• 한국추진공학회:학술대회논문집
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• 한국추진공학회 2007년도 제29회 추계학술대회논문집
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• pp.335-338
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• 2007

본 연구에서는 항공기 추진기관의 정확한 장착 성능해석 시 고려하여 할 주요 장착 손실 중 흡입구의 압력 손실을 계산하기 위해 2D 모델링을 수행하였으며 해석 결과를 이용하여 비행마하수와 유량에 따른 흡입구 압력손실 값을 나타낸 0D 성능 맵을 생성하였다. 이러한 성능 맵 생성 절차의 타당성을 검증하기 위해 일반적인 항공기용 엔진 흡입구 형상에 적용하여 타당성을 확인하였다.

• 한국추진공학회:학술대회논문집
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• 한국추진공학회 2008년도 제30회 춘계학술대회논문집
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• pp.263-267
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• 2008

본 연구에서는 헬리콥터 추진시스템의 장착 성능해석 모델링 시 고려하여야 할 흡입구 모델, 블리드 공기 손실, 보기류 시스템 구동에 사용되는 출력 추출 등을 포함한 장착 성능해석을 수행하였다. 흡입구의 압력 손실은 비행마하수와 유량에 따른 압력손실 값으로 나타낸 흡입구 성능 맵을 이용하였다. 추진시스템 장착 성능해석 모델링의 검증을 위해서는 실제 시험데이터와 비교해야 하지만 데이터 확보가 어려워 상용성능해석 프로그램인 GASTURB 해석결과와 비교 하였다. 해석결과 평균오차 0.5% 이내로 본 연구에서 수행한 추진시스템의 장착 성능해석 모델링의 타당성을 검증하였다.

• 한국추진공학회지
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• 제12권1호
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• pp.51-56
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• 2008

본 연구에서는 헬리콥터 추진시스템의 장착 성능해석 모델링 시 고려하여야 할 흡입구 모델, 블리드 공기 손실, 보기류 시스템 구동에 사용되는 출력 추출 등을 포함한 장착 성능해석을 수행하였다. 흡입구의 압력 손실은 비행마하수와 유량에 따른 압력손실 값으로 나타낸 흡입구 성능 맵을 이용하였다. 추진시스템 장착 성능해석 모델링의 검증을 위해서는 실제 시험데이터와 비교해야 하지만 데이터 확보가 어려워 상용성능해석 프로그램인 GASTURB 해석결과와 비교하였다. 해석결과 평균오차 0.5% 이내로 본 연구에서 수행한 추진시스템의 장착 성능해석 모델링의 타당성을 검증하였다.

• Journal of Mechanical Science and Technology
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• 제18권2호
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• pp.286-293
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• 2004

The air fuel ratios of current gasoline engines are almost controlled by several air flow meters. When CVVT (Continuous Variable Valve Timing) is applied to a gasoline engine for higher engine performance, the MAP (Manifold Absolute Pressure) sensor is difficult to follow the instantaneous air fuel ratio due to the valve timing effect. Therefore, a HFM (Hot Film Flow Meter) is widely used for measuring intake air flow in this case. However, the HFMs are incapable of indicating to reverse flow, the oscillation of intake air flow has an negative effect on the precision of the HFM. Consequently, the various duct configurations in front of the air flow sensor affect the precision of HFM sensitivity. This paper mainly focused on the analysis of the reverse flow, flow fluctuation in throttle upstream and the geometry of intake system which influence the HFM measurement.

• 한국정밀공학회지
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• 제18권10호
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• pp.161-167
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• 2001

This paper presents an approach to nonlinear engine idle controller and intake manifold absolute pressure(MAP) observer based on mean torque production model. A stable engine idle speed is important in that the unstable engine Idle mode can make engine to drooping or stall state. A sliding fuzzy controller has been designed to control engine idle speed under load disturbance. A sliding observer is also developed to estimate the intake manifold absolute pressure and compared with the actual MAP sensor value. The sliding mode observer has shown good robustness and good tracking performance. The inputs of sliding fuzzy controller are the errors of rpm and MAP. The output is a duty cycle(DC) for driving a idle speed control valve(ISCV).

• 한국정밀공학회지
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• 제22권3호
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• pp.123-129
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• 2005

The unbalance of the power output, noise, and vibration is happened by the disproportionate pressure variation in the cylinder. For this reason, decrease of the pressure in the cylinder and increase of the residual gas effect on the engine performance. If the abnormal combustion is continued, the crack would be occurred in the engine block. And it could be broken down. For the normal combustion of the SI engine, it is important to supply the balanced mixture by each operating condition. In this study, it was tested the combustion characteristics in the cylinder according to the abnormal adjusting of intake & exhaust valve. This test is willing to set a basic data's analysis fur developing an automotive diagnosis system by analyzing the pressure in the cylinder, the output signal of MAP sensor, the exhaust gas, etc.

