• International Journal of Aeronautical and Space Sciences
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• 제1권2호
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• pp.22-29
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• 2000

A method to simulate the gas turbine transient behavior is developed. The basic principles of the method and main input data required are described. Calculation results are presented in terms of whole operating regime of the engine. The influence of initial parameters such as starting engine power, moment of inertia of the rotor, fuel schedule on performance characteristics of gas turbine during transient operation is shown. In addition, the effect of bleeding air on transient behavior is also considered. For validation of the developed computer code, a comparative analysis with experimental data obtained from a heavy duty gas turbine is made. Calculation results agree well with the experimental data for the range of operating regime studied and proved applicability of the developed technique to initial design stage of control system.

• 한국소음진동공학회:학술대회논문집
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• 한국소음진동공학회 2001년도 춘계학술대회논문집
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• pp.609-615
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• 2001

In this paper, the eigenvalue sensitivity of vehicle powertrain was investigated by analytic method. The powertrain system was considered as a rigid body with multiple engine mounts, and the engine mounts were supposed as three linear springs in three orthogonal directions. The design parameters for the sensitivity analysis were engine mount properties (positions, stiffness, and orientations) and powertrain properties (mass, second moment of inertia, and center of gravity). Firstly, an effective form of eigenvalue problem for the powertrain system was introduced. Then, the analytic sensitivity of eigenvalue was derived using the equation. Lastly, the derived sensitivity equation was applied to a real powertrain system to provide its correctness and applicability.

• 한국자동차공학회논문집
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• 제17권2호
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• pp.57-66
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• 2009

In this paper, the steering characteristics of tracked vehicles are studied for the improvement of steering performance. The important design factor of military vehicles is high mobility. It is influenced by weight of a vehicle, engine capacity, power-train, and steering system. The military vehicle, which is equipped with caterpillar, has unique steering characteristics and is quite different from that of a wheeled vehicle. The steering of tracked vehicles is operated in the power pack due to different speeds of both sprockets. Under cornering conditions, power split and power regeneration are happened in the power pack. In case of power regeneration, power is transferred outside track after adding engine power and power inputted inside track from the ground. However, excessive power regeneration is transferred in the power pack. It damages mechanical elements. Therefore, it is necessary to analyze the steering system and check mentioned problem above. In this study, the detailed dynamic model of steering system is presented, which includes slippage between track and roadwheel, inertia force, and inertia moment. Finally, our model is compared with the Kitano model and we verified the validity of the model.

• 한국자동차공학회논문집
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• 제6권1호
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• pp.90-98
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• 1998

A Dual Mass Flywheel(D.M.F.) system is an evolution to the reduction of torsional vibration and impact noise occurring in powertrain when a vehicle is either moving or idling. The D.M.F. system has two flywh-eels, which is different from the conventional clutch system. One section belongs to the mass moment of in-ertia of the engine-side. The other section increases the mass moment of inertia of the transmission-side. These two masses are connected via a spring/damping system. This reduces the speed at which the dreaded resonance occurs to below idle speed. Since 1984m D.M.F. system has been developed. However, the processes of development of D.M.F. system don't have any difference from the trial and error method of conventional clutch system. This paper present the method for systematical design of D.M.F. system with dimensionless design varia-bles of D.M.F. system, mass ratio between two flywheels, natural frequency rate of two flywheels, and visc-osity coefficient. And expermental results are used to prove these theoretical results.

• 한국생산제조학회지
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• 제6권3호
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• pp.96-102
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• 1997

Eigenvalue analysis of vibration mode and an analysis by frequency response among the methods of predicting gear noise are related with transmitting sound of vibration. In this study we intended to reduce the vibration noise of differential gear by reducing torque fluctuation of drive pinion shaft which causes vibration noise of differential gear in rear wheel drive vehicles. For this we developed multi-degree of freedom analysis model in which mass moment of inertia and torsional spring combined and we examined the influence of torsional vibration of driveline elements by performing forced vibration analysis of engine excitation torque. We studied the methods for reducing torsional vibration of driveline according to the design factor of propeller shaft and examined the effects reducing vibration in differential gear by applying flexible coupling.

• 소음진동
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• 제7권5호
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• pp.853-860
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• 1997

For this study, the multi-degree of freedom analysis model of torsional vibration was developed. This model is combined with mass moment of inertia and torsional spring in two wheel drive and four wheel drive vehicle. We compared and analyzed torsional vibration characteristics by natural frequencies and mode shapes which are obtained by free vibration analysis of this model. And we studied torsional vibration contribution of driveline elements by performing the forced vibration analysis of engine excitation torque. The validity of this model is demonstrated by the field test. The reduction effect of the torsional vibration along the driveline design factor is presented by the analytical results.

