• Title/Summary/Keyword: 연소 가스

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Effect of Properties of Fly-ashes on the Characteristics of Fly-ash Mortars (플라이애시 종류에 따른 플라이애시 모르타르의 특성에 대한 연구)

  • Kim, Joo-Hyung;Park, Byoung-Sun;Jung, Sang-Hwa;Choi, Young-Cheol
    • Journal of the Korean Recycled Construction Resources Institute
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    • v.4 no.4
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    • pp.439-445
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    • 2016
  • Recently, a large number of researches about concrete containing high volume fly-ash(HVFA) have been carried to obtain carbon dioxide reduction, resource recycle and durable option in concrete industry. The quality of fly-ash such as chemical composition and fineness has high variability due to the differences of used fuels, operation condition in power plant. The aim of this study is to investigate the performances of fly-ash cement mortar containing different type of fly-ashes. The basic analysis of fly ash such as chemical composition, SEM image analysis were performed. Many mortar specimens were fabricated to evaluate the properties (compressive strength, drying shrinkage and carbonation) of mortar with various fly ash. From the test results, the quality of each fly ash must be considered and fully weighted in fly ash concrete.

An Economic Feasibility Study on Fuel Transfer of A Thermal Power Plant Considering CO2 Emission Cost (CO2 배출비용을 고려한 발전소의 연료교체 경제성에 대한 연구)

  • Lee, Sang-Joong;Jeong, Yeong-Ho
    • Journal of the Korean Institute of Illuminating and Electrical Installation Engineers
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    • v.23 no.2
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    • pp.125-130
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    • 2009
  • With respect to the goal of achieving at least 50[%] reduction of global emissions by 2050, the G8 leaders agreed to seek to share and adopt it with all Parties to the UNFCCC in the 34th Group of Eight Summit held in Toyako, Japan in July 2008. Korea is also expected to obey the Kyoto Protocol starting in 2013, which will result in a serious shock especially to the electric power industry. The power plants burning the fossil fuel produce more than 20 percent of national $CO_2$ emission. This paper presents an economic feasibility study on fuel transfer for a thermal power plant considering $CO_2$ emission cost. Calculation of the breakeven point for the fuel transfer from LNG to heavy oil of D power plant is demonstrated using the input-output coefficients obtained by the performance test.

Properties of Cement Mortar According to Substitution Ratio of High Calcium Fly Ash Based on Blast Furnace Slag (고로슬래그 기반 고칼슘 플라이애시 치환비율에 따른 시멘트 모르타르의 특성)

  • Cho, Seong-Woo;Mun, Kyung-Ju;Hyung, Won-Gil
    • Journal of the Korea Institute of Building Construction
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    • v.20 no.1
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    • pp.27-34
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    • 2020
  • In the industry, due to the carbon dioxide gas produced during cement production is increasing, research on recycling by-products has been actively conducted. In the industrial by-products, the high calcium fly ash(HCFA) produced by the blast-furnace in the circulating fluidized bed combustion method has a high ratio of CaO and CaSO4. In view of this, the purpose of this is to use high calcium fly ash(HCFA) as a stimulant in blast furnace slag powder and use it as a cement substitute. As a result, it is judged that the substitution ratio of HCFA should be 15% or less. In addition, although durability and strength are relatively lower than of OPC, it is considered that it can be utilized as an environmentally building material.

Research Activities of Transpiration Cooling for Liquid Rocket and Air-breathing Propulsions (액체로켓과 공기흡입식 추진기관을 위한 분출냉각의 연구동향)

  • Hwang, Ki-Young;Kim, You-Il;Song, In-Hyuck
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2010.11a
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    • pp.235-240
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    • 2010
  • Transpiration cooling is the most effective cooling technique for liquid rocket and air-breathing engines operating in aggressive environments with higher pressures and temperatures. Combustor liners and turbine vanes are cooled by the coolant(air or fuel) passing through their porous walls and also the exit coolant acting as an insulating film. However, its practical implementation has been hampered by the limitations of available porous materials. The search for more practical methods of increasing the internal heat transfer within the walls has led to the development of multi-laminate porous structures, such as Lamilloy$^{(R)}$ and Transply$^{(R)}$. This paper reviews recent research activities of transpiration cooling for the propulsions of liquid rocket, gas turbine, and scramjet.

