• Title/Summary/Keyword: 흡입온도

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Studies on the Morphology of Smoke Particles for Each Type of Fire by Using Steady State Tube Furnace (등속공급 튜브연소로를 이용한 각 연소조건에서의 연기입자 형상 분석)

  • Goo, Jaehark
    • Fire Science and Engineering
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    • v.28 no.1
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    • pp.44-51
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    • 2014
  • Smoke from fire is a mixture of combustion gases and particles which include micro-droplets formed from condensed organic vapors and carbonaceous agglomerates. The inhalation of smoke particles causes adverse health effects, and it is prerequisite for the hazard and risk analysis of the smoke particles to know how they behaviour in the respiratory tract. The characteristics of the absorption and adsorption of toxic gases and the amount and location of the particle deposition within the respiratory tract that determine the adverse health effects are related to the morphology and the size distribution of smoke particles. In the present work, as a preliminary study for the adverse health effects of smoke particles, the morphologies of the smoke particles from combustible materials were investigated for each fire stage: smouldering, well-ventilated flaming, small under-ventilated flaming, fully-developed under-ventilated fire. The steady-state tube furnace method given in ISO/TS 19700 was used for the generation of smoke particles. The fire stages were controlled by changing furnace temperature and equivalent ratio. The morphologies were analyzed by using Transmission Electron Microscope (Bio-TEM) by collecting the particles on TEM grids put on each stage of a cascade impactor.

Development of Organic Fertilizer based on the Cow Dung -II. Studies on Rapid Fermentation (우분(牛糞)의 유기질비료화(有機質肥料化) 연구(硏究) -II. 속성부숙방법(速成腐熟方法))

  • Lim, Dong-Kyu;Moon, Yoon-Ho;Shin, Jae-Sung;Woo, Ki-Dae
    • Korean Journal of Soil Science and Fertilizer
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    • v.24 no.3
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    • pp.192-199
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    • 1991
  • To manufacture a good organic fertilizer through rapid composting process, cow dung was mixed with bulking materials such as rice straws, shredded bark, wood chips, and saw dust. The mixing ratio of the cow dung and bulking material was two to one on volume basis and moisture content was adjusted to 60 to 70 percent, C/N ratio 25 to 30 and aeration forced with suction during the aerated pile fermentation. Aerated pile was established outdoors and curing pile was in vinylhouse and the experiment was conducted for 3 years from '88 to '90. After pilling, temperature in aerated pile was reached to the maximum level at 7 to 9 days and the temperatures of cow dung + shredded bark, cow dung + wood chips, and cow dung + rice straws were higher than that of cow dung, and cow dung + saw dust. Total carbon, and C/N ratio in aerated pile fermentation period were increased in the middle stage and then they were decreased with the process of days, and nutrient contents in curing pile period had the same tendency as in the aerated pile.

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Evaluation of Composite Mold for Small Composite Propeller (소형 복합재료 프로펠러를 위한 복합재료 몰드 평가)

  • Nhut, Pham Thanh;Yum, Young Jin
    • Transactions of the Korean Society of Mechanical Engineers A
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    • v.37 no.2
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    • pp.279-285
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    • 2013
  • The feasibility of substituting a composite mold for an aluminum mold in the fabrication of a small ship propeller was investigated. A small three-blade aluminum propeller was used as a plug for manufacturing the composite mold. A GRPG composite mold and propeller were made from an unsaturated polyester resin, Epovia gelcoat, and woven and mat glass fibers using the compression and vacuum method at room temperature. The hardness and surface roughness and the strength and deformation of the compression and suction molds were experimentally determined. The results were compared with the ISO 484/2 standard and some aluminum alloy materials. The results showed that the deformation of the mold satisfied the tolerance of the thickness of the blade. Some characteristics of the GRPG composite mold were better than those of the aluminum alloy mold (surface smoothness, weight, performance, and cost), and some characteristics were similar (detachment ability and life-cycle). Therefore, the composite mold is considered suitable for the fabrication of a small composite ship propeller.

