• 한국자동차공학회논문집
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• 제14권6호
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• pp.171-178
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• 2006

The performance in the practical combustion system including reciprocating engines and gas turbine combustors is being much governed by turbulent reacting flow that is often analyzed by both a laminar flamelets concept and flame interaction. The characteristics of laminar flame interaction have been investigated numerically to provide basic understanding of wrinkled turbulent flames under concentration interaction resulting from inhomogeneity in fuel-air mixing, especially focused on the transition of flame characteristics such as diffusion flame, partially premixed diffusion flame, and triple-layer flame by the variation in the degree of premixedness. The extinction stretch rates to the premixedness have also been obtained in this paper. The boundary defining the regime of the existence of triple-layer flames as functions of both stretch rate and premixedness has been determined which agrees well with previously reported experiment measuring OH radical concentration peaks based on PLIF.

• 한국추진공학회지
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• 제11권4호
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• pp.1-9
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• 2007

많은 산업체들은 현재 연소기의 열효율을 증가시키기 위해 노력하고 있으며, 증가되는 NOx 발생으로 환경적인 규제에 직면하고 있다. 우리는 이렇게 열효율 증가와 NOx 발생 감소를 동시에 해결할 수 있도록 새로운 방법을 연구하였다. 이 새로운 개념은 확실히 NOx와 같은 오염물질을 절감시키며, 동시에 반경방향 열전달을 증가시키는 것으로 알려져 있고 이를 세차제트 연소기라고 부른다. 이러한 세차제트 노즐의 특징은 가스터빈의 연소효율의 증가로 이어질 수 있을 것이다. 기본적인 세차제트 노즐에 대한 특설파악을 위해 FLUENT를 이용한 수치해석, 레이저를 이용한 가시화 시험을 진행하였고, 노즐단면에서의 속도분포를 다른 논문의 실험결과와 비교하였다. Centerbody가 있는 경우 세차현상이 잘 일어났고 노즐 출구에서의 확산각이 증가함을 확인하였다.

• 한국추진공학회:학술대회논문집
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• 한국추진공학회 2009년도 제33회 추계학술대회논문집
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• pp.213-216
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• 2009

가스터빈 연소기의 화염 특성을 알기 위하여 분할 연소기 시험을 수행하였다. 점화시험은 여러 가지 연소기 유입 공기속도와 공기과잉율에 따라 토치 점화장치를 이용하여 수행되었다. 또한, 연료를 충분히 공급한 상태에서 점화를 수행한 후 점차 연료량을 감소시켜가며 희박연소한계를 측정 하였다. 실험 결과, 공기과잉율 6에서 안정한 점화를 보였고 이 값은 연소기 공기 유입속도에 따라 점점 증가함을 보였다. 최소 실화한계는 연소기 공기 유입속도 40 m/s에서 약 4였고, 이 값 또한 연소기공기유입속도에 따라 약 10 까지 증가함을 보였다.

• 대한기계학회논문집B
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• 제25권7호
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• pp.905-914
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• 2001

A large eddy simulation(LES) is performed for turbulent flow around a bluff body inside a sudden expansion cylinder chamber, a configuration which resembles a premixed gas turbine combustor. To promote turbulent mixing and to accommodate flame stability, a flame holder is installed inside the combustion chamber. The Smagorinsky model is employed and the calculated Reynolds number is 5,000 based on the bulk velocity and the diameter of the inlet pipe. The simulation code is constructed by using a general coordinate system based on the physical contravariant velocity components. The predicted turbulent statistics are evaluated by comparing them with the laser-doppler velocimetry (LDV) measurement data. The agreement of LES with the experimental data is shown to be satisfactory. Emphasis is placed on the time-dependent evolutions of turbulent vortical structure behind the flame holder. The numerical flow visualizations depict the behavior of large-scale vortices. The turbulent mixing process behind the flame holder is analyzed by visualizing the sectional views of vortical structure.

