• Title/Summary/Keyword: 엔진냉각

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Numerical Simulation on Flows inside an Engine Room with Radiator and Cooling Fan Models (방열기 및 냉각팬을 고려한 엔진룸 내부유동 해석)

  • Kim S. L.;Lee S. C.;Lee K. H.;Hur N.
    • 한국전산유체공학회:학술대회논문집
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    • 1995.10a
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    • pp.70-75
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    • 1995
  • Recently, for the thermal system design in an engine room, the importance of the numerical analysis on the heat and fluid flow has been recognized. In the present study, the flow inside an engine room with complex geometry was analysed by use of TURBO-3D program being developed in KIST. Radiator and Cooling fan were simulated by porous media and momentum sources, and the result shows a good agreement with our expectation.

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A Numerical Simulation of Regenerative Cooling Heat Transfer for the Rocket Engine (로켓엔진의 재생 냉각 열전달 해석)

  • 전종국;박승오
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2003.05a
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    • pp.127-130
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    • 2003
  • This paper presents the numerical thermal analysis for regeneratively cooled rocket thrust chambers. An integrated numerical model incorporates computational fluid dynamics for the hot-gas thermal environment, and thermal analysis for the liner and coolant channels. The flow and temperature fields in rocket thrust chambers is assumed to be axisymmetric steady state which is presumed to the combustion liner. The heat flux computed from nozzle flow is used to predict the temperature distribution of the combustion liner. As a result, we present the wall temperature of combustion liner and the temperature change of coolant.

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Optimization of Automotive Engine-cooling Fan Noise Using Response Surface Method (반응면 기법을 이용한 자동차 엔진 냉각팬의 저소음설계)

  • Lee, J.;Ahn, J.;Lee, S.
    • Proceedings of the Korean Society for Noise and Vibration Engineering Conference
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    • 2000.06a
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    • pp.407-412
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    • 2000
  • Response surface method is employed in optimizing the acoustic performance of automotive engine-cooling axial fans. The effects of modifications in blade geometry on noise reduction are investigated. Taking the far-field noise level as the objective, a quadratic response surface is constructed utilizing D-Optimality condition as the candidate-points selection criteria. It is shown that the quadratic model exhibits an excellent fitting capability resulting in the blade design with low far-field noise level.

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Effect on emission reduction of the MWFs mist by a installation of a semi-enclosed double hood at the machine parts manufacturing process (기계가공라인에서 반밀폐식 이중후드 설치에 마른 MWFs 미스트 감소효과에 관한 연구)

  • 엄경호;이병규
    • Proceedings of the Korea Air Pollution Research Association Conference
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    • 2001.11a
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    • pp.293-294
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    • 2001
  • 자동차 엔진을 구성하는 소재 가공시에 냉각, 절삭용구와 가공표면의 용접현장(welding), 고온에서의 마모방지와 잔열로 인한 비틀림(distortion) 방지 등을 목적으로 사용되는 수용성(soluble) MWFs (Metalworking Fluids)의 기능에 필요한 구성물질인 기유(base oil)와 첨가제(additive)가 건강상 장해를 유발한다고 알려지고 있다(김신범, 1997). 하지만 수용성 MWFs를 사용하여 소재를 가공하는 산업현장에서는 MWFs 미스트 발생제어를 공정 상부에 외부식 후드를 국소적으로 설치하는 것이 일반적인 방법이다(Fig.2). (중략)

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Combustion Stability Test of LRE Thrust Chamber using Artificial Perturbation Method (강제교란 방법을 이용한 액체로켓엔진 연소기의 연소안정성 시험)

  • Lee, Kwang-Jin;Seo, Seong-Hyeon;Han, Yeoung-Min;Choi, Hwan-Seok;Ko, Young-Sung
    • Journal of the Korean Society of Propulsion Engineers
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    • v.14 no.3
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    • pp.52-60
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    • 2010
  • Combustion stability tests of 30 $ton_f$-class LRE thrust chamber with double swirl coaxial injector were carried out in domestic ground combustion test facility by means of artificial perturbation method. In these tests, thrust chambers with varying design factors like recess number of injector, baffle length, types of film cooling and chamber diameter were used and test results showed that these design factors are closely related with high frequency combustion stability. By using the oscillation decrement instead of the decay time in the combustion stability analysis of artificially perturbed LRE thrust chamber, it was confirmed that increment of damping factor results in the improvement of high frequency combustion stability of LRE thrust chamber.