Survey on the Concentration of Sulphur Dioxide Gas in the Plastic Film House Cultivation (시설(施設) 하우스내 아황산(亞黃酸)(SO2)가스 발생현황(發生現況) 조사(調査))

  • Kim, Bok-Young;Lee, Jong-Sik;Jung, Goo-Bok
    • Korean Journal of Soil Science and Fertilizer
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    • v.30 no.4
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    • pp.357-360
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    • 1997
  • To fine out the concentration of $SO_2$ gas in plastic film house, the survey was conducted at 343 sites throughout the nation. The $SO_2$ concentration in plastic film house were similar both heating and non-heating, but $SO_2$ cocentration higher than 0.8ppm was detected at those with heating. The $SO_2$ concentration in plastic film house cultivated red-pepper higher than those of cucumber or tomato cultivation, and it was produced higher amounts at day time than night due to the higher temperature. In plastic film house with heating, $SO_2$ was leaked at brocken parts of heater and joint of stove pipe, sometimes, $SO_2$ discharged from smokestack was resucked with air. $SO_2$ concentration in the plastic film house with and without ventilation were 0.2 and 0.6ppm, respectively.

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An Experimental Study on Fire-Resistant Boom (내화용 오일붐의 내화성에 대한 실험적 연구)

  • Yu J.S.;Sung H.G.;Oh J.H.
    • Journal of the Korean Society for Marine Environment & Energy
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    • v.3 no.2
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    • pp.25-32
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    • 2000
  • Fire-resistant boom is one of the most important facilities in in situ homing of spilled oil. Thermal response of a fire-resistant boom to turning is experimentally investigated in this paper by using an electric furnace and a burning test facility. This test facility is composed of a test tank, a fire boom, a hood for inhaling smoke, an incinerator for burning up gases and thermocouples, etc. Thereby a systematic method of approach in small laboratory scale is developed to study the performance of a fire-resistant boom. Burning test is carried out for the fire boom model which has been developed through the present study. It is shown that the present fire boom model has capability to withstand the high temperature around 800℃ and high rate of heat flux on it due to homing. For more realistic experimental environments, larger dimensions in devices and longer time in experiments are recommended in near future.

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The Isoflurane Concentration of Precision Vaporizer Goldman Vaporizer According to Room Temperature and Carrier Gas Flow Rate (온도 및 유량에 따른 흡입 마취제 전용 기화기와 Goldman 기화기의 isoflurane 농도 변화)

  • 김성미;장화석;이정선;최치봉;임희란;최준철;김휘율
    • Journal of Veterinary Clinics
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    • v.21 no.3
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    • pp.270-275
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    • 2004
  • Anesthetic machines may be equipped with either a precision or nonprecision vaporizer. A precision vaporizer is designed to deliver an exact concentration of anesthetic agent. Goldman vaporizer is a low-flow, closed-circle circuit with a low resistance vaporizer, in circuit. Vaporizers used within circle system(VIC) are not usually temperature compensated and this is generally thought to be a disadvantage. As the volatile agent is vaporized, heat is extracted from the liquid and temperature decreases. This cooling of the liquid leads to a decrease in concentration of the anaesthetic agent delivered by the vaporizer. The purpose of this study is to examine the mechanical consistency of the delivery of isoflurane from Goldman vaporizer and precision vaporizer at various gas flow rates and temperatures. And we first studied isoflurane concentration according to room temperature changes delivered by a Goldman vaporizer and precision vaporizer using different gas flow. The room temperature of $15^{\circ}C,$ $20^{\circ}C,$ $28^{\circ}C$ and fresh gas flow rates of 0.5, 1.0, 1.5, 2.0, 3.0 l/min were used. The inspired agent concentration was measured using a Datex-Ohmeda multigas analyzer. As rose in room temperature, the isoflurane concentration of precision vaporizer approximated the dial setting. On the other hand, at a dial setting concentration of 5.0 percent the delivered isoflurane concentration of precision vaporizer was more than the dial setting in high temperature. The isoflurane concentration of precision vaporizer remained constant despite the increase in temperature. The isoflurane concentration of Goldman vaporizer was increased with rise in room temperature and decreased with rise in gas flow.

