• Transactions of the Korean Society of Mechanical Engineers B
• /
• v.35 no.9
• /
• pp.975-979
• /
• 2011

Lean premixed gas turbine combustors were successful in meeting current NOx emission regulations. However, these combustors have been found to be susceptible to combustion instability. In this study, general mechanisms for combustion dynamics and instabilities in lean premixed gas turbine combustors are introduced. In addition, the flame transfer functions in the combustor are experimentally determined. The inputs to the flame transfer function are the imposed velocity fluctuations of the mixture. The key results of the measurements are reviewed.

• Journal of the Korea Academia-Industrial cooperation Society
• /
• v.15 no.6
• /
• pp.3370-3375
• /
• 2014

MILD combustion is a highly favored technology for solving the trade-off relation between high thermal efficiency and low pollutant emissions. The system has low NOx concentration in high temperature combustion by recirculating the combustion gas, as well as improving the thermal efficiency by making the internal temperature in a combustion furnace uniform. This study describes the combustion characteristics of a conical MILD combustor in a laboratory-scale furnace by adjusting the equivalence ratio with the fuel gas flow rate while maintaining a constant air flow rate of the furnace. The MILD regime in the furnace is well characterized and the in-furnace temperature and emissions were predicted, respectively, for the range of equivalence of 0.69 - 0.83. For the range of equivalence ratios, this study confirmed the existence of a stable flame region that has an approximately $300^{\circ}C$ temperature difference between the maximum flame temperature region and main reaction region.

• Proceedings of the Korea Water Resources Association Conference
• /
• 2020.06a
• /
• pp.198-198
• /
• 2020

기후 내적 변동성(Climate Internal Variability, CIV)은 기후를 이해하는 데 중요한 역할을 하며 기후예측에 있어 주요 불확실성 원인들 중 하나이다. 본 연구는 다양한 이산화탄소 배출 시나리오에 대해 CIV와 기후학적 평균(Climatological Mean, CM)을 추정하는 것을 목표로 한다. 확률론적 날씨생성기(Stochastic Weather Generator)를 이용하여 국내 40개 기상 관측소에 대해, 30년에 해당하는 시단위 시계열 100개 앙상블을 생성하였다. CIV는 Detrend 방법과 Differenced 방법을 이용하여 추정되었으며, noise 계산값과 비교하였다. 그 결과, CIV 값과 noise 값들 사이의 correlation이 매우 높았으며, 제시된 방법론이 신뢰할 수 있음을 검증하였다. 국내 40개 지역에 적용하여 계산된 CIV와 CM의 주요 결과는 다음과 같다. (1) 국내의 대부분의 지역에 있어 평균적으로 CM과 CIV는 미래에 증가할 것이며, 그 증가 정도는 RCP 8.5의 경우와 먼 미래END(2071-2100년) 기간에서 더 커질 것이다; (2) CM과 CIV의 미래 변화의 특성은 강수의 특성 지수에 따라 다르다. 강수량의 양을 나타내는 3개의 지수(총 강수량, totPr, 일 최대 강수량, maxDa 및 시간당 최대 강수량, maxHr)와 강수량의 발생일수를 나타내는 지수(무강우 일수, nonPr)의 특성은 크게 다르다. (3) CIV와 CM의 변화 요인들 사이의 관계를 조사하면 maxDa와 maxHr에 대해서는 그들 사이에 높은 상관관계가 있지만 다른 지수에는 그렇지 않다. (4) 국내에서 CIV 값이 공간적으로 변동성이 큰 경우는 계절적으로 여름이며, 이는 totPr 및 maxDa에서만 유효하다. 시단위 시계열 앙상블을 생성하여 추정된 기후내적변동성 정보는 기후 변화의 영향을 평가하고 적절한 적응 및 대응 전략을 개발하는 데 도움이 될 것이다.

• Journal of Soil and Groundwater Environment
• /
• v.13 no.4
• /
• pp.62-68
• /
• 2008

The Low Temperature Thermal Desorption (LTTD) System equipped with a soil transfer unit, a rotary kiln, RTO, cyclones and a bag filter etc. was developed. The LTTD system was designed to be economically operated using LPG as a fuel and recirculating the discharged gas from the LTTD system through RTO. For the performance test of LTTD system the soil contaminated with light and heavy oils (2,690 mg TPH/kg soil) and with particle sizes below 50 mm was fed into the rotary kiln of LTTD system at 7$m^3$/hr with retention time of 15 minutes. Operation temperatures of LTTD system for the removal of soil TPH were $567^{\circ}C$ and $692^{\circ}C$. The residual TPH after treatment was 46 mg/kg and 32mg/kg respectively at each temperature condition, which shows high TPH removal efficiencies of the developed LTTD as 98.3% and 98.9%.

• Proceedings of the Korean Society of Propulsion Engineers Conference
• /
• 2011.11a
• /
• pp.981-984
• /
• 2011

A high-resolution numerical study is carried out to investigate the transient process of the combustion and the shock-train developments in an ethylene-fueled direct-connect dual-mode scramjet combustor. Following the fuel injection, air-throttling is applied at the expansion part of the combustor to provide mass addition to block the flow to subsonic speed. The ignition occurs several ms later when the fuel and air are mixed sufficiently. The pressure build up by the combustion leads to the shock train formation in the isolator section that advances to the exit of the intake nozzle. Then, the air-throttling is deactivated and the exhaust process begins and the situation before the air-throttling is restored. Present simulation shows the detailed processes in the dual-mode scramjet combustor for better understanding of the operation regimes and characteristics.

