• Title/Summary/Keyword: 배기가스 감소

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기미부 형상과 엔진화염에 의한 유도탄의 항력 영향 수치해석

  • 정석영;안창수
    • 한국전산유체공학회:학술대회논문집
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    • 2002.10a
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    • pp.23-27
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    • 2002
  • 천음속으로 비행하는 공기흡입유도탄의 경우, 비행거리 및 요구기동을 충족시키기 위해서는 추진제트에 의해 변화하는 기체 기미부의 압력항력을 정확히 예측하고 이 항력을 감소시키기 위한 기미부 형상설계는 매우 중요하며 필수적이다. 제트 Plume에 의한 기체 기미부 및 base의 압력분포에 따른 항력해석을 난류모델링을 고려한 수치해석 결과를 제시한다. Jet plume의 크기 및 배기가스 조건에 따른 항력변화, 및 기미부 형상에 따른 항력변화 그리고 천음속 마하수에 따른 결과 등을 제시한다.

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A Study on the Development of $CO_2$ Recycle Oxy-Fuel Combustion Heating System ($CO_2$ 재순환형 산소연소 가열시스템 개발에 관한 연구)

  • Jeong Yu-Seok;Lee Eun-Kyung;Go Chang-Bok;Jang Byung-Lok;Han Hyung-Kee;Noh Dong-Soon
    • Proceedings of the Korea Society for Energy Engineering kosee Conference
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    • 2006.05a
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    • pp.412-419
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    • 2006
  • An Experimental study was conducted on $CO_{2}$ recycle combustion heating system using pure oxygen instead of conventional air as an oxidant, which is thereby producing a flue gas of mostly $CO_{2}$ and water vapor($H_{2}O$ and water vapor($H_{2}O$) and resulting in higher $CO_{2}$ concentration. The advantages of the system are not only the ability to control high temperatures characteristic of oxygen combustion with recycling $CO_{2}$ but also the possibility to reduce NOx emission in the flue gas. A small scale industrial reheating furnace simulator and specially designed variable flame burner were used to characterize the $CO_{2}$ recycle oxy-fuel combustion, such as the variations of furnace pressure, temperature and composition in the flue gas during recycle. It was found that $CO_{2}$ concentration in the flue gas was about 80% without $CO_{2}$recycle. The furnace temperature and pressure and pressure were decreased due to recycle and the NOx emission was also reduced to maintain under 100ppm.

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Emission Evaluation of Emulsion Fuel Prepared from Bunker C Oil (벙커 C유를 사용한 에멀젼 연료유의 배기가스 특성)

  • Lim, HeungKyoon;Lee, MyungJin;Chi, Gyeong-Yup;Lim, JongChoo
    • Applied Chemistry for Engineering
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    • v.28 no.2
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    • pp.186-192
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    • 2017
  • In this study, water in oil (W/O) emulsion fuel was prepared with surfactant mixture of OIMS90 and NP12 by varying ratio of water to bunker-C oil, surfactant concentration and composition, emulsification time, stirring intensity, temperature and mixing time. Diesel engine performance and exhaust emissions were measured and analyzed with prepared emulsified fuel and compared with those measured using bunker Coil. The results indicated that bunker C emulsion fuel stabilized by surfactant mixture of OIMS90 and NP12 is efficient in reducing emissions of particulate matter, $NO_2$, CO, $CO_2$ and $SO_2$. The biggest reduction in exhaust emission was achieved by using emulsion fuel prepared by OIMS90/NP12 = 4 : 6, 500 ppm of total surfactant concentration and 10% water content at $80^{\circ}C$. Boiler efficiency test measured with emulsion fuel showed excellent energy efficiency compared with bunker C oil.

Pressure Recovery in a supersonic ejector of a high altitude testing chamber (초음속 이젝터의 압력회복에 관한 연구)

  • Omollo, Owino George;Kong, Chang-Duk
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2010.11a
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    • pp.833-837
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    • 2010
  • This study aims at finding an optimal exhaust diffuser design of a high altitude testing chamber for a low bypass turbofan engine (F404-402) with thrust pound force of 17,700 and air mass flow rate of 66kg/s ejecting at a speed of Mach 1.66. The final proposed ejector size has better pressure recovery characteristics and targets to reduce operational cost at engine performance testing. Conventional high altitude test chamber layout was adopted and first drawn in two dimensions using Autocad software so as to determine the gas path, the ejector frontal size was then determined from gas dynamics equations considering traditional gas ejection method where both the engine exhaust and cell cooling air are exhausted via the ejector. Modification to a smaller ejector with an alternative secondary cell cooling exhaust port was then performed and modelled in 3D using Solid Works software.

