• 한국산학기술학회논문지
• /
• 제18권1호
• /
• pp.345-350
• /
• 2017

디젤 엔진의 연비와 배기를 개선하고자 하는 노력으로 다운사이징이 강화되고 있다. 이에 따라 엔진의 사이즈는 작아지고, 엔진 연소실 내 온도와 압력은 상승하는 추세이다. 따라서 높은 온도와 압력 조건에서 연료 분무의 발달과정과 연소과정 연구가 매우 중요하다. 본 연구에서는 디젤 엔진 연소실의 고온 고압 환경을 벤치에서 모사해줄 수 있는 정적 연소실을 개발하였다. 정적 연소실은 예혼합기를 연소시켜 순간적으로 온도와 압력을 급격하게 상승시킨 다음, 주변으로의 열전달에 의해 온도와 압력이 감소할 때 시험 목표조건인 온도와 압력 조건에 다다르면, 연료 분사기에 신호를 인가하여 연료분무를 개시하며 쿼츠 창을 통하여 연료 분무를 가시화 한다. 이 때, 정적 연소실 내에 연료 분무가 이루어지는 영역의 온도를 정확히 측정하여 정확한 시험 조건을 형성해야 한다. 본 연구에서는 고속으로 온도를 측정할 수 있는 열전대를 직접 개발 및 제작하여 연소실 내 시공간적 온도분포를 측정하였다. 측정 결과, 전체 체적 온도보다 연료 분무가 개시되는 중심 공간의 온도가 더 높게 나타났으며, 이는 연소실 벽면으로의 열전달 때문임을 확인하였다. 또한 횡방향으로의 온도 편차는 약 10%이내 수준이었으나, 종방향으로 온도편차가 최대 15%수준으로 나타났고 이는 부력으로 인한 고온의 연소가스의 상승효과 때문으로 판단되었다.

• 한국연소학회:학술대회논문집
• /
• 한국연소학회 1999년도 제19회 KOSCO SYMPOSIUM 논문집
• /
• pp.11-20
• /
• 1999

Acoustic pressure response and NO formation of hydrogen-air diffusion flames at various pressures are numerically studied by employing counterflow diffusion flame as a model flame let in turbulent flames in combustion chambers. The numerical results show that extinction strain rate increases linearly with pressure and then decreases, and increases again at high pressures. Thus, flames are classified into three pressure regimes. Such non-monotonic behavior is caused by the change in chemical kinetic behavior as pressure rises. Acoustic pressure response in each regime is investigated based on the Rayleigh criterion. At low pressures, pressure-rise causes the increase in flame temperature and chain branching/recombination reaction rates, resulting in increased heat release. Therefore, amplification in pressure oscillation is predicted. Similar phenomena are predicted at high pressures. At moderate pressures, weak amplification is predicted. Emission index of NO shows similar behaviors as to the peak-temperature variation with pressure.

• 한국추진공학회지
• /
• 제20권5호
• /
• pp.51-59
• /
• 2016

STS 321 스테인리스강은 액체 로켓 엔진을 비롯한 고온 고압의 시스템의 재료로서 많이 사용된다. 321 스테인리스강의 고온에서의 변형 거동을 예측하기 위해 Kocks의 전위 장벽 모델을 근거로 유동응력에 대한 구성 방정식을 열적 응력 요소와 비열적 응력 요소를 사용하여 제안하였다. 제안한 모델은 321 스테인리스강의 상온부터 $500^{\circ}C$의 넓은 온도 영역에서 재료의 변형 거동들을 잘 예측하였다.

• 한국세라믹학회지
• /
• 제31권6호
• /
• pp.637-642
• /
• 1994

Using SHS(Self-propagating High-temperature Synthesis) method, the optimum synthetic condition of titanium carbonitride was established by controlling the parameters such as relative density of mixture (Ti+C), nitrogen pressure, additive amounts of titanium hydride(TiH1.924) and protecting heat loss. Under 1 atm nitrogen pressure, nitridation ratio with changing relative density of the sample compacts has a maximum (87.2%) at about 55%, and in the case of enveloping the pellet with a quartz tube, the highest nitridation ratio of 90% was obtained at about 68%. At relative density of 55%, nitridation ratio with the nitrogen pressure has a miximum (87.3%) at 7 atm. As the amounts of additive titanium hydride increased, nitridation ratio decreased at below 7 atm nitrogen pressure and, increased at above this pressure until percent of addition percent reached 15 wt% and decreased abruptly upon futher increases in titanium hydride. In the synthesis of TiCxNy by combustion reaction, heat transfer from combustion zone to preheating zone and nitrogen gas penetration into the compact were found to be important factors affecting the TiCxNy formation. It was difficult to obtain high nitridation ratio when the conbustion temperature was either too high or too low, and it seems that the retention of high temperature after a combustion wave sweeped through the reactant mixture pellet is critical to obtain a satisfactory nitridation ratio.

