• 제목/요약/키워드: Thermal Sizing

검색결과 62건 처리시간 0.028초

가호조건에 따른 호부사의 물성변화 (The Physical Properties of Sizing Yarn According to Sizing Condition)

  • 박명수
    • 한국염색가공학회지
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    • 제16권3호
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    • pp.31-38
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    • 2004
  • Polyester fabrics, which is a major product in Daegu and Kyungbuk district, recently have a frequent warp streak phenomenon of sizing textiles for peach skin. So, this paper intensively focuses on the analysis of finding causes of poor products which may be produced in the process of sizing. Depending on the changes of sizing yarn's physical characteristic varying on sizing conditions, results of the research are as followed. 1. Sizing add-on rate, following tension changes of originally supplied yarn in sizing, does not fluctuate until 30g sizing tension, but marks high on the increase of sizing speed. 2. Sizing add-on amount increases approximately by 2.5% when interlacing pressure is raised from 1.5kg/$cm^2$ to 3.5kg/$cm^2$ at $130^{\circ}C$ sizing temperature. 3. Following the increase of sizing tension from 10g to 50g, boiling shrinkage rate of desizing yarn changes approximately from 7% to 11%. But the more sizing temperature and speed increases, the bigger the change rate becomes. 4. The thermal stress of desizing yarn is sensitively influenced by sizing tension in the sizing degree of above $130^{\circ}C$. 5. The deviation rate of sizing yarn's initial modulus value, which is influenced by air pressure in interlacing raw yarn, marks the highest at 40g and 50g strength.

Sizing of a tube inlet orifice of a once-through steam generator to suppress the parallel channel instability

  • Yoon, Juhyeon
    • Nuclear Engineering and Technology
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    • 제53권11호
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    • pp.3643-3652
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    • 2021
  • Sizing the tube inlet orifice of a Once-Through Steam Generator (OTSG) is important to protect the integrity of the tubes from thermal cycling and vibration wear. In this study, a new sizing criterion is proposed for the tube inlet orifice to suppress the parallel channel instability in an OTSG. A perturbation method is used to capture the essential parts of the thermal-hydraulic phenomena of the parallel channel instability. The perturbation model of the heat transfer regime boundaries is identified as a missing part in existing models for sizing the OTSG tube inlet orifice. Limitations and deficiency of the existing models are identified and the reasons for the limitations are explained. The newly proposed model can be utilized to size the tube inlet orifice to suppress the parallel channel instability without excessive engineering margin.

Conceptual design of a copper-bonded steam generator for SFR and the development of its thermal-hydraulic analyzing code

  • Im, Sunghyuk;Jung, Yohan;Hong, Jonggan;Choi, Sun Rock
    • Nuclear Engineering and Technology
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    • 제54권6호
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    • pp.2262-2275
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    • 2022
  • The Korea Atomic Energy Research Institute (KAERI) studied the sodium-water reaction (SWR) minimized steam generator for the safety of the sodium-cooled fast reactor (SFR), and selected the copper bonded steam generator (CBSG) as the optimal concept. This paper introduces the conceptual design of the CBSG and the development of the CBSG sizing analyzer (CBSGSA). The CBSG consists of multiple heat transfer modules with a crossflow heat transfer configuration where sodium flows horizontally and water flows vertically. The heat transfer modules are stacked along a vertical direction to achieve the targeted large heat transfer capacity. The CBSGSA code was developed for the thermal-hydraulic analysis of the CBSG in a multi-pass crossflow heat transfer configuration. Finally, we conducted a preliminary sizing and rating analysis of the CBSG for the trans-uranium (TRU) core system using the CBSGSA code proposed by KAERI.

정지궤도위성 광학탑재체 복사 열제어 시스템 개념 설계 (A CONCEPTUAL DESIGN OF RADIATIVE THERMAL CONTROL SYSTEM IN A GEOSTATIONARY SATELLITE OPTICAL PAYLOAD)

  • 김정훈;전형열
    • 한국전산유체공학회지
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    • 제12권3호
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    • pp.62-68
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    • 2007
  • A conceptual thermal design is performed for the optical payload system of a geostationary satellite. The optical payload considered in this paper is GOCI(Geostationary Ocean Color Imager) of COMS of Korea. The radiative thermal control system is employed in order to expect a small thermal gradient in the telescope structure of GOCl. Two design margins are applied to the dedicated radiator dimensioning, and three kinds of configuration to the heater power sizing. A Monte-Carlo ray tracing method and a network analysis method are utilized to calculate radiative couplings and thermal responses respectively. At the level of conceptual design, sizing thresholds are presented for the radiator and heater on the purpose of determining the mass and power budget of the spacecraft.

