• Title/Summary/Keyword: 열적 사이클

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A study on the comparative test of chemical and thermal properties of virgin and recycled PET products (버진 및 리사이클 PET 제품의 화학적·열적 특성 비교시험에 관한 연구)

  • Kim, Kyoung Pil;Seo, Kyung Jin;Park, Soo-Yong;Chung, Ildoo
    • Journal of the Korea Academia-Industrial cooperation Society
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    • v.22 no.2
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    • pp.33-39
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    • 2021
  • As the interest and demand in the recycled yarn field has increased rapidly worldwide, domestic companies are also promoting research and development and business on recycled yarn. The chemical and thermal properties of four types of virgin and recycled PET samples from A and B company, which are the leading domestic companies in the recycled polyester yarn business, were confirmed through infrared (FT-IR) spectroscopy and differential scanning calorimetry (DSC). Virgin and recycled PET from two companies were compared. FT-IR spectroscopy revealed the typical spectra of PET for both companies and a different peak at 872 cm-1. DSC confirmed that the melting point and crystallization temperature of recycled PET were lower than those of virgin PET. These results indicate that small amounts of contaminants are an important parameter affecting the thermal properties of recycled PET. In the DSC results after seven repeats of the heating and cooling processes, all four samples showed that a lower melting point, crystallization temperature, and low heat flow intensity increased with increasing number of cycles. The results of melting and crystallization enthalpy also showed similar patterns.

Measurement of CTE Change in a Composite Laminate with Aging under Space Environment using Fiber Optic Sensors (광섬유센서를 이용한 우주환경하에서 복합재료 적층시편의 노화에 따른 열팽창계수변화 측정)

  • Gang,Sang-Guk;Gang,Dong-Hun;Kim,Cheon-Gon;Hong,Chang-Seon
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.31 no.10
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    • pp.21-26
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    • 2003
  • In this research, the change of coefficient of thermal expansion (CTE) of graphite/epoxy composite laminate under space environment was measured using fiber optic sensors. Two fiber Bragg grating (FBG) sensors have been adopted for the simultaneous measurement of thermal strain and temperature. Low Earth Orbit (LEO) conditions with high vacuum, ultraviolet and thermal cycling environments were simulated in a thermal vacuum chamber. As a pre-test, a FBG temperature sensor was calibrated and a FBG strain sensor was verified through the comparison with the electric strain gauge (ESG) attached on an aluminun specimen at high and low temperature respectively. The change of the CTE in a composite laminate exposed to space environment was measured for intervals of aging cycles in real time. As a whole, there was no abrupt change of the CTE after 1000 aging cycles. After aging, however, the CTE decreased a Little all over the test temperature range. These changes are caused by outgassing, moisture desorption, matrix cracking etc.

Thermal Behavior of Spacecraft Liquid-Monopropellant Hydrazine($N_2$$H_4$) Propulsion System (인공위성 단기액체 하이드라진($N_2$$H_4$) 추진시스템의 열적 거동)

  • Kim, Jeong-Soo
    • Journal of the Korean Society of Propulsion Engineers
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    • v.3 no.4
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    • pp.1-11
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    • 1999
  • Thermal behavior of spacecraft propulsion system utilizing monopropellant hydrazine ($N_2$$H_4$) is addressed in this paper. Thermal control performance to prevent propellant freezing in spacecraft-operational orbit was test-verified under simulated on-orbit environment. The on-orbit environment was thermally achieved in space-simulation chamber and by the absorbed-heat flux method that implements an artificial heating through to the spacecraft bus panels enclosing the propulsion system. Test results obtained in terms of temperature history of propulsion components are presented and reduced into duty cycles of the avionics heaters which are dedicated to thermal control of those components. The duty cycles are subsequently converted into the electrical power required in the operational orbit. Additionally, cyclic temperature of each component, which was made under thermal-balanced condition of spacecraft, is compared to the acceptable design range and justified from the viewpoint of system verification.

