration of cement causes the internal temperature rise at early age, paticular in massive concrete structures. As the results of the temperature rise and restraint condition, the thermal stress may induce cracks in concrete. The prediction of the thermal stress is important in design and construction stages in order to control the cracks in mass concrete. It is poor economy to analysis for prediction of the thermal stress on each design or construction. In this study, the hydration heat and thermal stress analysis is performed by ABAQUS program, as a results of thermal analysis, the formula of size-placing depth relationship is proposed.

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지구관측 소형위성 비행모델의 열제어계 개발 및 성능 검증 (Development and Performance Validation of Thermal Control Subsystem for Earth Observation Small Satellite Flight Model)

  • 장진수;정연황;김병진
    • 한국항공우주학회지
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    • 제36권12호
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    • pp.1222-1228
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    • 2008
  • ㈜쎄트렉아이는 UAE의 EIAST와 함께 2008년 발사를 목표로 SI-200 표준버스시스템을 기반으로 하는 DubaiSat-1 비행모델을 개발하였다. DubaiSat-1 비행모델의 열제어계는 전력 소비의 최소화를 위해 수동 열제어를 기반으로 하되, 주요 부품에는 히터를 이용한 능동 열제어가 이뤄지도록 설계되었다. 또한 열해석 모델을 작성하여 DubaiSat-1의 임무궤도에 대해 열해석을 수행하였으며, 해석 결과를 토대로 모든 구성품이 설계 요구조건을 만족시킬 수 있도록 설계 보정 작업을 진행하였다. 또한 우주환경을 모사한 열진공시험을 수행하여 DubaiSat-1 비행모델의 열제어 성능에 대해 검토하였으며, 시험 결과와 해석 결과의 비교를 통한 열해석 모델의 보정 작업을 완료하였다.

상용 소프트웨어 ANSYS를 이용한 열전도문제의 형상설계 민감도 해석 (Shape Design Sensitivity Analysis of Thermal Conduction Problems using Commercial Software ANSYS)

  • 최주호
    • 대한기계학회논문집A
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    • 제24권3호
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    • pp.645-652
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    • 2000
  • A method for shape design sensitivity analysis is proposed utilizing commercial software ANSYS for thermal conduction problems. While the sensitivity formula is derived analytically by introduing adjoint variable concept, sensitivity calculation in practice as well as the primal and adjoint solution of thermal conduction is performed using the ANSYS very easily. Since the formula always takes boundary integral form, sensitivity evaluation in ANSYS requires a little more addition of post-processing routine which involves evaluation of boundary variable from the obtained solution. Though the BEM has been used as a better tool for this purpose, the present study shows it can also be calculated using any kind of analysis code such as ANSYS since the formula is based on analytic nature. Therefore the present study provides a new and efficient way of optimization which was not possible before using commercial software. The usefulness of the method is illustrated via a weight minimization problem of thermal diffuser.

고집적 원통형 수냉식 엔진 오일쿨러의 열적 해석 (Thermal Analysis of Compact Circular Water Cooled Engine Oil Cooler)

  • 윤준규
    • Journal of Advanced Marine Engineering and Technology
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    • 제22권6호
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    • pp.771-781
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    • 1998
  • A highly compact and thermally efficient water cooled oil cooler for automotive use without offset strip fin and casing is developed in this study. The study result has shown that eliminating the fin and casing in the oil cooler the manufacturing process and cost and can be simplified and reduced greatly without sacrificing the thermal capacity. The oil cooler developed in the study uses the dimply type heat transfer core element design instead of offset strip fin and eliminates the outer casing for coolant water flow by applying specially made parallel loop flow design. In the study the thermal design program for the present oil cooler also was developed and validated experimentally.

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열차폐코팅의 미세구조가 TGO 계면 응력에 미치는 영향 평가를 통한 미세구조 형상 설계 (Design of Microstructure by Evaluating the Effect of Thermal Barrier Coating's Microstructure on TGO Interface Stress)

  • 김담현;박기범;위성욱;김기근;박수;석창성
    • 한국군사과학기술학회지
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    • 제23권5호
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    • pp.435-443
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    • 2020
  • Thermal barrier coating(TBC) applied to fighter and turbine engines is a technology that improves the durability of core parts by lowering the surface temperature of base material. The thermal stress caused by mis-match of the coefficient of thermal expansion between the top coating and the TGO interface is the main cause of TBC breakage. Since the thermal stress is dependent on the microstructure of the TBC, designing microstructure of TBC can improve the durability as well as lower the thermal stress. In this study, the effect of coating thickness, volume of porosity and vertical cracking on the thermal stress was analyzed through finite element analysis. Through the analysis results, a design range of a microstructure that can improve the durability of thermal barrier coating by lowering thermal stress is proposed.

Conceptual design and analysis of rotor for a 1-kW-Class HTS rotating machine

  • Kim, J.H.;Hyeon, C.J.;Quach, H.L.;Chae, Y.S.;Moon, J.H.;Boo, C.J.;Kim, H.M.
    • 한국초전도ㆍ저온공학회논문지
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    • 제19권4호
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    • pp.45-50
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    • 2017
  • This paper presents a conceptual design and analysis for a 1-kW-class high-temperature superconducting rotating machine (HTSRM) rotor. The designed prototype is a small-scale integration system of a HTSRM and a HTS contactless rotary excitation device (CRED). Technically, CRED and HTSRM are connected in the same shaft, and it effectively charges the HTS coils of the rotor field winding by pumping fluxes via a non-contact method. HTS coils in rotor pole body and toroidal HTS wire in CRED rotor are cooled and operated by liquid nitrogen in cryogen tank located in inner-most of rotor. Therefore, it is crucial to securely maintain the thermal stability of cryogenic environment inside rotor. Especially, we critically consider not only on mechanical characteristics of the rotor but also on cryogenic thermal characteristics. In this paper, we conduct two main tasks covering optimizing a conceptual design and performing operational characteristics. First, rotor parameters are conceptually designed by analytical design codes. These parameters consider to mechanical and thermal performances such as mechanical strength, mechanical rigidity, and thermal heat losses of the rotor. Second, mechanical and thermal characteristics of rotor for 1-kW-class HTSRM are analyzed to verify the feasible operation conditions. Hence, three-dimensional finite element analysis (3D-FEA) method is used to perform these analyses in ANSYS-Workbench platform.