• Proceedings of the SAREK Conference
• /
• 2008.06a
• /
• pp.1190-1194
• /
• 2008

The study aims to analyzed and identify the heat transfer characteristics of water-jet-impingement with use of 3-D numerical-analysis in order to design the old water duct. The temperature comparison processes were done with various duct flows. In addition, the optimal conditions of water-jet-impingement were proposed as jet-pressure, the temperature on the beat plane, and so on.

• Proceedings of the Korean Society of Propulsion Engineers Conference
• /
• 2006.11a
• /
• pp.59-63
• /
• 2006

A direct photograph measurement technique was used to determine the spatial distribution of the spray droplet diameter in subsonic crossflow and it also obtain that SMD distribution by using PLLIF technique. The injector internal flow was classified as three modes such as a normal, cavitation, and hydraulic flip. The objectives of this research are getting a droplet distribution and drop size measurement of normal flow and compare with the other flow effects. Although the study showed visually that drop size were spatially dependent of Air-stream velocity, fuel injection velocity, and normalized distance from the injector exit length.(x/d, y/d) There are also difference characteristics between cavitation, hydraulic flip and the normal flow.

• Journal of the Korean Society of Propulsion Engineers
• /
• v.5 no.1
• /
• pp.34-41
• /
• 2001

A study has been conducted to observe the slot film cooling effect on a convergent nozzle wall. The slot film cooling is used to protect the nozzle wall from the hot combusted gas by the coolant injected from the slot around the inner wall of the nozzle. The film cooling effectiveness and the heat transfer to the nozzle wall are influenced significantly by the blowing ratio of the coolant to the main flow and those are also influenced by the shape of the slot and the flow acceleration in the nozzle. In the present study, the heat transfer for the various blowing ratios has been performed by the experimental method and the results are compared with the results computed by the empirical formula. The numerical method has been conducted to compare the film cooling effectiveness of the convergent nozzle with that of the cylinder. For the relatively low blowing ratio, the cooling effectiveness increases sharply as the blowing ratio increases, and the increasing rate slows down for the high blowing ratio.

• 월간 기계설비
• /
• s.119
• /
• pp.71-83
• /
• 2000

점차 복잡해지고 있는 사회적 욕구를 만족시키기 위한 건물에서는 반드시 복잡한 설비가 요구되고 있고, 이러한 설비시스템 중에는 급수, 급탕 및 배수설비라고 하는 배관시스템이 없다면 기능유지에 막대한 지장을 초래할 것은 자명하다고 하겠다. 이러한 배관시스템에서는 항시 또는 일부 사용되어질 물이나 사용된 물이 흐르기 때문에 배관내부에 발생하는 스케일(scale)이나 슬라임(slime) 등은 피할 수 없는 사실인 것이다. 건축물 내에 설치된 각종 배관은 건물의 기능을 유지하고 보건위생과 직결되는 중요한 기능을 담당하고 있어 세척의 필요성이 매우 높음에도 불구하고 배관의 수명이 다할 때까지 거의 세척이 이루어지지 않고 사용되어 왔다. 이들 배관에 대한 세척은 배관의 수명연장과 관마찰 계수를 낮추어 급수의 수송동력을 절감할 수 있고, 난방관의 열전달 효과를 높여 에너지 절약 효과를 거두어 건물의 유지관리 비용 절감에 기여할 수 있음에도 적절한 세척공법이 개발되지 않고 있다. 이러한 관점에 맞추어 건물배관의 특성에 맞도록 고압 세척장치를 개발하고 이를 이용한 세척공법을 적용하고자 하였다. 즉, 배관 내에 압축공기를 주기적으로 분사하여 맥동현상이 일어나도록 하면서 기포를 발생시켜 기포가 관의 내벽에서 성장하여 파괴될 때 관내에 부착된 이물질을 제거할 수 있고, 또한 세척효과를 높이기 위하여 관의 벽면에 접촉하면서 배출되는 과정에서 이물질을 제거할 수 있도록 구조와 아울러 이들 장치를 이용한 세척방법의 적용성에 대해서 고찰하고자 한다.

• Proceedings of the KIEE Conference
• /
• 2006.07c
• /
• pp.1548-1549
• /
• 2006

모세관 방전은 내벽의 절연 물질이 용발되어 수만도 영역에서 고압의 플라즈마를 생성하는 장치로서 이로부터 분사된 플라즈마 제트는 추진제 점화나 신물질 제조 둥에 이용할 수 있다. 본 연구에서는 수십 $m{\Omega}$ 영역에서 수 ms에 걸쳐 수십 kA의 펄스 전류가 흐르는 모세관 방전에 대해 플라즈마의 온도 및 압력에 의해 결정되는 저항을 통하여 펄스 전원 회로를 해석하며, 이로부터 공급되는 오옴열에 의해 플라즈마의 온도, 압력 등이 결정되는 유체역학적 변화를 수치적으로 계산하였다. 이 결과는 용발에 의해 정상 상태에 도달하는 플라즈마의 특성을 잘 보여주고 있으며, 모세관 방전 실험의 전기적, 유체역학적 변수 예측에 유용하게 쓰일 수 있다.

