• 한국산학기술학회논문지
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• 제18권3호
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• pp.711-717
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• 2017

본 논문은 엔진 다운사이징의 관점에서 널리 사용되는 터보과급기 로터의 관성모멘트 측정에 관한 연구이다. Trifilar 방법을 이용하여 관성모멘트를 측정하기 위한 장치를 설계 제작한 후, 장치를 검증하기 위하여 교정로터의 관성모멘트를 측정하였다. 측정의 변동계수는 0.43%, CAD 도면의 관성모멘트와 비교하여 0.75% 오차를 보여 개발된 측정장치가 로터의 관성모멘트 측정에 적합함을 확인하였다. 소형 터보과급기의 터빈 로터와 압축기 휠 각 2개에 대한 관성모멘트 측정을 수행하여 1.0% 미만의 변동계수를 보여 정밀한 측정이 가능함을 보였다. 그러나 CAD 도면의 관성모멘트와 비교한 오차는 터빈 로터는 2.76%와 1.30%로 양호하였으나, 압축기 휠의 경우 27.6%와 24.4%로 상당히 크게 나타났다. 연구에 사용된 압축기 휠은 질량이 소형으로 상대적으로 공기저항이 크고 정확한 주기 측정의 어려움으로 큰 오차를 보였다. 따라서 터빈 로터와 압축기 휠을 결합한 상태에서 측정한 값에서 터빈 로터의 관성모멘트를 빼는 간접 방법으로 측정을 수행하였다. 이때 압축기 휠의 관성모멘트 측정에서 1.2% 미만의 변동계수를 보이고 오차는 5.68%, 7.88%의 값을 보였다.

• Journal of Advanced Marine Engineering and Technology
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• 제24권6호
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• pp.110-119
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• 2000

In this paper, an experimental study is carried out under the operating conditions of low speed and rapid acceleration in order to investigate and improve the response characteristics of a turbocharged diesel engine with radial turbine driven by exhaust gas. A rapid acceleration for investigating the response performance is applied to the fuel-pump rack of the engine from 0-10% to 0-40% in steps of 10%, and accelerating time of 1, 2 and 3 seconds is applied to the engine. Further experiment for improving the low speed torque and acceleration performance is also performed by means of injecting air into the inlet manifold at compressor exit during the period of low speed and application of a rapid acceleration. The effects of air injection on the response performance are represented at subjected engine speed with the changes of response performance factors such as air injection pressure, air injection period, accelerating rate, accelerating time and load. From the experimental results obtained throughout this study, it is shown that air injection into the inlet manifold at compressor exit is closely related to the improvement of low speed and acceleration performance of a turbocharged diesel engine.

• 한국유체기계학회 논문집
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• 제13권5호
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• pp.35-42
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• 2010

This paper deals with the development of analytical model of a turbocharger and its detail rotordynamic analysis. Two analytical models, which are verified by experimental modal testing, are proposed and the analytical model including rotor shaft extended to compressor and turbine wheel end side is chosen. A rotordynamic analysis includes the critical map, Campbell diagram, stability, and unbalance response, especially nonlinear transient response considering nonlinear fluid film force at bearings. Although the linearized analysis accurately predicts the critical speeds, stability limit, and stability threshold speed, the predicted vibration results are not valid for speeds above the stability threshold speed since the rotor vibrates with a subsynchronous component much larger than the one synchronous with rotor speed. Hence, for operating speed above the stability threshold, a nonlinear transient analysis considering nonlinear fluid film force must be performed in order to accurately predict vibration responses of rotor and guarantee results of analysis.

• 한국생산제조학회지
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• 제9권4호
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• pp.123-130
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• 2000

Studies on the turbocharger itself or various aspects generated from turbocharged engine have been made on the performance for the natural aspirated engine equipped with the turbocharger and the intercooler. In this study, the performance prediction program based on turbocharger theory is developed for simulation which may reduced the cost and the trial -and-error time. The program is verified with the experimental results for 11, 000 cc diesel engine with the turbocharger and the intercooler . Also, various factors which are invisible in experiment are predicted using this program.

• 유체기계공업학회:학술대회논문집
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• 유체기계공업학회 2002년도 유체기계 연구개발 발표회 논문집
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• pp.453-458
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• 2002

The feasibility study on supporting a turbocharger rotor on air foil bearing is investigated. Based on finite difference method and Newton-Raphson method, the static equilibrium position of a turbocharger rotor is predicted. And using finite difference method and perturbation method, dynamic characteristics of air foil bearings are calculated. Rotordynamic analysis is performed by finite element method, with collaboration of calculated stiffness and damping of foil bearing. The effect of compliance and clearance of bump foil bearing on the oil-free turbocharger is investigated in terms of rotordynamics. And the critical speeds, eccentricity ratio, vibration amplitude, and stability are considered. It is demonstrated that foil bearings offer a rlausible replacement for oil-lubricated bearings in turbocharger.

• 한국유체기계학회 논문집
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• 제6권1호
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• pp.51-56
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• 2003

The feasibility study on the oil-free turbocharger supported by air foil bearings is investigated. Using the perturbation method, dynamic characteristics of air foil bearings are calculated based on the static equilibrium position of a turbocharger rotor is predicted. With collaboration of calculated stiffness and damping of foil bearing, rotordynamic analysis is performed using the finite element method. The effects of bump compliance and bearing clearance on rotordynamic characteristics of the oil-free turbocharger such as the critical speeds, eccentricity ratio, vibration amplitude and stability are investigated.