케로신/액체산소 다단연소 사이클 로켓엔진용 산화제 과잉 예연소기 기술

  • Mun, Il-Yun;Yu, Jae-Han;Ha, Seong-Eop;Mun, In-Sang;Lee, Su-Yong
    • The Bulletin of The Korean Astronomical Society
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    • v.37 no.2
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    • pp.151.2-151.2
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    • 2012
  • 터보펌프 구동에 사용된 가스발생기 생성가스를 연소기로 공급하여 주추력 발생에 사용하는 다단연소 사이클 로켓엔진은 고추력을 요하는 우주 발사체에 널리 사용되고 있다. 다단연소 사이클 로켓엔진에 사용되는 가스발생기를 예연소기라 부르며 케로신과 액체산소를 추진제로 하는 다단연소 사이클 로켓엔진에는 산화제 과잉 예연소기가 사용된다. 예연소기는 터보펌프 구동을 목적으로 하기 때문에 예연소기 생성가스의 횡단면 온도분포는 터빈에 의해 제한되는 온도범위 내에서 균일하여야 하며 넓은 운전영역에서 안정적인 연소가 이루어져야 한다. 산화제 과잉 예연소기는 모든 추진제가 혼합헤드를 통해 분사되는 방식과 추진제를 혼합헤드와 연소실로 나누어 공급하는 방식이 있다. 기술검증을 위해 산화제 일부와 연료를 혼합헤드를 통해 연소실에 공급하여 1차 연소시키고 나머지 산화제를 연소실 냉각채널을 거쳐 연소실 중앙의 분사공을 통해 연소실로 주입하여 기화시키는 형태로 최종적으로 연소압 20MPa, 혼합비 60에서 작동하는 산화제 과잉 예연소기를 설계하여 연소시험을 수행하였다. 혼합헤드에는 별도의 점화용 분사기 없이 전체 연료 분사기를 통해 점화용 연료인 TEA/TEB 혼합물을 분사하여 점화하였다. 추진제를 2단으로 공급할 수 있도록 고안된 가압식 연소시험 설비에서 10회, 누적 60초 이상의 연소시험이 성공적으로 수행되었다. 연소시험결과 넓은 작동영역에서 안정적 연소특성과 생성가스 온도 분포의 균일성을 확인할 수 있었다. 고온 고압의 산화제 과잉 예연소기 기술 확보를 통해 케로신/액체산소 다단연소 사이클 로켓엔진 개발을 위한 기술적 기반을 마련하였다.

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State of the Art in the Development of Methane/Oxygen Liquid-bipropellant Rocket Engine (메탄/산소 이원액체추진제 로켓엔진 기술개발 동향)

  • Kim, Jeong Soo;Jung, Hun;Kim, Jong Hyun
    • Journal of the Korean Society of Propulsion Engineers
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    • v.17 no.6
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    • pp.120-130
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    • 2013
  • A study was conducted for the performance characteristics of methane taking recently the limelight in the world as a next-generation propellant, with the survey for state of the art in the development of methane/oxygen rocket engine being accompanied. Liquid methane as a rocket fuel has the favorable characteristics such as non-toxic, low cost, regenerative cooling capability, and potential for in-situ resource utilization (ISRU). The combination of liquid methane and liquid oxygen also provides the excellent performance including high specific impulse and low system mass. For these reasons, many researches have been actively carried out on the methane/oxygen engine, nevertheless, its technology readiness level is not that high enough just yet. Therefore, it is judged that it is the time to mitigate the technical gap with the space technology of advanced countries through a swift onset of the development of methane rocket engine.