• 한국자동차공학회논문집
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• 제11권4호
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• pp.37-43
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• 2003

The exhaust gas recirculation (EGR) is needed for one of various strategies to reduce NOx emission. But to get the proper EGR rate, the intake and exhaust system become complicated, also application of EGR system is difficult because of the penalty in fuel consumption and the increase in particulate matter. This study is focused on the development of EGR valve using the electrical method. The effects of EGR on the characteristics of NOx, CO, CO2 emissions and particulate mater have been investigated using small-displacement size 0.8-liters engine of diesel passenger car operating at several loads and speeds. After the analysis and comparison between conventional E-EGR valve and developed E-EGR valve performance by test bench, the estimation of vehicle application was executed through the EGR map and CVS-75 test result measured on the chassis dynamometer.

• 한국컴퓨터정보학회논문지
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• 제25권3호
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• pp.33-42
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• 2020

각종 감시체계에서 육안에 의존하여 물체를 식별해내는 것은 어렵고 실수하기 쉬우므로 군 감시체계에서 자동식별능력의 필요성은 더욱 높아지고 있다. 사회에 발표되는 모형들은 군 무기체계에 대한 데이터가 반영되지 않아 군에 바로 적용하는 것은 제한된다. 본 연구는 군용 헬기의 이미지에 합성곱 신경망을 적용하여 피아식별 모형을 구축한 연구이다. 제안하는 모형은 우리나라에서 주로 사용하고 있는 헬기인 AH-64 기종과 공산권 국가에서 주로 사용하고 있는 헬기인 Mi-17 기종의 이미지를 통해 학습시켜 구축되었다. 제안하는 모형의 성능을 살펴보면, 평가척도를 이용하여 평가한 결과 97.8%의 정확도, 97.3%의 정밀도, 98.5% 재현율과 97.9%의 F-measure의 성능을 보임을 확인하였다. 이런 분류 결과에 대해서 Feature-map을 통해 아군 헬기의 바퀴와 무장, 그리고 흡기구 주변이, 적군 헬기의 바퀴, 흡기구, 그리고 창문 부위가 피아식별 모형의 분류 기준임을 확인할 수 있었다. 본 연구는 CNN을 이용하여 군 무기체계 중 헬기의 영상정보에 대한 피아식별에 대한 분류를 처음으로 시도한 연구이며, 본 연구에서 제안하는 모형은 기존의 다른 무기체계에 대한 분류 모형보다 높은 정확도를 보인다.

• 한국자동차공학회논문집
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• 제10권4호
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• pp.77-84
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• 2002

For the purpose of obtaining a fundamental data which is needed to develope the port injection type charged LPLi engine system, we manufactured intake port injection system of liquid charging LPG and modified heavy duty single cylinder LPLi engine from heavy duty diesel engine. Engine output and emission characteristics were analyzed under variable air/fuel ratio and charging pressure. Since LPG is consisted of propane and butane, we investigated combustion characteristics using this two kinds of fuel. From the result of charging engine performance test, engine torque increase about 30% ∼ 40% with 0.3bar charging pressure. In low speed condition, as charging pressure increase, combustion stability improve ill lean bum condition, but, in high speed condition, combustion stability make worse in lean bum condition. We know that engine output decreased rapidly from the condition of air excess ratio 1.3. In addition, we measured emission characteristics under the lean bum and charging condition. From this experiment, we found that CO emission is out of the question in the range from stiochiometric to lean burn and charging condition, but charging pressure has influence on HC emission.

• 한국추진공학회:학술대회논문집
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• 한국추진공학회 2004년도 제22회 춘계학술대회논문집
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• pp.848-853
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• 2004

Regarding to the project SUAV (Smart Unmanned Aerial Vehicle) in KARI (Korea Aerospace Research Institute), several engine configurations has been evaluated. However it's not an easy task to collect all the necessary data of each engine for the analysis. Usually, some kind of modeling technique is required in order to determine the unknown data. In the present paper a qualitative method for reverse engineering is proposed, in order to identify some design patterns and relationships between parameters. The method can be used to estimate several parameters that usually are not provided by the manufacturer. The method consists of modeling an existing engine and through a simulation, compare its transient behavior with its operating envelope. In the simulation several parameters such as thermodynamics, performance, safety and mechanics concerning to the definition of operation-envelope, have been discussed qualitatively. With the model, all engine parameters can be estimated with acceptable accuracy, making possible the study of dependencies among different parameters such as power-turbine total inertia, TIT, take-off time and part load, in order to check if the engine transient performance is within the design criteria. For more realistic approach and more detailed design requirements, it will be necessary to enhance the compressor map first, and more realistic estimated values must be taken into account for intake-loss, bleed-air and auxiliary power extraction. The relative importance of these “unknown” parameters must be evaluated using sensitivity analysis in the future evaluation. Moreover, fluid dynamics, thermal analysis and stress analysis necessary for the resulting life assessment of en engine, will not be addressed here but in a future paper. With the methodology presented in the paper was possible to infer the relationships between operation-envelope and engine parameters.