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Influences of the Surface Pollution Cause by the Marine Growth on Ship Hulls on Engine Performance and Output (선체 해양생물의 선저오염이 엔진성능과 출력에 미치는 영향)

  • Jung, Kyun-Sik
    • Journal of Advanced Marine Engineering and Technology
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    • v.39 no.4
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    • pp.399-404
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    • 2015
  • The cost of fuel in ships has recently increased due to a rapid increase in international oil prices and international restrictions regarding the greenhouse effect generated from the burning of fuel. Therefore, different methods for changing the hull designs for improving energy efficiency, developing coating for reducing friction resistances, developing additives for improving engine thermal efficiency, and low-speed operation for reducing fuel consumption have been considered. The developments of high-speed, large-scale, and energy-saving vessels are deemed essential to adapt to the recent high oil price era. Therefore, it is important to analyze Precisely the qualitative and quantitative changes in the resistance value of the local areas of the hull surface. In this study, the engine performance before and after docking was analyzed to examine friction resistance caused by marine growth on the hull as a basic study for improving the energy efficiency. The result was then presented by comparing it with the previous data for 2.5 years between docks to investigate the performance of the main engine, the change in friction resistances and loads, the fuel consumption and ship speed.

Premixed Combustion of the Mixture of Anode-off Gas from Reformer and LNG (개질기용 Anode off gas와 LNG의 예혼합 연소특성)

  • Lee, Jae-Young;Lee, Pil-Hyong;Han, Sang-Seok;Park, Chang-Soo;Hwang, Sang-Soon
    • Proceedings of the KSME Conference
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    • 2008.11b
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    • pp.2198-2203
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    • 2008
  • Hydrogen which can be produced through reforming process of hydrocarbon fuel is supplied into anode side of fuel cell system. In the fuel cell, only 70% of hydrogen is consumed through electrochemical reaction and 30% hydrogen passed by as anode off gas. When electrical output of fuel cell is within range of 1.0 to 3.0kW, burner for the reformer uses only anode off gas. And it uses mixture gas of anode off gas and LNG within range of 3.5 to 5.0kW in electrical output. CHEMKIN 4.1 program's Premixed code was used for calculating the properties of each gas. Results show that burning velocity and adiabatic flame temperature are 34.4cm/s, 1681.7K at equivalence ratio 0.8 within range of 1.0kW to 3.0kW and for cases of 3.5kW, 5.0kW, of electrical output, burning velocity and adiabatic flame temperature represent 30.5, 29.8cm/s and 1722.8, 1750K respectively. CO shows the lowest emission index at equivalence ratio 0.8 and NOx reveals the highest emission index at equivalence ratio 1.

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The Study on the Synthesis of Triazole Derivatives as Energetic Plasticizer (트리아졸 계열의 에너지 가소제 합성 연구)

  • Lee, Woonghee;Kim, Minjun;Park, Youngchul
    • Journal of the Korean Society of Propulsion Engineers
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    • v.20 no.2
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    • pp.31-38
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    • 2016
  • Most of propellants that is used widely in the world release toxic gases such as methane gas and carbon dioxide during combustion which are noxious to the environment. This study established a synthetic process of a high nitrogen containing derivative of triazole, 4,5-bis(azidomethyl)-methyl-1,2,3-triazole (DAMTR), which can be applied as energetic plasticizer to environmental concerns. Also, the compound was characterized by NMR, IR spectroscopy, and physical properties such as glass transition temperature, melting point, decomposition temperature, density, impact sensitivity, viscosity and volatility were measured. In addition, the heats of formation (${\Delta}H_f$) and detonation properties (pressure and velocity) of DAMTR were calculated using Gaussian 09 and EXPLO5 programs.