Characteristics of Combustion by Varying Different Coolant-temperature in a Hydrogen Engine for HALE UAV (고고도 무인기용 수소연료엔진의 냉각수 온도변화에 따른 연소 특성)

  • Yi, Ui-Hyung;Jang, Hyeong-Jun;Park, Cheol-Woong;Kim, Yong-Rae;Choi, Young
    • Journal of the Korean Institute of Gas
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    • v.22 no.2
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    • pp.59-66
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    • 2018
  • Using hydrogen fuel is expected to be suitable as a reciprocating internal combustion engine with heightened interest in HALE(High Altitude Long Endurance) UAV(Unmanned Aerial Vehicle). Hydrogen is hightest energy density per mass so it can continue to charge for long periods of time and have positive part of the environmental effects. However, it is estimated that there is less research on hydrogen fuel engine currently applied, and many studies need to be done. Depending on the operation, there are factors that result in supercooling due to reduced radiation or reduce cooling performance due to low air density. Therefore, the experiment was to change the temperature of the cooling water and investigate the effect on engine combustions. The limitation of the stable operation range due to backfire is dominated by the excess air ratio rather than the effect of the cooling water temperature change. When the cooling water temperature increases, the volumetric efficiency decreases and the torque decreases. As the cooling water temperature decreases, the heat loss was increased and consequently the thermal efficiency was decreased.

A Study on the Safety Code Development of Gas Engine Micro Combined Heat and Power System (소형 가스엔진 열병합 발전시스템 안전기준 개발)

  • Kwon, Jun-Yeop;Kim, Min-Woo;Lee, Jung-Woon
    • Journal of the Korean Institute of Gas
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    • v.25 no.4
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    • pp.27-35
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    • 2021
  • Recently, as a solution to the sharp drop in "power reserve ratio", it is being converted to a microgrid that enables bi-directional transmission and distribution. A microgrid is composed of a small-scale distributed power supply and a load. As a representative technology of distributed power generation, there is a Micro Combined Heat and Power system applied to homes and buildings. In this study, a safety standard was developed by dividing the power generation system, cooling system, lubrication system, and exhaust system to derive safety standards for a small gas engine power generation system with a gas consumption less than 232.6kW (200,000 kcal/h). In the case of the power generation system, a filter was installed and the system was stopped by detecting gas leakage and abnormalities in engine speed or output and the cooling system is stipulated to stop the system in case of insufficient cooling water or overheating. The lubrication system monitors the pressure and temperature of the lubricating oil and stops the system when an abnormality occurs, and the exhaust gas emission concentration regulation value was specified in accordance with domestic and foreign standards. Through the results of this study, it is judged that the safety of the gas engine power generation system can be improved and it can contribute to the commercialization of products.

A Study on the Characteristics of Fuel Consumption and Emissions of Diesel Vehicles Using Engine Coolant Flow Rate On/Off Control (엔진 냉각수 유량 단속에 의한 디젤 차량의 연비 및 배기가스 특성 연구)

  • Kim, Sung Chul
    • Journal of the Korea Academia-Industrial cooperation Society
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    • v.14 no.5
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    • pp.2069-2074
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    • 2013
  • The use of the electromagnetic clutch water pump for internal combustion engine vehicles saves fuel and leads to a reduction in emissions. The clutch water pump allows the engine cooling system to select the optimum operation condition by using coolant flow rate on/off control. This study investigated the characteristics of fuel consumption and emissions of the diesel engine cooling system using the clutch water pump. The electromagnetic clutch operation reduced by about 49% of engine warm up period at idle condition and controlled the optimum high coolant temperature at driving condition. Therefore, fuel consumption was enhanced by about 5%, and emissions such as HC, CO and $CO_2$ were also reduced to a certain degree even though NOx increased a little bit, compared to those of the conventional water pump under NEDC mode which represents the real driving pattern.