• 대한기계학회논문집B
• /
• 제27권11호
• /
• pp.1595-1603
• /
• 2003

Droplet combustion at high ambient pressures is studied numerically by formulating one dimensional combustion model in the mixture of n-heptane fuel and air. The ambient pressure is supercritical conditions. The modified Soave-Redlich-Kwong state equation is used in the evaluation of thermophysical properties to account for the real gas effect on fluid p-v-T properties in high pressure conditions. Non-ideal thermodynamic and transport property at near critical and supercritical conditions are also considered. Several parametric studies are performed by changing ambient pressure and initial droplet diameter. Droplet lifetime decreased with increasing pressure. Surface temperature increased with increasing pressure. Ignition time increased with increasing initial droplet diameter. Temporal or spatial distribution of mass fraction, mass diffusivity, Lewis number, thermal conductivity, and specific heat were presented.

• 한국추진공학회:학술대회논문집
• /
• 한국추진공학회 2005년도 제25회 추계학술대회논문집
• /
• pp.341-345
• /
• 2005

본 논문은 액체로켓엔진용의 약 1.5MW급 터빈을 구동할 수 있고, 액체산소와 케로신을 추진제로 하는 연료과잉 영역에서 작동하는 실물형 가스발생기의 고압연소특성에 대한 것이다. 실물형 가스발생기 개발과정의 개략적인 과정, 연소시험 결과 분석에 따른 혼합비와 온도관계식, 연소가스의 물성치인 분자량 및 비열비 등에 대한 내용을 기술하였다. 혼합비에 따른 온도관계식을 고압에서 새롭게 얻을 수 있었으며 연소가스의 분자량 및 비열비를 수정하고 유량관계식을 통해 이들의 타당성을 확인하였다.

• Journal of Advanced Marine Engineering and Technology
• /
• 제34권2호
• /
• pp.243-249
• /
• 2010

디젤기관에 있어서 PM과 NO의 동시저감을 위한 에멀전연료의 적용은 급속도로 발전되어져왔다. 하지만, C중유 에멀젼연료의 연소계측 해석은 다른 연료에 비하여 복잡한 연소형태 때문에 어려움이 많다. 본 연구에서는 높은 압력과 온도의 정적연소실에서 에멀젼 C중유를 분사 연소시켜, 연소해석에 대한 실질적인 근거를 제시한다.

• 한국자동차공학회논문집
• /
• 제7권8호
• /
• pp.43-54
• /
• 1999

The effects of equivalence ratio and pressure on burnt gas temperature in premixed fuel rich propane-oxygen-inert gas combustion are investigated over the wide ranges of equivalence ration from 1.5 to 2.7 and pressure from 0.1 to 7 MPa by using a specially designed disk -type constant-voume combustion chamber, The premixtures are simultaneously ignited by eight spark plugs located on the circumference of combustion chamber with 45 degree interals. The eight converging flames compress the end gases to high pressures. The burnt gas temperature is meausured by the nmodifie dtow-colr pyrometry method. The transmissivity in the chamber center during the final stage of combustion at the hightest pressure is meausred by in situ laser extinction method. It is found that a temperature difference between the burnt gas temperature measured by mofidied and conventrational two-color method is 10 to 20 K, but the accuracy of the modified two-color methdo is higher if the local transmissivity in observed region is uniform , and the combustion at higher pressures results gas density conditions and the burnt gas temperature increases as the volume fraction of argon is increased because the specific heat of argon is lower compared to that of nitrogen with a constant equivalence ratio.

• 한국자동차공학회논문집
• /
• 제16권2호
• /
• pp.143-149
• /
• 2008

The present study is mainly motivated to investigate the vaporization, auto-ignition and spray combustion processes in DI diesel engine using DME and n-heptane. In order to realistically simulate the dimethyl ether (DME) spray dynamics and vaporization characteristics in high-pressure and high-temperature environment, the high-pressure vaporization model has been utilized. The interaction between chemistry and turbulence is treated by employing the Representative Interaction Flamelet (RIF) model. The detailed chemistry of 336 elementary steps and 78 chemical species is used for the DME/air reaction. Based on numerical results, the detailed discussion has been made for the distinctly different combustion characteristics of DME diesel engine in term of vaporization, ignition delay, pollutant formation, and heat release rate.

• 한국자동차공학회논문집
• /
• 제19권2호
• /
• pp.105-110
• /
• 2011

Through this study, the performance evaluation on the addition of low-pressure loop EGR(Exhaust Gas Recirculation) in a 6.0 L commercial diesel engine was carried out using WAVE modeling and simulation. Since the key technology of advanced diesel engine combustion such as low-temperature combustion is to steadily supply high rates of EGR in a wide operating range, the current study could be effectively contribute to the design and development processes of up-to-date diesel engine systems as real-world reference data. The current simulation results show that the system in which low-pressure loop EGR is added shows almost 2.3 times increase in maximum EGR rate at 1000 rpm as well as almost 1.6 times increase at 2200 and 1600 rpm in comparison with an engine system employing high-pressure loop EGR only. Also, both turbocharger axis speed and charging pressure level did not deteriorate due to the addition of low-pressure loop EGR at 2200 and 1000 rpm, but they were fairly decreased at 1600 rpm.