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A Study on Flow Characteristics of a Separate Triangular Bar Differential Pressure Flow Meter for Measuring Exhaust Flow Rate of Diesel Engine (디젤엔진 배기 가스 유량 측정용 삼각 분리 막대형 차압유량계 유량 특성 연구)

  • Lee, Choong-Hoon;Kim, Kwang-Il;Kim, Min-Chang;Park, Dong-Sun
    • Journal of the Korean Society for Railway
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    • v.10 no.5
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    • pp.563-568
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    • 2007
  • A separate triangular bar type differential pressure flow meter was developed for measuring exhaust gas flow rate from Diesel engine. Three kinds of the separate triangular bar flow meters whose aerodynamic angles are different one another are made and evaluated, respectively. The experimental results show that an aerodynamic shape has a effect on the pressure difference between upstream and downstream at the flow meter, that is, the thinner the shape of the separate triangular bar flow meter is, the smaller the pressure difference at the flow meter is. The separate triangular bar type flow meter was calibrated at both cold and high temperature of the gas flow. A burner system was designed for raising the gas temperature and it was well operated in controlling the gas temperature. An empirical correlation between mass flow rate and differential pressure at the separate triangular bar flow meter was obtained and the empirical correlation was also corrected by the gas temperature.

Evaluation of Ventilation Performances for Various Combinations of Inlets and Outlets in a Residential Unit through CO2 Tracer-Gas Concentration Decay Method (CO2 추적가스 농도감소법을 이용한 공동주택의 급·배기구 조합에 따른 환기 성능 분석)

  • Sang Yoon Lee;Soo Man Lee;Jong Yeob Kim;Gil Tae Kim;Byung Chang Kwag
    • Land and Housing Review
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    • v.14 no.4
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    • pp.111-120
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    • 2023
  • Indoor air quality has become increasingly important with the increase in time spent in residential environments, impact of external fine dust, yellow dust, and the post-COVID 19 pandemic. Residential mechanical ventilation plays a key role in addressing indoor air quality. The legal standard for residential air changes per hour in Korea is 0.5 ACH. However, there are no standards for the location of supply and return vents. This study atempts to analyze the impact of ventilation performance based on the location of supply and return vents. An experiment was conducted using the CO2 tracer gas concentration decay method in a mock-up house set inside a large chamber to minimize external influences. The experimental results indicated that the commonly used combination of 2 supply and 2 return vents in living room spaces had a lower mean age of air than the combination of 1 supply and 2 return vents. Using multiple supply and return vents had lower mean age of air than using just 1 supply and 1 return vent.

A study of NOx performance for Cu-chabazite SCR catalysts by Sulfur poisoning and desulfation (Cu-Chabazite SCR Catalysts의 황 피독 및 탈황에 의한 NOx 저감 성능에 관한 연구)

  • Nam, Jeong-Gil
    • Journal of Advanced Marine Engineering and Technology
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    • v.37 no.8
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    • pp.855-861
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    • 2013
  • Small-pore Cu-chabazite SCR catalysts with high NOx conversion at low temperatures are of interest for marine diesel engines with exhaust temperatures in the range of 150 to $300^{\circ}C$. Unfortunately, fuels for marine diesel engines can contain a high level of sulfur of up to 1.5% by volume, which corresponds to a $SO_2$ level of 500 ppm in the exhaust gases for an engine operating with an A/F ratio of 50:1. This high level of $SO_2$ in the exhaust may have detrimental effects on the NOx performance of the Cu-chabazite SCR catalysts. In the present study, a bench-flow reactor is used to investigate the effects of sulfur poisoning on the NOx performance of Cu-chabazite SCR catalysts. The SCR catalysts were exposed to simulated diesel exhaust gas stream consisted of 500 ppm $SO_2$, 5% $CO_2$, 14% $O_2$, 5% $H_2O$ with $N_2$ as the balance gas at 150, 200, 250 and $300^{\circ}C$ for 2 hours at a GHSV of 30,000 $h^{-1}$. After sulfur poisoning the low-temperature NOx performance of the SCR catalyst is evaluated over a temperature range of 150-$300^{\circ}C$ to determine the extent of the catalyst deactivation. Desulfation is also carried out at 600 and $700^{\circ}C$ for 30 minutes to determine whether it is possible to recover the NOx performance of the sulfur-poisoned SCR Catalysts.