Modeling of an Once Through Helical Coil Steam Generator of a Superheated Cycle for Sizing Analysis

  • Kim, Yeon-Sik;Sim, Yoon-Sub;Kim, Eui-Kwang
    • 한국원자력학회:학술대회논문집
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    • 한국원자력학회 1997년도 추계학술발표회논문집(1)
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    • pp.558-563
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    • 1997
  • A thermal sizing code, named as HSGSA (Helical coil Steam Generator Sizing Analyzer), for a sodium heated helical coil steam generator is developed for KALIMER (Korea Advanced LIquid MEtal Reactor) design. The theoretical modeling of the shell and tube sides is described and relevant correlations are presented. For assessment of HSGSA, a reference plant design case is compared to the calculational outputs from HSGSA simulation.

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다운 스피딩이 NEDC 모드 연비에 미치는 기여도 산출에 관한 연구 (Analysis of Down Speeding Effect on Fuel Economy during NEDC)

  • 심범주;박경석;박준수
    • 한국자동차공학회논문집
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    • 제20권5호
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    • pp.88-94
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    • 2012
  • Development trend of modern HSDI diesel engine is now focusing on low fuel consumption and emission because of strong interest in global environmental protection. Two big branches of criteria for modern diesel engine development are down sizing and down speeding. Down sizing keeps engine operation condition to the direction of higher load and thus pursuing for better thermal efficiency. But this may cause degraded vehicle dynamic performance because of reduced back up torque. Down speeding keeps engine operation condition to the direction of slightly higher load and lower engine speed. Therefore reduction of back up torque can be limited within flat torque area. This study analyzed fuel economy effect of down speeding on a vehicle powered by HSDI diesel engine in aspect of engine friction work, intake and exhaust pumping work, exhaust hat loss and thermal loss of fuel leakage of fuel injection system. Contribution factor of each engine and vehicle related parameters under basic and down speeding condition were compared and work balance of down speeding during NEDC was analyzed.

초음파 Spectroscopy에 의한 Resin내의 크기 측정에 관한 연구

  • 한응교;김용재;이범성;박익근;소반신부
    • 한국정밀공학회:학술대회논문집
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    • 한국정밀공학회 2001년도 추계학술대회 논문집
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    • pp.139-143
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    • 2001
  • In manufacturing process of semiconductor package, thermal stress owing to high temperature in moulding and bubbles generated in chip bonding process become main causes to producing void. Therefore, on this study we evaluated quantitatively void size by ultrasonic spectroscopy method which analyze the frequency of this received pulse using pulses with broad band frequency, and after destructive test we verified effectiveness of sizing void by ultrasonic spectroscopy as we find error degree between the real size of void and the sizing void by ultrasonic spectroscopy.

초음파 분량법에 의한 레진 내부 결합의 크기 측정에 관한 연구 (Sizing of lnner Flaw in Resin by using Ultrasonic spectroscopy)

  • Han, E.K.;Kim, Y.J.;Park, I.G.
    • 한국정밀공학회지
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    • 제10권3호
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    • pp.182-190
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    • 1993
  • In manufacturing process of semiconductor package, the thermal stress owing to high temperature in moulding and the bubbles generated in chip bonding process become main causes to produce void. On this study we evaluated quantitatively void size by use of ultrasonic spectroscopy method which analyze the reflective pulses with broad band frequency in frequency domain, and after destructive testing we verified effectiv- eness of sizing void by use of ultasonic spectroscopy.

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고속 비행체 연료공급 및 냉각계통 예비 열설계 (Preliminary Thermal Sizing of Fuel Supply and Cooling System for High-speed Vehicles)

  • 최세영;박수용;최현경;김준태;정해승;박정배
    • 한국추진공학회지
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    • 제18권1호
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    • pp.97-104
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    • 2014
  • 고속 비행체에 연료를 공급하고, 내/외부의 열부하를 처리하기 위한 연료공급 및 냉각계통의 예비 열설계를 수행하였다. 이를 위해 임의의 임무형상에 대한 해석모델을 구성하고 성능해석을 진행하였다. 산출된 연료소모율과 내부의 유동 상태량을 이용하여 시스템의 각부 경계조건에 대한 열부하량을 계산하고 검증하였다. 이를 연료의 흡열반응을 이용한 시스템의 냉각성능과 비교하여 설계 요구조건을 충족시키는 것을 확인하였다.