• 대한기계학회논문집
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• 제10권5호
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• pp.689-697
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• 1986

본 연구에서는 3자유도(3방향의 병진운동만 고려) 고무마운트모형의 타당성을 검증하기 위하여, 먼저 고무자체의 물성치인 강성계수와 감쇠계수를 진동수와 초기변 형률에 따라 실험을 통해 구하였다. 질량행렬의 모든요소를 쉽게 구할 수 있는 간단 한 시험구조물을 제작하고 여기에 고무아운트를 부착하여 6자유도를 갖는 모의 엔진- 마운트계를 구성한 후 가진실험을 통해 얻은 오무드 매개변수들과 고무의 물성치를 이 용한 컴퓨터 시뮬레이션의 결과를 비교함으로써 고무아운트 모형의 타당성을 검증하였 다. 특히 본 연구에는 유압가진 실험으로부터 얻은 실험결과를 바탕으로 고무의 강 성계수를 주파수의 1차함수로 고려한 경우와 전진동수 영역에서 균일하다고 가정하는 경우를 비교하였다.

• 한국소음진동공학회논문집
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• 제13권12호
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• pp.923-929
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• 2003

As for the marine propulsion shafting system using 4 stroke diesel engine, it is common to apply a reduction gear box between diesel engine and shafting to increase propulsion efficiency, which requires inevitably a certain elastic coupling to avoid chattering and hammering inside of gear box. In this study, the optimum method of rectifying propulsion shafting system in case of 750 ton fishing vessel is theoretically studied in a view of dynamic characteristics of torsion. After the replacement of diesel engine and gear box, the torsional vibration get worse and so some countermeasures are needed. The elastic coupling is modified from a present rubber coupling of block type having relatively high torsional stiffness to a rubber coupling haying two serially connected elements. Torsional vibration damper was installed at crankshaft free end additionally and moment of inertia of flywheel was adjusted. The dynamic characteristics of shafting system was improved by these modification. The theoretical analysis of torsional vibration are compared to measurement results using two laser torsion meters during the sea trial.

• 한국추진공학회지
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• 제11권3호
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• pp.20-28
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• 2007

압축기의 써지 현상을 관찰하는 가장 쉬운 방법의 하나로는 부분품의 성능특성도상에 정적 그리고 동적 운용 특성을 나타내는 것이 될 수 있다. 이 경우 엔진의 작동범위가 써지 범위에 의하여 제한될 것이고 따라서 엔진은 엔진의 정적 또는 과도 성능의 전 과정에 걸쳐 일정한 써지 한계를 갖도록 요구되고 있다. 로터의 극관성 모멘트, 닥트 내 공기/가스의 용적 그리고 열전달 효과 등은 엔진의 작동이 정적 특성으로부터 일탈하게 되는 주요 요소들이다. 시스템 내에서 열교환기가 존재하는 경우처럼 큰 용적의 경우 그것은 동적 작동 특성에 상당한 영향을 주게 될 것인데 본 논문에서는 보조동력기관으로 사용되는 마이크로터빈의 예를 들어 엔진의 과도성능 특성에 압축기의 출구에서 추출되는 냉각공기가 미치는 영향을 조사코자 하였다. 질량 및 일 그리고 회전수 일치 법칙에 근거하여 터빈을 흐르는 가스 유량, 압력비, 회전 속도, 동력 그리고 모멘트가 계산되었다. 본 연구의 결과는 제어시스템 설계를 위한 기초 자료로 활용될 수 있을 것이다. 이러한 과도 성능을 계산하기 위한 프로그램을 개발을 위해서 상업용 MathCAD 소프트웨어를 사용하였다.

• Journal of Advanced Marine Engineering and Technology
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• 제40권9호
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• pp.743-748
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• 2016

선박의 주기관으로 통상 사용되는 디젤기관은 터빈기관과 같은 회전기관과 달리 왕복동기관이기 때문에 실린더의 폭발력과 피스톤의 왕복관성력에 의한 불평형 관성력 및 관성모멘트, 실린더내의 주기적인 변동가스압력 등으로 인하여 본질적인 진동문제를 안고 있다. 이것은 엔진의 진동은 소음의 원인이 되고, 선체구조나 인접구조물에 전달되어 2차진동이 발생시키는 경우가 많다. 본 연구는 선박의 엔진과 축계의 자유진동해석과 엔진 폭발에 의한 강제진동해석을 하고, 나아가서 플라이휠에 부진동 장치인 동흡진기를 설치하여 진동을 줄이는 방법을 제안하고자 한다.