• 한국산학기술학회논문지
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• 제18권1호
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• pp.107-114
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• 2017

터보차저는 배기가스로 구동되는 엔진 과급기를 말하며, 배기에너지를 이용하여 배기통로에 연결된 터빈의 회전력을 변화시켜, 혼합 가스의 충전효율을 높여 출력과 연비를 향상 시키는 부품이다. 이러한 목적에 따라 과급을 조절해주는 것이 중요하며, 핵심 부품 중 노즐 슬라이드 조인트가 있다. 소재는 현재 오스테나이트 계 스테인리스강으로 높은 내열성과 내식성 등의 우수한 기계적 성질을 이용하고 있다. 그러나 절삭성이 나쁘기 때문에 절삭가공에 의해 복잡한 형상의 제품을 만드는데 어려운 점이 많다. 현재 노즐 슬라이드 조인트의 가공방법은 금속분말 사출성형후 치수정밀도를 위해 절삭가공을 행하고 있다. 따라서 본 연구에서는 Nitronic 60을 이용하여 터보차저 과급유량을 조절해주는 노즐 슬라이드 조인트의 제작 공정에서 절삭가공이 필요 없는 정형가공 공정을 제안하기 위하여, 기계적 특징에 영향과 연관이 있는 소결온도, 제품의 응력 및 변형률, 형상과 관련이 있는 모따기 펀치각도 및 펀치의 곡률반경을 설계변수로 선정하였다. 그에 따라 유한요소해석과 실험계획법인 다구찌법 및 SN비를 이용하여 가장 좋은 공정 조건을 제안하였다. 최종제품과 유한요소해석 결과의 상대밀도 및 정수압을 비교하여 경향이 일치함을 알 수 있었다. 따라서 다구찌법을 이용한 금속분말의 성형공정 설계에 유용하게 적용할 수 있을 것으로 판단된다.

• 한국산학기술학회논문지
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• 제12권11호
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• pp.4745-4750
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• 2011

본 연구에서는 터보과급기 테스트 벤치, 실시간용 소프트웨어와 DAQ의 HIL 플랫폼, 그리고 Matlab/ Simulink로 작성한 엔진 모델로 구성된 HIL 시스템을 구축하고, HIL 시스템의 정상 작동 여부를 파악하기 위해 연료 공급량을 단계적으로 변화시키는 시뮬레이션을 수행하였다. 연료 공급량을 1.8944 kg/h와 4.7360 kg/h 사이에서 단계적으로 변화시키고, 시스템이 설정된 목표 공연비 32를 추종하는지 여부를 분석하였다. 시뮬레이션의 결과 연료 공급량을 변화시킨 상태에서 20초 정도의 시간이 경과한 후 설정된 목표 공연비에 정상적으로 수렴하였다. 또한 연료 공급량의 변화에 따라 터빈 베인 듀티비와 압축기의 부스트 압력도 적절하게 변화함을 확인하였다. 따라서 본 시스템은 터보과급기 개발 및 성능 개선에 유용하게 사용될 수 있을 것으로 기대된다.

• 한국자동차공학회논문집
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• 제24권1호
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• pp.33-38
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• 2016

The turbocharger is an essential component to realize the engine down-sizing. The moment of inertia of turbocharger rotor is an important parameter with respect to acceleration performance of the vehicle. It can be calculated from the CAD software based the geometry data and the material properties. But the accurate value of the inertia of turbocharger rotor must be measured through the experimental method. In this study, the measurement of moment of inertia of turbocharger rotor for 2.0 L spark-ignition engine was carried out. First, an experimental equipment using a trifilar method was designed and fabricated. Some optical devices, that is, photo sensor, counter, convex lens, etc, were used to increase the accuracy of the measurement. Second, error sensitivity for the equipment was analyzed. The error of period time and the radius can give big affects to the accuracy of the moment of inertia. When the amount of error of these two were each 1.0 %, maximum error of the moment of inertia was under 3.0 %. Third, the calibration for the equipment was performed using a calibration rotor which has similar shape to turbine rotor but simple. Calculated value from CAD software and measured one for the calibration rotor were compared. The total error of the equipment and the measurement is about 1.3 %. This result shows that the equipment can give the good result with resonable accuracy. Finally the moment of inertia of the turbine rotor and compressor wheel were measured. The coefficient of variations, the ratio of standard deviation to mean value, were reasonably small at 0.57 % and 0.73 % respectively. Therefore this equipment is suitable for the measurement of the moment of inertia of the turbine rotor and compressor wheel.

• 한국자동차공학회논문집
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• 제24권3호
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• pp.319-329
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• 2016

Globally, many researchers have been trying to improve the fuel economy of a vehicle for satisfying future $CO_2$ regulation and minimizing air pollution problem. For the same background, diesel engine and vehicle system optimization using simulation models have been key technologies for the improvement of vehicle system efficiency. Therefore, in this study, calibration method for the air breathing system of a WGT diesel engine using mean value model has been composed for efficient engine and vehicle optimization simulation researches. And virtual WGT performances have been calculated for a 2 cylinder downsized diesel engine system. From these researches, the calibration method for the boost pressure and EGR rate of a virtual diesel engine related with WGT performances could be composed and some of technical issue related with downsized diesel engine could be investigated.