• 한국자동차공학회논문집
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• 제17권3호
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• pp.29-34
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• 2009

Diesel particulate filter (DPF) has been developed to optimize engine out emission, especially particulate matter (PM). One of the main important factors for developing the DPF is estimation of soot mass being accumulated inside the DPF. Evaluation of pressure drop over the DPF is a simple way to estimate the accumulated soot mass but its accuracy is known to be limited to certain vehicle operating conditions. The method to compensate drawback is adoption of integrating time history of the engine out PM and burning soot. Present study demonstrates current status of the soot estimation methods including the results from the engine test benches and vehicles.

• 한국자동차공학회논문집
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• 제5권5호
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• pp.213-218
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• 1997

CNG dual fuel engine for heavy duty diesel engine has been equipped to a Korean bus engine and tested to compare th engine performance and the emission characteristics with the existing diesel fueled engine. The results are summarized as follows. Diesel fueled engine has the fuel injection timing of BTDC17°. The injection timing of CNG modified engine is retarded to BTDC14° for reduction of NOx. Performance optimization has been carried out to have engine power equivalent to or better than the diesel fueled engine. Smoke is decreased by 85% by Korean smoke 3 mode test. By 6 mode test CO is increased by 313% and THC is increased by 1407%. NOx is decreased by 27%. Even though THC is increased very much, it's not too serious problem since CO and THC emission of diesel engine are very little compared to gasoline engine and THC don't give bad effect on human health. But the reduction technologies of CO and THC need to be considered.

• 한국농업기계학회:학술대회논문집
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• 한국농업기계학회 1993년도 Proceedings of International Conference for Agricultural Machinery and Process Engineering
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• pp.267-276
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• 1993

A kinetmatic stirling engine with a domed heater was designed, fabricated and test. In designing and fabrication of the engine various problems were confronted and solved. Among various parts of the engine, cooler and main seal needed sophisticated techniques to fabricated in order to prevent leakage of working gas from the parts and to ensure their proper functions in the engine. The engine had a series of experiment at various working gas pressure, heater temperatures and engine speeds to evaluate its performance. Indicated and brake power outputs and indicated and brake thermal efficiencies were determined from the experimental data. The engine resulted a little inferior performance to that of the GPU-3 engine of which performance was well reported . Several recommendations were made to improve the performance of the engine during the evaluation of its performance.

• Journal of Mechanical Science and Technology
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• 제15권10호
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• pp.1442-1450
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• 2001

The EGR system has been widely used to reduce nitrogen oxides (NO$\_$x/) emission, to improve fuel economy and suppress knock by using the characteristics of charge dilution. However, as the EGR rate at a given engine operating condition increases, the combustion instability increases. The combustion instability increases cyclic variations resulting in the deterioration of engine performance and emissions. Therefore, the optimum EGR rate should be carefully determined in order to obtain the better engine performance and emissions. An experimental study has been performed to investigate the effects of EGR on combustion stability, engine performance,70x and the other exhaust emissions from 1.5 liter gasoline engine. Operating conditions are selected from the test result of the high speed and high acceleration region of SFTP mode which generates more NO$\_$x/ and needs higher engine speed compared to FTP-75 (Federal Test Procedure) mode. Engine power, fuel consumption and exhaust emissions are measured with various EGR rate. Combustion stability is analyzed by examining the variation of indicated mean effective pressure (COV$\_$imep/) and the timings of maximum pressure (P$\_$max/) location using pressure sensor. Engine performance is analyzed by investigating engine power and maximum cylinder pressure and brake specific fuel consumption (BSFC)

• 한국산업융합학회 논문집
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• 제27권3호
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• pp.629-634
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• 2024

The Korea Research Institute of Ships and Ocean Engineering (KRISO) has developed a test module that can vertically ascend and descend with a buoyancy engine to verify the performance of the developed buoyancy engine. The independent test module has been tested in the Ocean Engineering Basin(C.M.Lee et al., 2023). After that, more tests were performed in the Deep Ocean Engineering Basin and at sea. In the 50-meter depth pit test of the Deep Ocean Engineering Basin, there were no problems with the ascent and descent operations, but the buoyancy engine was not properly maintained due to various problems in the independent test module, resulting in a difference between the calculated results using the solution of the equations of motion and the actual measurement results. The East Sea test was conducted at a depth of approximately 110 meters north-east of Pohang, with a dive to 100 meters. The difference between the pressure sensor value and the calculated value was observed, but after checking the results of the underwater position tracking device(USBL, Ultra Short Base Line system), it was estimated that the difference was caused by the influence of the current.