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Thermal Analysis of a Combined Absorption Cycle of Cogeneration of Power and Cooling for Use of Low Temperature Source (저온 열원의 활용을 위한 흡수 발전/냉각 복합 사이클의 열적 해석)

  • Kim, Kyoung-Hoon
    • Korean Journal of Air-Conditioning and Refrigeration Engineering
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    • v.23 no.6
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    • pp.413-420
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    • 2011
  • Thermodynamic cycles using binary mixtures as working fluids offer a high potential for utilization of low-temperature heat sources. This paper presents a thermodynamic performance analysis of Goswami cycle which was recently suggested to produce power and cooling simultaneously and combines the Rankine cycle and absorption refrigeration cycle by using ammoniawater mixture as working fluid. Effects of the system parameters such as concentration of ammonia and turbine inlet pressure on the system are parametrically investigated. Results show that refrigeration capacity or thermal efficiency has an optimum value with respect to ammonia concentration as well as to turbine inlet pressure.

Study on the Thermal Characteristics of Organic Rankine Cycles for Use of Low-Temperature Heat Source (저온열원 활용을 위한 유기랭킨사이클의 열적 특성에 관한 연구)

  • Jin, Jae-Young;Kim, Kyoung-Hoon
    • 한국태양에너지학회:학술대회논문집
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    • 2011.04a
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    • pp.191-194
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    • 2011
  • Low-grade waste heat has generally been discarded in industry due to lack of efficient recovery methods. In recent years, organic Rankine cycle(ORC) has become a field of intense research and appears as a promising technology for conversion of heat into useful work of electricity. In this work thermodynamic performance of ORC with superheating of vapor is comparatively assessed for various working fluids. Special attention is paid to the effects of system parameters such as the evaporating temperature on the characteristics of the system such as maximum possible work extraction from the given source, volumetric flow rate per 1 kW of net work and quality of the working fluid at turbine exit as well as thermal efficiency.

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Effects of Internal Heat Exchanger on Performance of Organic Rankine Cycles (유기랭킨사이클의 성능에 미치는 내부열교환기의 영향)

  • Kim, Kyoung-Hoon;Jung, Yoong-Guan
    • Transactions of the Korean hydrogen and new energy society
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    • v.22 no.3
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    • pp.402-408
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    • 2011
  • Organic Rankine cycles (ORC) can be used to produce power from heat at different temperature levels available as geothermal heat, as biogenic heat from biomass, as solar or as waste heat. In ORC working fluids with relatively low critical temperatures and pressures can be compressed directly to their supercritical pressures and heated before expansion so as to obtain a better thermal match with their heat sources. In this work thermal performance of ORC with and without an internal heat exchanger is comparatively investigated in the range of subcritical and transcritical cycles. R134a is considered as working fluid and special attention is paid to the effect of turbine inlet pressure on the characteristics of the system. Results show that operation with supercritical cycles can provide better performance than subcritical cycles and the internal heat exchanger can improve the thermal efficiency when the temperature of heat source becomes higher.

Fatigue Life Analysis for Solder Joint of Optical Thin Film Filter Device (다층 박막 광학 필터 디바이스의 패키징시 솔더 조인트의 피로파괴 수명 해석)

  • 김명진;이형만
    • Journal of the Microelectronics and Packaging Society
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    • v.10 no.2
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    • pp.19-26
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    • 2003
  • Plastic and creep deformations of a solder joint on thermal cycle play an important role in the reliability of optical telecommunication components. Solder joint strain is increased with the thermal cycle time and it causes mis-alignments and power loss in the optical component. Furthermore, the component can be failed since the deformation exceed the limitation of the fatigue life. We applied the finite element analysis method to solve the problem of the solder joint reliability on thermal cycle. Plastic and creep deformations are calculated by the finite element method. And, the fatigue lire is predicted by using creep-fatigue prediction models with calculated strains. The temperature conditon of the analysis was referred from the Telcordia reliability schedule (-40 to 75). Also, the three ramp renditions, 1/min, 10/min and 50/min, and dwelling time were considered to analyze the differences of results.

