• 제목/요약/키워드: Low temperature liquid

검색결과 894건 처리시간 0.021초

분리형 에어컨용 2중 열교환 배관 특성에 관한 실험적 연구 (Experimental Study of Characteristics on Double Heat Exchange Pipe Used Separation Type Air-Conditioner)

  • 김재돌
    • 동력기계공학회지
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    • 제10권4호
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    • pp.31-37
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    • 2006
  • In this study, the ability for the function of double pipe inserted liquid pipe with small diameter in the gas pipe with large diameter for the circulating of liquid of high temperature and high pressure and low temperature and low pressure at the same time is presented. And in this double pipe, liquid pipe of high temperature and pressure is used to connect condenser and expansion valve and gas pipe of low temperature is used to connect evaporator and compressor. Also, when liquid refrigerant of high temperature and gas refrigerant of low temperature is circulated by reversed flow in the double pipe. The contribution of liquid gas heat exchange pipe is studied by comparison of the effect of heat transfer by temperature difference when liquid pipe and gas pipe is installed separately.

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횡단 공기유동장으로 분사되는 저온 에탄올 제트의 침투거리 (Penetration Height of Low-temperature Ethanol Jet Injected Into a Crossflow Airstream)

  • 이종권;구자예
    • 한국분무공학회지
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    • 제25권2호
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    • pp.74-80
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    • 2020
  • The jet in crossflow is a spray method used in the various air-breathing engine. In order to understand the spray characteristics in various environments, many prior studies have been conducted. However, there is a lack of understanding of the low-temperature liquid spray characteristics below 273 K. With this in mind, we tried to enhance the knowledge of the low-temperature liquid spray characteristics by identifying the penetration height of low-temperature ethanol. The experiment was conducted under phase pressure, and 273 K of air and 293, 263, and 233 K of ethanol was used. Shadowgraphy was employed to measure the liquid penetration, and Otsu's method was used to analyze the penetration height. The heights tend to decrease as the temperature of the liquid jet decreases. A correlation for the penetration height in the experimental conditions was derived and presented.

액체암모니아 처리 면직물의 염색성 - 저온형과 고온형 반응성 염료에 의한 염색물의 색상강도 - (Dyeability of Cotton Fabrics Treated with Liquid Ammonia - Color strength of the dyeings with low-temperature and high-temperature reactive dyes -)

  • 전성기;이창수;임용진;김태경
    • 한국염색가공학회지
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    • 제16권2호
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    • pp.1-7
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    • 2004
  • The dyeability of cotton fabrics treated with liquid ammonia was investigated using low-temperature and high-temperature reactive dyes. From the results of dyeing rates of direct dye, the inversion time was shown at 600 hours at $40^{\circ}C$, and however it was shown at 10 minutes at $80^{\circ}C$. This was applied to reactive dyeings. In the low-temperature reactive dyes, the color strength of the fabrics treated with liquid ammonia was lower than that of mercerized fabrics. By contrast, in the high-temperature reactive dyes, the color strength of the fabrics treated with liquid ammonia was higher than that of mercerized one.

Fast Switching of Vertically Aligned Liquid Crystals by Low-Temperature Curing of the Polymer Structure

  • Park, Byung Wok;Oh, Seung-Won;Kim, Jung-Wook;Yoon, Tae-Hoon
    • Journal of the Optical Society of Korea
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    • 제18권4호
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    • pp.395-400
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    • 2014
  • We proposed a method for fast turn-off switching of a vertically-aligned liquid crystal cell by low-temperature curing of the polymer structure. We confirmed that the turn-off times of the fabricated cells were reduced significantly as the curing temperature was lowered to $-20^{\circ}C$. We accounted for the effect of low-temperature curing on the turn-off time by using a mathematical model and by observing images obtained via scanning electron microscopy. We also confirmed that low-temperature curing is more effective in reducing the response time when the device is operated at a low temperature.

Low Temperature Test of HWR Cryomodule

  • Kim, Heetae;Kim, Youngkwon;Lee, Min Ki;Park, Gunn-Tae;Kim, Wookang
    • Applied Science and Convergence Technology
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    • 제25권3호
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    • pp.47-50
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    • 2016
  • Low temperature test for half-wave resonator (HWR) cryomodule is performed at the superfluid helium temperature of 2 K. The effective temperature is defined for non-uniform temperature distribution. Helium leak detection techniques are introduced for cryogenic system. Experimental set up is shown to make the low temperature test for the HWR cryomodule. The cooldown procedure of the HWR cryomodule is shown from room temperature to 2 K. The cryomodules is precooled with liquid nitrogen and then liquid helium is supplied to the helium reservoirs and cavities. The pressure of cavity and chamber are monitored as a function of time. The vacuum pressure of the cryomodule is not increased at 2 K, which shows leak-tight in the superfluid helium environment. Static heat load is also measured for the cryomodule at 2.5 K.

