• Title/Summary/Keyword: 연료비

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A Study on the RDF fuel mixing with household and organic wastes (생활(生活)쓰레기 및 유기성폐기물(有機性廢棄物) 혼합(混合)에 따른 RDF 연료화(燃料化)에 관한 연구(硏究))

  • Ha, Sang-An;You, Mi-Young;Kim, Dong-Kyun;Wang, Jei-Pil
    • Resources Recycling
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    • v.20 no.5
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    • pp.52-57
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    • 2011
  • This study was conducted to examine the possibilities to utilize the mixture of domestic and organic wastes from B-city as a fuel. All types of mixing ratio for uncarried waste, sludge cake, and food waste were found 10 generate heating value with 6,000 kcal/kg, and in case of sludge cake the concentration of toxic substance produced was found to be decreased as air-fuel ratio and temperature were increased. It was noted that toxic gases such as CO, NOx, and SOx were observed below concentration of emission standard, and temperature inside the incinerator was stabilized at 2 of air-fuel ratio and 800$^{\circ}C$. It was observed that a heating value of 6000 kcal/kg generated using RDF(Refuse Derived Fuel) was appropriate to utilize a fuel if a complete combustion was attained.

Response Characteristics of the HIL System for Passenger Diesel Engine (승용 디젤엔진 HIL 시스템의 응답 특성)

  • Chung, Jin-Eun;Roh, Ho-Jong
    • Journal of the Korea Academia-Industrial cooperation Society
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    • v.12 no.11
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    • pp.4745-4750
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    • 2011
  • A HIL(hardware-in-the-loop) system was established and the simulation was carried out to determine whether the system operates normally. The system consists of turbocharger test bench, HIL platform with real time S/W and DAQ, and engine model using Matlab/Simulink. In the simulation the supplied fuel rate is changed step-by-step from 1.8944 kg/h to 4.7360 kg/h. The change of air-fuel ratio is analyzed and observed whether the air-fuel ratio follow the target air-fuel ratio 32. When the supplied fuel rate is changed, the air-fuel ratio is converged to the target air-fuel ratio after about 20 seconds. And the vane duty ratio of turbine and the boost pressure of compressor are also changed properly. Therefore this HIL system can be used to develop the new turbocharger and improve the performance of the modified turbocharger.

Simulation of governing equations for direct methanol fuel cell(DMFC) using FEMLAB (FEMLAB를 이용한 직접메탄올 연료전지(DMFC) 지배방정식의 전산모사)

  • Park, Tae-Hyeon;Kim, In-Ho
    • Clean Technology
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    • v.10 no.1
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    • pp.9-17
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    • 2004
  • Direct methanol fuel cell(DMFC) with proton exchange membrane (PEM) has advantages over the conventional power source (e.g. vehicle). DMFC, however, has a problem to be solved such as methanol crossover, high anodic overpotential and limiting current density, etc. The physicochemical phenomena in DMFC can be described by coupled PDEs (partial differential equations), which can be solved by a PDE solver. In this paper, we utilized a commercial software FEMLAB to solve the PDEs. The FEMLAB is one of the software programs available which are developed as a solver for building physics problems based on PDEs and is designed to simulate systems of coupled PDEs which may be 1D, 2D, 3D, non-liner and time dependent. We performed simulation using the Tafel equation as an electrochemical reaction model to analyze methanol concentration profile in DMFC system. We confirm that the rapid decrease of methanol concentration at anodic catalyst layer with the increase of the current density is a main reason of the low performance in DMFC through simulation results.

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Effects of Partial Premixing on Flame Structure and NOx Emission Characteristics in an Unstable Gas Turbine Combustor (불안정 가스 터빈 연소기에서 부분 예혼합이 화염구조와 NOx 배출 특성에 미치는 영향)

  • Lee Jae-Ho;Lee Jong-Ho;Kim See-Hyun;Chang Young-June;Jeon Chung-Hwan
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2005.11a
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    • pp.437-444
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    • 2005
  • Experiments were carried out in an atmospheric pressure, lab-scale gas turbine combustor to see the effect of partial premixing on unstable flame structure and Nox emission characteristics. The swirl angle is 45 deg., fuel-air mixing degrees were varied 0, 50 and 100% respectively at equivalence ratio ranging from 0.53 to 0.79. The evolution of phased-locked OH chemiluminescence images were acquired with an ICCD. NOx emission characteristics were also investigated at each experimental condition. The effect of the fuel-air mixing degree on the flame structure was obtained from phase-locked $OH^*$ images. And it was obtained from local heat release characteristics that the information about the region which the combustion instability was amplified or damped. It also could be confirmed that $\sigma$ has greatly influence on NOx emission characteristics at lean regimes. It would be expected that it could provide invaluable data for understanding the mechanism of combustion instability.

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High Efficiency Power Conversion System of Non Isolated Type Applied in Fuel Cell Generator Used to Fire Prevention Installation (소방 방재설비용 연료전지 발전시스템의 비절연형 고효율 전력변환기 설계)

  • Kwak, Dong-Kurl
    • Journal of the Microelectronics and Packaging Society
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    • v.13 no.3 s.40
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    • pp.19-26
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    • 2006
  • In this paper, author proposes to a fuel cell generation system used to fire prevention installation at emergency. The proposed system is used with a power source of fire prevention installation in preparation for breaking of commercial power supply at emergency. A part of most power loss of the fuel cell generation system is power converter. And the major losses of power converter are switching losses of power semiconductor switches used to power conversion. This parer is designed with a high efficiency power converter of non isolated type in order to increase efficiency of fuel cell power system. The controlling switches used in power conversion system are operated with soft switching, which is applied to partial resonant method to reduce switching loss. The result is that the fuel cell power system gets to high efficiency. Some computer simulated results and experimental results are confirmed to the validity of the analytical results.