• 한국추진공학회지
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• 제8권2호
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• pp.18-24
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• 2004

가스터빈엔진 압축기의 서지마진을 구하기 위하여 연료 돌출 시험을 수행하였다. 본 시험에 사용된 연료 돌출 신호는 엔진 제어기 신호에 중첩되어 연료 밸브를 제어하는 데 사용되었으며 신호 중첩을 위해 연료 제어기와 함수 발생기로 구성된 보조시스템이 사용되었다. 한국항공우주연구원의 고공엔진시험설비에서 실제 엔진 시험이 이루어졌으며 예비 시험결과, 연료 돌출 신호는 연료 라인과 압축기 토출부에서의 압력 신호와 잘 일치하였다. 이에 따라 특정 속도에서의 서지점을 측정하기 위한 시험이 수행되었으며 시험 결과 연료 돌출시험이 서지 측정에 매우 효과적임을 확인하였다.

• 한국추진공학회:학술대회논문집
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• 한국추진공학회 2011년도 제37회 추계학술대회논문집
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• pp.56-61
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• 2011

한국형발사체 추진기관 개발을 위한 연소기 연소시험설비, 터보펌프 실매질 시험설비, 3단 엔진 연소시험설비, 엔진 지상 및 고공모사 연소시험설비, 추진기관 시스템 시험설비 구축 계획에 대해 간략히 기술하였다. 연소기, 터보펌프, 엔진 시험설비에서는 3단 엔진 및 75톤급 액체로켓엔진의 부품 및 엔진시스템의 개발 및 인증시험을 수행할 예정이고, 추진기관 시스템 시험설비에서는 한국형발사체 1/2/3단용 추진기관 시스템의 개발 시험을 수행할 예정이다. 추진기관 시험설비는 나로우주센터에 건설될 예정이며 구축 일정, 예산, 안전거리, 효율성 등을 고려하여 구축하고자 한다.

• 한국추진공학회지
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• 제22권3호
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• pp.119-127
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• 2018

중소형급 무인 항공기에 활용되고 있는 왕복동 엔진의 고도시험을 위한 시험 장치를 설계 및 제작하였으며, 예비 성능시험과 계산을 통하여 활용가능 여부를 판단해 보았다. 시험 장치는 현재 한국항공우주연구원에서 운용 중인 터보샤프트 엔진 고도시험설비에서 활용이 가능하도록 구성하였으며, 왕복동 엔진의 고도시험을 수행하기 위한 각종 제한조건을 가정하고 이를 만족할 수 있도록 개발하였다. 특히 대유량의 공기와 연료가 필요한 터보샤프트 엔진에 비하여 적은 유량이 필요한 왕복동 엔진의 성능시험을 위하여 고도 및 비행 마하수 조건의 제어가 가능하도록 장치를 구성하였으며, 엔진에 공급되는 연료의 온도를 보다 손쉽게 조절할 수 있는 장치들을 개발하였다.

• Tribology and Lubricants
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• 제16권1호
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• pp.33-38
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• 2000

Abstract- In this paper tribological characteristics of solid and liquid phase sintered W/C-35%Ni tappets were investigated. Three test methods were performed to investigate the wear and surface damage mechanism of sintered tappets. First, block-on-ring wear test was performed to investigate the wear characteristics under pure sliding condition. Second, simplified cam and tappet tests (called component wear test hereafter) were carried out to simulate the real contact history of cam and tappet. Also, after the test, contact surfaces were analyzed with scanning electron microscope to study the wear mechanism. As a final screening, engine dynamo tests were performed. Results showed that in the block on ring sliding wear test, solid phase sintered specimens showed superior wear resistance to liquid phase sintered specimens. The component wear tests and engine dynamo tests also showed the same results. Therefore, in these tests, solid phase sintered tappet material revealed superior wear resistant properties to liquid phase sintered one.

• 대한기계학회:학술대회논문집
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• 대한기계학회 2002년도 학술대회지
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• pp.271-274
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• 2002

This paper is investigated construction of the Scramjet test facility and test method of Scramjet engine combustor model. Scramiet engine combustor model test was performed at Lab C-16BK CIAM (Central Institute of Aviation Motors) at Tyraevo in Moscow. The velocity of flow in the combustion chamber equal to Mach number 2.49 with single hole fuel spray nozzle injector and test duration equal to 7 seconds. Therefore In this paper is showed high altitude test method of Scramjet combustor model and the proper structure of combustor with single hole fuel spray nozzle.