• Proceedings of the KSME Conference
• /
• 2007.05b
• /
• pp.3311-3316
• /
• 2007

To analyze the influence of valve overlap period on a backfire occurrence, the single cylinder research engine with MCVVT(Mechanical Continuous Variable Valve Timing) system is developed and backfire limit equivalence ratio defined as fuel-air ratio equivalence ratio at which backfire occurs is examined according to various valve overlap period. The MCVVT is the system to control valve overlap period by mechanical device. It is estimated that the lower valve overlap period has the higher backfire limit equivalence ratio though the same energy is supplied. When the valve overlap period is changed from 30$^{circ}$ CA to 0$^{circ}$ CA, backfire limit equivalence ratio is increased 74%, approximately. It means that valve overlap period is concern in backfire occurrence, and may be one of the methods for controlling back fire occurred in a $H_2$ engine.

• Transactions of the Korean hydrogen and new energy society
• /
• v.18 no.4
• /
• pp.374-381
• /
• 2007

In order to verify the feasibility of expansion of back-fire limit equivalence ratio in the hydrogen-fueled engine with external mixture, the characteristics of performance and combustion are experimentally analyzed with change of intake/exhaust valve timings under the fixed valve overlap period of $0^{\circ}$ CA(non-valve overlap period). These characteristics are also tested for the change of exhaust valve closing timing while intake valve opening timing is fixed to clear the main cause of back-fire occurrence. As the results, the less valve overlap period center is retarded, the more back-fire limit equivalence ratio increases and back-fire does not occurred after TDC. In addition, it was shown that the control of back-fire is dependent on intake valve opening timing than valve overlap period.

• Transactions of the Korean hydrogen and new energy society
• /
• v.17 no.3
• /
• pp.255-262
• /
• 2006

To develop a hydrogen fueled engine with external mixture which uses in high reliability, low cost and low pressure, the single cylinder research engine with MCVVT(Mechanical Continuous Variable Valve Timing) system is developed and its basic characteristics analyzed. The MCVVT developed has high reliability and the valve timing change is possible in wide range continuously. Though the mechanical loss due to MCVVT system is increased a little, back-fire suppression research for valve overlap period is no difficulty. It's also confirmed that the hydrogen-fueled engine has lower torque and is possible high lean burn. As fuel-air equivalence ratio is high, as thermal efficiency is remarkable increasing.

• Transactions of the Korean hydrogen and new energy society
• /
• v.24 no.2
• /
• pp.136-141
• /
• 2013

In order to achieve simultaneously the ultra-low NOx, the high power and the high efficiency in a hydrogen-fueled engine with SI and the external mixture, the effects of low temperature combustion, performance and exhaust are compared and analyzed by the application of the lean boosting. As the results, the decrease rate of the high temperature in the hydrogen is less decreased than the other fuels by high constant-volume specific heat. However, when the conditions of 1.7bar and ${\Phi}=0.33$ are reached by the lean boosting, the maximum gas temperature of hydrogen is decreased under the temperature of NOx formation and it is possible to stabilize combustion below 2% of COVimep. Also, at that condition, it is feasible to achieve simultaneously NOx-free and the power of gasoline level. Therefore, it is found that the lean boosting is useful in the hydrogen-fueled engine.

• Transactions of the Korean hydrogen and new energy society
• /
• v.20 no.6
• /
• pp.464-470
• /
• 2009

In order to analysis the possibility of high expansion and performance without backfire in a hydrogenfueled engine using external mixture injection, combustion characteristics and performance enhancement were analyzed in terms of retarding valve timing and increasing the boosting pressure. As the results, it was found that thermal efficiency increased by retarding intake valve timing with the same level of supplied energy is over 6.6% by the effect of high expansion including effect of combustion enhancement due to supercharging. It was also shown that the achievement of high power (equal to that of a gasoline engine), low brake specific fuel consumption and low emission (NOx of less than 16 ppm) without backfire in a hydrogen-fueled engine is possible around a boosting pressure of 1.5 bar, intake valve opening time of TDC and $\Phi$=0.35 in fuel-air equivalence ratio.