A Study on the Flow Uniformity and Characteristics of Exhaust gas in Diesel Particulate Filter/Diesel Oxidation Catalyst of Ship Diesel Reduction System by Computational Fluid Dynamics (CFD에 의한 선박용 DPF/DOC내 배기가스의 유동 균일도 및 특성 연구)

  • Kim, YunJi;Han, Danbee;Baek, Youngsoon
    • Clean Technology
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    • v.25 no.2
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    • pp.153-160
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    • 2019
  • As air pollution becomes more serious due to the increased number of diesel vessel operations, ship regulations on harmful emissions strengthen. Therefore, the development of a diesel exhaust after-treatment system for ships is required, and the higher the flow uniformity of the exhaust treatment system, the higher the treatment efficiency. With the computer software ANSYS Fluent, pressure drop and flow uniformity were used in this study to simulate flow rate with and without a baffle in both a Diesel Oxidation Catalyst (DOC) and Diesel Particulate Filter (DPF) system. The system pressure drop was found to be 38 to 40 mbar in the existing system condition, and the flow uniformity was approximately 84 to 92% at the inlet and outlet of the DOC. When the baffle was installed inside the system, the pressure increased and the flow uniformity was lowered due to an increase in flow rate. When the exhaust gas flow was reduced by 50% from $7,548kg\;h^{-1}$ to $3,772kg\;h^{-1}$, the flow uniformity at the inlet and outlet of the DOC increased by approximately 1 to 3% due to the low flow rate. In the case of DPF, the flow uniformity of exhaust gas was 98 to 99% because the uneven flow proceeded after uniformly flowing from the DOC.

Experimental Study of a Micro Turbo Jet Engine Performance and IR Signal with Nozzle Configuration (배기노즐 형상변화에 따른 마이크로 터보제트 엔진의 성능 및 적외선신호 실험연구)

  • Park, Gyusang;Kim, Sunmi;Choi, Seongman;Myoung, Rho-Shin;Kim, Woncheol
    • Journal of the Korean Society of Propulsion Engineers
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    • v.20 no.5
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    • pp.1-8
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    • 2016
  • Micro turbojet engine test and infrared signal measurement were conducted to understand the characteristics of the engine performance and infrared signal with the variants of the exhaust nozzle configuration. A cone type nozzle and five rectangle type nozzles which has aspect ratio from one to five were used for the experimental work. The results show that there are not much difference between cone and rectangle nozzles of the thrust and specific fuel consumption. However infrared signal from exhaust gas become smaller as increasing aspect ratio.

Effects of Multi-stage Pilot Split Injection Strategy on Combustion and Emission Characteristics in a Single-Cylinder Diesel Engine (단기통 디젤엔진에서 다단 파일럿 분할 분사 전략이 연소 및 배기가스 특성에 미치는 영향)

  • Lee, Hyungmin
    • Journal of the Korea Academia-Industrial cooperation Society
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    • v.21 no.7
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    • pp.692-698
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    • 2020
  • This paper examines the effects of a multi-stage pilot split injection strategy on combustion and exhaust emission factors in a single-cylinder diesel engine. One analysis noted that in the single-injection condition, the maximum in-cylinder pressure and rate of heat release were highest. The pilot injection quantity was evenly divided, showing a tendency to decrease as the number of injections increased. In another injection condition, when the multi-stage pilot split injection strategy was applied, IMEP, engine torque, and combustion increased. The COVIMEP was greatest with the lowest combustion efficiency. The combustion ability was poor. In a single injection condition, the O2 concentration in the exhaust gas was the lowest and the CO2 was the highest. When the multi-stage split injection strategy was applied, the low temperature combustion process proceeded, and the oxidation rate of CO2 decreased while the emission level increased. In a single injection condition in which a locally rich mixture was formed, the HC emission level showed the highest results. A 55.6% reduction of NOx emission occurred under a three-stage pilot injection condition while conducting a multi-stage pilot split injection strategy.