Internal Flow Characteristics of Simulated Dual Pulse Rocket Motor by Using the Hot Gas and Cold Gas (Hot Gas와 Cold Gas를 이용한 모사 이중펄스 로켓 추진기관의 내부 유동 특성)

  • Cho, Kihong;Park, Jungho;Kim, Euiyong
    • Journal of the Korean Society of Propulsion Engineers
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    • v.19 no.2
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    • pp.1-8
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    • 2015
  • Dual pulse rocket motor is a variant of solid rocket motor with two propellant grain separated by a pulse separation device. The major performance of such a rocket motor is influenced by the change in the hole area of pulse separation device to nozzle throat area ratio. In this study, we performed flow analysis to investigate the internal flow characteristics according to the pulse separation device hole area to nozzle throat area ratio change. Gases used flow analysis were used combustion gas of HTPB/AP composite propellant and nitrogen gas. Flow analysis results of the dual pulse rocket motor were validated by comparison with experimental results of pneumatics. Commercial CFD code ANSYS FLUENT 14.5 is used in this study to simulate flow analysis.

A Computational Study on Cooling Analysis of the Flame Deflector for the 75 tonf Class Propulsion Test Facility (75톤급 추진기관 시험설비 화염유도로 냉각해석에 관한 수치적 연구)

  • Moon, Seong-Mok;Cho, Nam-Kyung;Kim, Seong-Lyong;Jun, Sung-Bok;Lee, Kyoung-Hoon;Kim, Dong-Hwan
    • Journal of the Korean Society of Propulsion Engineers
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    • v.19 no.2
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    • pp.55-64
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    • 2015
  • In this study, a 3-D flame cooling analysis is conducted to examine thermal safety for the flame deflector of the 75 tonf class propulsion test facility, and the safe discharge of the exhaust gas is assessed by using numerical results. The Mixture multiphase model is adopted for the simulation of heat transfer and phase exchange process between flame and cooling water, and the computational study using the single species unreacted model for the exhaust plume is carried out for the flame cooling. Numerical analysis predicts maximum temperature on the flame deflector wall for different water flow rates, and evaluates the safe minimum flow rate of water corresponding to the fire-resistant temperature for concrete.

A Study on Toxicity Bio-markers of a Mouse using Combustion Gas SO2 generated from Fire (마우스(mouse)를 이용한 건축물 마감재료 연소가스 SO2의 독성생체지표 연구)

  • Rie, Dong-Ho;Cho, Nam-Wook;Choi, Soon-Young
    • Journal of the Korea Safety Management & Science
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    • v.14 no.1
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    • pp.43-51
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    • 2012
  • This study was carried out to observe the impacts of a mouse's inhalation of toxic gas SO2 generated from combustion on its organs by different concentrations. As for research methods: First, after concentrations of SO2 generation from combustion had been set to three: low (10.4 ppm), middle (24.9 ppm) and high (122 ppm) through Gas Toxicity Testing Method (KS F 2271) and SO2 combustion gas was exposed to eight mice in each concentration. Five mice that were able to move based on LD50, a criterion, which sets the down time of a mouse's average behaviors to over 9 minutes, were randomly selected in each concentration, and they were set up as the subjects of the study on toxicity bio-markers. Second, tissues were taken from heart, liver, lungs, spleen and the thymus gland of the mice selected in each concentration and a pathological examination of them was carried out. As a result, microvascular congestion appeared in the heart, and cell necrosis, cortex congestion and tubule medulla congestion, etc. in each concentration were observed in addition to vascular congestion in liver, lungs, spleen and the thymus gland. Also, it was found that the higher the concentrations of SO2 exposure is, the greater, the changes in the organs get. Through this study, SO2 of various toxic gases generated from fire turned out to affect the tissues of each organ of a mouse, it is expected that the toxic gases may greatly affect human body in case of actual fire, and this study is evaluated as having a significance as a basic data on inhalation toxicity assessment of toxic substances generated in combustion.