• 대한금속재료학회지
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• 제49권7호
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• pp.535-540
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• 2011

The tensile and creep behaviors of Alloy 263, which is a wrought Ni-base superalloy used for gas turbine combustion systems, was studied. Anomalous increase of yield strength and abrupt decrease of elongation with increasing temperature were observed after tensile testing at an intermediate temperature. Elongation of the superalloy decreased as the temperature increased to and above 540$^{\circ}C$, and it reached a minimum value at 760$^{\circ}C$. It was found that creep strain was also very low at the same temperature. Inhomogeneous deformation with intensive slip bands was observed in the specimens tested at low temperature. A thermally-assisted dislocation climb process was regularly conducted at high temperature. Twinning was found to be an important mechanism of both tensile and creep deformations of the superalloy at an intermediate temperature where ductility minimum was observed.

• 항공우주시스템공학회지
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• 제18권2호
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• pp.95-103
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• 2024

무인기에 적용되는 다양한 추진기관 기술은 항공의 중요한 개발 방향 중의 하나인 무인기의 비행 성능에 크게 관련이 있다. 본 논문에서는 무인기의 내연기관(왕복엔진, 로타리엔진, 가스터빈엔진), 하이브리드 및 순수한 전기 추진시스템에 대하여 조사를 수행하였다. 특히 이러한 추진기관들의 분류, 작동사이클, 특성 및 주요 기술들에 대하여 제시하였다. 그러므로 미래의 무인기 추진시스템의 개발 틀, 종합적인 예측 및 다양한 비교를 정립하는데 도움을 줄 것으로 판단된다.

• 한국추진공학회지
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• 제12권1호
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• pp.29-36
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• 2008

APU 가스터빈에 적용되는 연료노즐의 분무특성을 확인하였다. 분무시험은 항공기의 비행조건에 따라 4개의 작동조건에 대하여 수행하였으며 각 분무조건은 지상에서의 무부하 및 통합부하 조건과 고도 20,000 feet에서의 무부하 및 통합부하에 대해서 실험을 수행하였다. 분무특성은 레이저 빔을 이용한 가시화와 PDPA 시스템을 이용하여 SMD 및 속도측정을 수행하였으며 노즐출구에서 $20{\sim}100\;mm$지점에서 측정하였다. 연구결과 20,000 feet 무부하 조건의 경우 $90{\sim}95\;{\mu}m$ 정도의 SMD를 나타내었고 지상무부하의 경우 약 $60{\sim}75\;{\mu}m$로 측정되었으며 20,000 feet 통합부하의 경우 약 $55{\sim}65\;{\mu}m$ 지상 통합부하의 경우 $30{\sim}70\;{\mu}m$의 값을 나타내었다. 20,000 feet 무부하의 경우 화염 불안정이 발생할 가능성이 있으므로 연료분무입자의 크기를 감소하는 다양한 노력이 요구된다.

• Korean Chemical Engineering Research
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• 제59권1호
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• pp.60-67
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• 2021

본 연구에서는 CO2 포집을 포함하는 500 MWe 급 전기를 생산하는 순산소 석탄화력발전소에 대한 공정흐름도를 제시하였고, 기술경제성 평가를 수행하였다. 이 석탄화력발전소는 순환 유동층 보일러(CFB), 초초 임계 증기 사이클 증기 터빈, 보일러에서 배출되는 배기가스내 수분과 오염물질을 제거하는 배기가스 정제 장치(FGC), 산소 분리 초저온 공정(ASU), 이산화탄소를 분리하는 극저온 공정(CPU)을 포함한다. 건식 배기가스 재순환(FGR)은 CFB연소기내 온도 제어와 고농도 CO2 배출을 위하여 사용되었다. 이 순산소 석탄화력발전소의 열효율을 증가시키기 위하여 FGR 흐름에 대한 열교환, ASU에서 배출되는 질소 흐름에 대한 열교환, 그리고 CPU 내 기체 압축기의 열 회수를 고려하였다. FGR열교환기의 온도차(ΔT)의 감소는 배기가스의 더 많은 폐열 회수를 의미하며, 전기 및 엑서지 효율을 증가시켰다. FGR열교환기의 ΔT가 10 ℃ 에서 FGR과 FGC 주변의 연간 비용이 최소가 되었다. 이때, 전기 효율은 39%, 총투자비는 1371 M$, 총생산비용은 90 M$, 그리고 투자수익률은 7%/y, 그리고 투자회수기간은 12년으로 예측되었다. 본 연구를 통하여 순산소 석탄화력발전소의 열효율 향상을 위한 열교환망이 제시되었고, FGR 열교환기의 최적 운전 조건이 도출되었다.