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Thermal Behavior of NiFe2O4 for Hydrogen Generation (NiFe2O4를 이용한 열화학 사이클 H2 제조)

  • Han, S.B.;Kang, T.B.;Joo, O.S.;Jung, K.D.
    • Transactions of the Korean hydrogen and new energy society
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    • v.14 no.4
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    • pp.298-304
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    • 2003
  • The thermal behavior of $NiFe_2O_4$ prepared by a solid-state reaction was investigated for $H_2$ generation by the thermochemical cycle. The reduction of $NiFe_2O_4$ started from $800^{\circ}C$, and the weight loss was 0.2-0.3 wt% up to $1000^{\circ}C$. In the $H_2O$ decomposition reaction, $H_2$ was generated by oxidation of reduced $NiFe_2O_4$. The crystal structure of $NiFe_2O_4$ maintained during the redox reaction of 5 cycles. From this observation, the lattice oxygen in $NiFe_2O_4$ is released without the structural change during the thermal reduction and oxygen deficient $NiFe_2O_4$ can be restored to the spinel structure of $NiFe_2O_4$.

크라이오펌프 국산 개발품 공정 신뢰성 및 내구성 시험

  • In, Sang-Ryeol;Gang, Sang-Baek;No, Yeong-Ho;Yu, Jae-Gyeong
    • Proceedings of the Korean Vacuum Society Conference
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    • 2013.08a
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    • pp.119-119
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    • 2013
  • 5년 동안 진행된 고진공 펌프 개발 사업의 일환으로 맥동관형 냉동기에 활성탄 어레이를 장착한 흡기구 직경 14인치 국산 크라이오펌프 완제품이 만들어졌다. 이미 지난해에 완성한 시제품을 가지고 모든 배기성능시험을 완료하고 목표를 뛰어 넘는 성능을 가지고 있음을 입증하였지만 완제품의 경우는 현장에서 스퍼터링 공정에 대한 신뢰성과 열적 내구성 시험이 중요한 항목으로 대두되었다. 개발된 펌프를 생산 공정에 직접 투입하는 모험을 하지 않으면서도 신뢰성을 확보하는 방편으로 카이스트 나노종합팹 센터에서 가동중인 스퍼터링 장비에 완제품을 달고 기존 공정과 같은 방식으로 장치를 운영하면서 외제 상용품을 사용했을 때와 진공성능 및 공정수율을 비교하는 시험을 수행하였다. 또 내구성 시험 항목으로 열부하 시험과 열 사이클 시험을 수행하였다. 열부하 시험은 300도까지 온도를 올릴 수 있는 열판을 펌프 흡기구 배플 앞에 설치하여, 냉동기 2차 냉각단 온도가 20 K 이하로 유지될 수 있는 최대 허용 복사열을 측정하는 방식으로 진행되었으며 열 사이클 시험은 크라이오 펌프의 활성화 기능을 활용하여 완전 활성화(full regen., 10K-300K-10K) 과정을 10회 연속 시행하여 펌프의 배기성능과 기계적 이상 유무를 관찰하였다.

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Thermal Behavior of $NiFe_2O_4$ for Hydrogen Generation (열화학 사이클 $H_2$ 제조를 위한 $NiFe_2O_4$의 열적 거동)

  • 한상범;강태범;주오심;정광덕
    • Proceedings of the Korea Society for Energy Engineering kosee Conference
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    • 2003.11a
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    • pp.51-55
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    • 2003
  • The thermal behavior of NiFe$_2$O$_4$ prepared by a solid-state reaction was investigated for H$_2$ generation by the thermochemical cycle. The reduction of NiFe$_2$O$_4$ started from 800 $^{\circ}C$, and the weight loss was 0.2-0.3 wt% up to 1000 $^{\circ}C$. At this reaction, NiFe$_2$O$_4$ was reduced by release of oxygen bonded with the Fe$^3$ion in the B site of NiFe$_2$O$_4$. In the $H_2O$ decomposition reaction, H$_2$ was generated by oxidation of reduced NiFe$_2$O$_4$. The crystal structure of NiFe$_2$O$_4$ for redox reaction maintained spinel structure. Then, NiFe$_2$O$_4$ is excellent material in the thermochemical cyclic reaction due to release oxygen at low temperature for the reduction reaction and produce H$_2$ maintaining crystal structure for redox reaction.

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