A Study on Improving Environmental Characteristics of Cyclone Vacuum Cleaner using Life Cycle Assessment (LCA 평가를 이용한 싸이클론 진공청소기의 친환경성 개선방안에 관한 연구)

  • Hwang, Bo-Seok;Yoon, Yong-Han;Lee, Chanhyun;Yi, Hwa-Cho
    • Clean Technology
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    • v.20 no.3
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    • pp.241-250
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    • 2014
  • In this study, performance and environmental characteristics of cyclone vacuum cleaners are analyzed and product improvement methods are investigated to minimize environmental effect of the cleaners using the result. A simplified LCA method is used to analyze environmental characteristics of the cyclone vacuum cleaners. Two cyclone vacuum cleaners with similar specifications are chosen for the experiment. Typical characteristics of cyclone vacuum cleaners such as energy consumption, suction force, noise and temperature are measured and compared. Most environmental effect was caused by the energy consumption in use phase of life cycle. Some ideas are created to reduce energy consumption of the vacuum cleaners in use phase like installing baffle, and methods to extend exchange period of filter. It is analyzed how recyclability rate of vacuum cleaners could be improved to reduce the environmental effect in whole life of the vacuum cleaners.

Performance Analysis by CFD and Aerodynamic Design of 100kW Class Radial Turbine Using Waste Heat from Ship (선박 폐열을 이용한 100kW급 구심터빈 공력설계 및 CFD에 의한 성능해석)

  • Mo, Jang-Oh;Kim, You-Taek;Kim, Mann-Eung;Oh, Cheol;Kim, Jeong-Hwan;Lee, Young-Ho
    • Journal of Advanced Marine Engineering and Technology
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    • v.35 no.2
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    • pp.175-181
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    • 2011
  • The purpose of this study is to secure the design data for the optimization of the radial turbine and heat cycle system, by using the CFD analysis technique and the design of 100kW class radial turbine applicable to waste heat recovery generation system for ship. Radial turbine was comprised of scroll casing, vane nozzle with 18 blades and rotor with 13 blades, and analysis grid was used to about 2.3 million. Mass flow rate and rotational speed was 0.5kg/s, 75,0000rpm, respectively. Eight kinds of inlet pressure was set between 195 and 620kPa. As the flow accelerated through the nozzle passage to the throat, the pressure level at the pressure and suction sides becomed similar to about Mach number of 0.35. When the inlet temperature and pressure was $250^{\circ}C$, 352kPa respectively, the isentropic efficiency and mechanical power showed the analysis results of 74% and 108kW.

Effect of Plastic Injection on the Blast Furnace Operation Under One-Tuyere Test (플라스틱의 풍구 1본 시험흡입에 따른 고로조업영향)

  • 허남환;임창희
    • Resources Recycling
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    • v.7 no.2
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    • pp.16-22
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    • 1998
  • Recently, the new technology for the recycling of waste plastics as an alternative he1 of blast furnace ha been developed. In this shldy, the test of plastics injection into a tuyere af the foundry blast furnace were carried out. The injection rate of plastics far this tcst facility war expressed as follows, ${W}_{s}=0.265\frac{{delta}PA}{U}_{g}$, where. Ws, AP, A and Ug are plastic conveying ratc (kgisec), pressure drop between feed hopper and blaqt pressure (alm), cross sectional area of conveying pipe (mi) and superficial velocity of transport air (mhzc) respcctiuely. From the results of semi-continuous test operation during 96 hours, the replacement raho mned out to be 1.38 according to the injection rate of 6. 4 kg-plasticsit-p. With increasing the rate of plaslics injcchon, the content of hydrogen in top gas became increased and the brick temperahlre at bzlly was also increased due to Lhe changes ot the combustion zone shape.

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Ignition of Fuel-rich Propellant Coated with Ignition Support Material in the Ramjet Combustor Condition (램젯 연소실 조건에서 점화보조제가 도포된 Fuel-rich 추진제의 점화)

  • Jung, Woosuk;Baek, Seungkwan;Kim, Youngil;Kwon, Taesoo;Park, Juhyun;Kwon, Sejin
    • Journal of the Korean Society of Propulsion Engineers
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    • v.21 no.4
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    • pp.79-88
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    • 2017
  • Ignition test of the fuel-rich propellant coated with ignition support material in the ramjet combustor condition was conducted. Ignition delay and flame holding was measured. Fuel grain consist of HTPB mixed with AP particle 15 wt.%, Al particle 5 wt.%. To cause the short ignition delay, ignition support consist of $NC/BKNO_3$ and composite propellant was coated to the fuel grain. Ethanol blended $H_2O_2$ gas generator control the temperature, pressure, $O_2$ concentration in the oxidizer gas in the air. Gas is supplied with mass flux of $200kg/m^2s$. Through the test ignition support operated well and ignition delay of 0.6 second and the Flame was sustained.