• 한국신재생에너지학회:학술대회논문집
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• 한국신재생에너지학회 2010년도 추계학술대회 초록집
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• pp.131.1-131.1
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• 2010

This study was conducted for engineering optimization for the gasification process which is the key factor for success of Taean IGCC gasification plant which has been driven forward under the government support in order to expand to supply new and renewable energy and diminish the burden of the responsibility for the reduction of the green house gas emission. The gasification process consists of coal milling and drying, pressurization and feeding, gasification, quenching and HP syngas cooling, slag removal system, dry flyash removal system, wet scrubbing system, and primary water treatment system. The configuration optimization is essential for the high efficiency and the cost saving. For this purpose, it was designed to have syngas cooler to recover the sensible heat as much as possible from the hot syngas produced from the gasifier which is the dry-feeding and entrained bed slagging type and also applied with the oxygen combustion and the first stage cylindrical upward gas flow. The pressure condition inside of the gasifier is around 40~45Mpg and the temperature condition is up to $1500{\sim}1700^{\circ}C$. It was designed for about 70% out of fly ash to be drained out throughout the quenching water in the bottom part of the gasifier as a type of molten slag flowing down on the membrane wall and finally become a byproduct over the slag removal system. The flyash removal system to capture solid particulates is applied with HPHT ceramic candle filter to stand up against the high pressure and temperature. When it comes to the residual tiny particles after the flyash removal system, wet scurbbing system is applied to finally clean up the solids. The washed-up syngas through the wet scrubber will keep around $130{\sim}135^{\circ}C$, 40~42Mpg and 250 ppmv of hydrochloric acid(HCl) and hydrofluoric acid(HF) at maximum and it is turned over to the gas treatment system for removing toxic gases out of the syngas to comply with the conditions requested from the gas turbine. The result of this study will be utilized to the detailed engineering, procurement and manufacturing of equipments, and construction for the Taean IGCC plant and furthermore it is the baseline technology applicable for the poly-generation such as coal gasification(SNG) and liquefaction(CTL) to reinforce national energy security and create new business models.

• Journal of Electrical Engineering and Technology
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• 제9권5호
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• pp.1511-1519
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• 2014

The objective of this paper is to propose a modelling of a small compressed air energy storage system, which drives an induction generator based on a field-oriented control (FOC) principle for a renewable power generation. The proposed system is a hybrid technology of energy storage and electrification, which is developed to use as a small scale of renewable energy power plant. The energy will be transferred from the renewable energy resource to the compressed air energy by reciprocating air compressor to be stored in a pressurized vessel. The energy storage system uses a small compressed air energy storage system, developed as a small unit and installed above ground to avoid site limitation as same as the conventional CAES does. Therefore, it is suitable to be placed at any location. The system is operated in low pressure not more than 15 bar, so, it easy to available component in country and inexpensive. The power generation uses a variable speed induction generator (IG). The relationship of pressure and air flow of the compressed air, which varies continuously during the discharge of compressed air to drive the generator, is considered as a control command. As a result, the generator generates power in wide speed range. Unlike the conventional CAES that used gas turbine, this system does not have any combustion units. Thus, the system does not burn fuel and exhaust pollution. This paper expresses the modelling, thermodynamic analysis simulation and experiment to obtain the characteristic and performance of a new concept of a small compressed air energy storage power plant, which can be helpful in system designing of renewable energy electrification. The system was tested under a range of expansion pressure ratios in order to determine its characteristics and performance. The efficiency of expansion air of 49.34% is calculated, while the efficiency of generator of 60.85% is examined. The overall efficiency of system of approximately 30% is also investigated.