• Journal of the Korea Organic Resources Recycling Association
• /
• v.11 no.4
• /
• pp.79-89
• /
• 2003

The purpose of this study is to investigate appropriate environmental factors when domestic waste is decomposed as aerobic digestion. So stabilization degree was measured after the waste is mixed as certain rates and water content was controlled by 55% and 60%. Variation of VS showed food waste in reactors of number 1, 2, 3, 4 and 5 was decomposed fully except reactor of number 6. Decomposition degree of VS in reactors of number 1, 2, 3 and 4 was not different high because Vinyl and plastic inserted played role bulking agent in reactor number 1, 2, 3 and 4. In reactors, maximum temperature indicated $57{\sim}59^{\circ}C$ and temperatures in reactors 1, 2, 3 and 4 were higher and remained longer than in reactor 5 and 6 for 2~4 days. Variation of $CO_2$ was similar to that of VS. The reduction rate of water content was low because moisture generated by oxidation fever of microorganism did not evaporated well. pH was low in the beginning of the reaction however, as time passed, it increased slightly and remained regular pattern. EC and C/N showed the same pattern as pH. Settlement and weight reduction rates were similar to the factors above. Reactor 1, 2, 3, and 4 showed higher settlement and weight reduction rate than reactor 5 and 6.

• Transactions of the Korean Society of Mechanical Engineers B
• /
• v.33 no.9
• /
• pp.658-665
• /
• 2009

Lean premixed combustors are used for significant NOx reduction which one of issues in current gas turbine combustor. This study was investigated to estimate the effects of the unmixedness of fuel-air, equivalence ratio on the instability mechanism, NOx emission and combustion oscillation in a lean premixed combustor. The experiments were conducted in a dump combustor at atmospheric pressure conditions using methane as fuel. The swirler angle was $45^{\circ}$, the degrees of fuel-air mixing were 0, 50 and 100 and inlet temperature was 650K. The equivalence ratio was ranging from 0.5 to 0.8. This paper shows that NOx emission was increased when the degree of fuel-air mixing is increased in same equivalence ratio and when equivalence ratio is increased. And the range of the combustion instability was enlarged as a function of increasing of the degree of fuel-air mixing.

• Journal of the Korean Society for Aeronautical & Space Sciences
• /
• v.45 no.4
• /
• pp.300-309
• /
• 2017

A spacecraft obtains a reaction momentum required for an orbit correction and an attitude control by exhausting a combustion gas through a small thruster in space. If the exhaust plume collides with spacecraft surfaces, it is very important to predict the exhaust plume behavior of the thruster when designing a satellite, because a generated disturbance force/torque, a heat load and a surface contamination can yield a life shortening and a reduction of the spacecraft function. The purpose of the present study is to ensure the core technology required for the spacecraft design by analyzing numerically the exhaust gas behavior of the 10 N class bipropellant thruster for an attitude control of the spacecraft. To do this, calculation results of chemical equilibrium reaction between a MMH for fuel and a NTO for oxidizer, and continuum region of the nozzle inside are implemented as inlet conditions of the DSMC method for the exhaust plume analysis. From these results, it is possible to predict a nonequilibrium expansion such as a species separation and a backflow in the vicinity of the bipropellant thruster nozzle.

• Applied Chemistry for Engineering
• /
• v.34 no.3
• /
• pp.307-312
• /
• 2023

In this study, a catalytic oxidation-heat recovery system was designed that can remove unreacted with a concentration of about 1% to 6% in the exhaust gas of hydrogen fuel cells and recover heat to ensure safety in the hydrogen economy. The safety system was devised by filling hydrogen oxidation catalysts at room temperature that can remove unreacted hydrogen without any energy source, and an exhaust-heat recovery device was integrated to efficiently recover the heat released from the oxidation reaction. Through CFD analysis, variations in pressure and fluid within the system were shown depending on the filling conditions of the hydrogen oxidation system. In addition, it was found that waste heat could be recovered by optimizing the temperature of the exhaust gas, flow rate, and pressure conditions within the heat recovery system and securing hot water above 40 ℃ by utilizing the exhaust gas oxidation heat source above 300 ℃. Through this study, it was possible to confirm the potential of utilizing hydrogen processes, which are applied in small to medium-sized systems such as hydrogen fuel cells, as a safety system by evaluating them at a pilot scale. Additionally, it could be a safety guideline for responding to unexpected hydrogen safety accidents through further pilot-scale studies.

• Journal of the Korean Applied Science and Technology
• /
• v.34 no.4
• /
• pp.892-898
• /
• 2017

In this study, the basic properties of recoverable gaseous and solid materials were investigated from heavy oil contained in the resources. The basic characteristics of pyrolysis reaction for the conversion of bituminous oil to pyrolysis various temperature were investigated. The characteristics of gas and solid phase byproducts were also investigated with a laboratory scale fixed bed reactor according to various reaction temperature. As a result, it was confirmed that the oil yield was about 17% at $550^{\circ}C$ and $CH_4$, $CaCO_3$ and CaO could be recovered as by-products.