Bath cryostat의 제작특성에 관한 연구 (A study on the construction characteristic of bath cryostat)

  • Kim, G.Y.
    • 한국정밀공학회지
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    • 제10권2호
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    • pp.138-145
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    • 1993
  • The bath cryostat of cryogenic apparatuses which are generally used to study physical phenomena under low temperature and ultra low temperature has been desigened and constructed. The practical use of the cryostat is verified by the measurement of the storage life of liquid heloum and liquid nitrogen vessels. The cryostat consists of triple structure of high vacuum environment in order to minimize the evaporation rate of liquid helium and liquid nitrogen by thermal conductivity and radiant heat. The minimum thickness which can stand against inner and outer pressures is calculated from considering the strength of the material.

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저온 열분해시 HDPE 및 LDPE의 액화 특성 (Liquefaction Characteristics of HDPE and LDPE in Low Temperature Pyrolysis)

  • 이봉희;박수열;김지현
    • 한국응용과학기술학회지
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    • 제23권4호
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    • pp.307-318
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    • 2006
  • The pyrolysis of high density polyethylene(HDPE) and low density polyethylene(LDPE) was carried out at temperature between 425 and $500^{\circ}C$ from 35 to 80 minutes. The liquid products formed during pyrolysis were classified into gasoline, kerosene, gas oil and wax according to the petroleum product quality standard of Korea Petroleum Quality Inspection Institute. The conversion and yield of liquid products for HDPE pyrolysis increased continuously according to pyrolysis temperature and pyrolysis time. The influence of pyrolysis temperature was more severe than pyrolysis time for the conversion of HDPE. For example, the liquid products of HDPE pyrolysis at $450^{\circ}C$ for 65 minutes were ca. 30wt.% gas oil, 15wt.% wax, 14wt.% kerosene and 11wt.% gasoline. The increase of pyrolysis temperature up to $500^{\circ}C$ showed the increase of wax product and the decrease of kerosene. The conversion and yield of liquid products for LDPE pyrolysis continuously increased according to pyrolysis temperature and pyrolysis time, similar to HDPE pyrolysis. The liquid products of LDPE pyrolysis at $450^{\circ}C$ for 65 minutes were ca. 27wt.% gas oil, 18wt.% wax, 16wt.% kerosene and 13wt.% gasoline.

윤활상태에서 플라스틱의 마찰특성에 관한 연구 (A Study of the Friction Characteristics of Plastics on Lubricated Condition)

  • 강석춘
    • Tribology and Lubricants
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    • 제8권1호
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    • pp.48-55
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    • 1992
  • The friction characteristic of plastics (PTFE, Nylon, Acetal and phenolic) was studied on the lubricated condition with a pin on disk machine. Mineral oil without additive (base oil) and water were used as liquid lubricants at the controlled temperature. From the experimental work, it was found out that the coefficient of friction of plastics was controlled by the mechanical properities of plastic more than that of liquid for various load and temperature. Viscosity of liquid has affected on the friction only at low temperature under lighb load. Among the tested plastics, the coefficient of friction of PTFE was the lowest under light load and at low temperature while Nylon at medium load and temperature, and Acetal at heavy load and high temperature. The coefficient of friction of soft plastics like PTFE and Nylon were increased as the load and temperature were increased, while that of hard plastic (Acetal) was decreased and that of thermo setting plastic (phenolic) was mixed. Also for soft plastics, the coefficient of friction under heavy load was always higher than that under light load, while hard plastic was vice versa.

액분사 사이클을 이용한 공기 열원 열펌프의 사이클 시뮬레이션 (Cycle Simulation of an Air Source Heat Pump Using Liquid Injection)

  • 김욱중;홍용주;남임우;강원일;공용상
    • 설비공학논문집
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    • 제12권3호
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    • pp.244-250
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    • 2000
  • An air source heat pump using liquid injection technique, which can be applied for very low temperature climate, has been simulated to examine the design options. Comparison between the simulation and experiment has been carried out to validate the simulation method. Effects of various design parameters such as liquid injection rate and injection pressure are Investigated to optimize the performance of the heat pump. Finally, optimal liquid infection rate and injection pressure to maintain sufficient heating capacity and moderate discharge refrigerant temperature are suggested when the heat pump was operated at very low outdoor temperature.

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저온 비등 팽창유체와 고점성 유체마개를 이용한 고출력 저전력형 마이크로 분사기 (High-impulse, Low-Power Microthruster using Liquid Propellant with High-Viscosity Fluid Plug)

  • 김상욱;강태구;조영호
    • 대한기계학회논문집B
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    • 제26권6호
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    • pp.868-874
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    • 2002
  • A high-impulse, low-power, digital microthruster has been developed using low-boiling-temperature liquid propellant with high-viscosity fluid plug. The viscous fiction force of the fluid plug increases the blast pressure and the low-boiling-temperature liquid propellant is intended to reduce input power consumption. The three-layer microthruster has been fabricated by surface micromachining as well as bulk micromachining in the size of 7$\times$13$\times$1.5㎣. A digital output impulse bit of 6.4$\times$10$^{-8}$ Nsec has been obtained from the fabricated microthruster using perfluoro normal hexane (FC72) propellant and oil plug, resulting in about ten times increase of the impulse bit using one hundredth electrical input energy compared to the conventional multiple-shot microthruster.