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Numerical Study on Pilot Ratio Effect of Shale-Gas in a Commercial Gas Turbine (상용급 가스터빈에서 셰일가스 파일럿비 영향에 관한 수치해석적 연구)

  • Seo, Dong Kyun;Joo, Yong-Jin;Park, Seik;Kim, Mi-yoeng;Shin, Jugon
    • KEPCO Journal on Electric Power and Energy
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    • v.5 no.3
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    • pp.189-195
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    • 2019
  • In this work, the flow and combustion characteristics using a 3-D numerical simulation was evaluated for a shale gas fueled combustor in a commercial class gas turbine. The Standard k-e turbulence model, 2 step methane oxidation mechanism, Finite rate/Eddy dissipation reaction model, DTRM radiation model were employed and validated well at the baseline condition (Natural Gas, Pilot Ratio 0.2). Based on the validated models, the combustion characteristics of shale gas was evaluated for three pilot ratios cases. It was found that NOx concentrations for all shale gas cases were less than the that for city gas, which imply that, at the selected PRs, the condition for combustion stability is satisfied. In addition, for higher PR, whereas the average temperatures at the exit are the same, the NOx increases. It means that diffusion combustion portion increases due to the higher PR.

Fuel Droplet Entrainment and Low Frequency Instability in Hybrid Rocket Combustion (하이브리드 로켓 연소에서 연료액적의 발생과 저주파수 연소불안정)

  • Kim, Jina;Lee, Changjin
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.49 no.7
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    • pp.573-580
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    • 2021
  • Paraffin wax is attracting many attentions for promising solid fuel of hybrid rocket because of its higher regression than other fuels. However, even with paraffin fuel combustion, unsteady low-frequency oscillation of combustion pressure is still observed. And, this is related to the formation of liquid layer and the entrainment of fuel droplets entering the axial combustion gas flow. This study investigates the effect of additional combustion of fuel droplets on the occurrence of low-frequency combustion instability. On the other hand, the formation of fuel droplets depends on Weber Number (the ratio of the inertial force to the surface tension of the liquid) and Reynolds Number of the oxidizer flow. Therefore, a laboratory-scale hybrid rocket was used to monitor the occurrence of combustion instability while changing We number. A series of combustion tests were conducted to control We number by changing the oxidizer flow rate or adding LDPE (low density polyethylene) to base fuel. In the results, it was confirmed that there is a critical We number above which the low-frequency combustion instability occurs.

An Experimental Study on the Spray Characteristics of a Rotating Fuel Nozzle of a Slinger Combustor for Different Flow Rates and Rotating Speeds (슬링거 연소기 회전연료노즐의 유량과 회전수에 따른 분무특성에 대한 실험적 연구)

  • Shim, Hyeon-Seok;Bae, Jonggeun;Kim, Jupyoung;Kim, Shaun;Kim, Donghyun;Ryu, Gyongwon
    • Journal of the Korean Society of Propulsion Engineers
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    • v.25 no.4
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    • pp.59-70
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    • 2021
  • An experimental study was conducted to observe the spray characteristics for different flow rates and rotating speeds of a rotating fuel nozzle of a slinger combustor. The water spray ejected from the nozzle orifice was visualized using a high-speed camera and a light source. It was confirmed that the atomization was improved, as the flow rate decreased and rotating speed increased. The characteristic maps for the spray characteristics and performance parameters showed that the aerodynamic Weber number and the liquid-air momentum flux ratio were associated with the liquid primary breakup, and the liquid-air momentum flux ratio and Rossby number were closely correlated with the liquid ejection mode.

Numerical Simulation of Transient Laminar Reacting Flows Around Fuel Droplets (연료액적 주변의 비정상 층류 화염장 해석)

  • You S. W.;Kang S. M.;Kim Y. M.
    • Journal of computational fluids engineering
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    • v.6 no.1
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    • pp.47-55
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    • 2001
  • The transient laminar reacting flows around fuel droplet have been numerically analyzed. The physical models used in this study can account for the variable thermophysical properties and the chemistry is represent by the one-step global reaction model. The present study is focused on the vaporization and ignition characteristics, flame structure including wake flame, transition flame and envelope flame, and interaction between droplets. Special emphasis is given to the triple flame structure and flame stabilization.

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Construction of Map for Transient Condition of a Sl Engine and Refinement of Intake Air Model & Fuel Model (가솔린 엔진의 비정상 상태에 대한 Map 구성과 공기 및 연료 모델 개선)

  • 심연섭;강태성;강승표;고상근
    • Transactions of the Korean Society of Automotive Engineers
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    • v.10 no.5
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    • pp.1-8
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    • 2002
  • For gasoline engines, a three-way catalytic converter that has the maximum efficiency at stoichiometric air/fuel ratio is used to clean up the exhaust gas. So a precise air/fuel ratio control is necessary to maximize the catalytic conversion efficiency, For a transient condition, a fred-forward air/fuel ratio control method that estimates the air mass inducted into a cylinder is being used. In this study, a fuel injection map that makes an accurate air/fuel ratio control possible was constructed for the very same transient condition. For the same condition above, intake air model and fuel model were refined so that fuel injection values based on air mass through a throttle valve and intake manifold pressure are equal to the map values.