• Proceedings of the Korean Society for Technology of Plasticity Conference
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• 2003.10c
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• pp.28-37
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• 2003

• Proceedings of the Korean Society for Technology of Plasticity Conference
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• 2003.05a
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• pp.199-203
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• 2003

Idler of excavator are large product with diameter 500 - 600 mm and parts of a power transmit device. The object of the paper is developed large products by hot closed-die forging. The forging process which is proposed from numerical analysis and various tests is developed a large products with good quality. To estimate the design process parameters such as working load, temperature and flash thickness so on, numerical analysis are used by DEFORM 2D. To obtain a flow stress data and optimal forging temperature is carried out hot compression and tensile test at a various temperature range. Developed product is tested mechanical properties of elongation, hardness and tensile strength so on. Test results are presented excellent mechanical properties.

• Proceedings of the Korean Society for Noise and Vibration Engineering Conference
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• 1995.04a
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• pp.307-312
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• 1995

장거리 시스템의 경우에 있어서 기동과 정지 시의 동적하중은 구동부 입력크기의 변화와 구동부간이 기동 시간차이로부터 발생되며, 벨트로 전파되어 장력변화를 일으키고, 과도한 장력의 변화는 인장과 압축의 탄성파로 벨트요소의 응력을 증가시키며, 벨트, 풀리, 아이들러(idler)등의 벨트요소들을 파괴시킨다. 따라서 동적해석에 의한 설계가 필수적으로 요구되어 벨트의 동적거동 해석에 대한 연구가 많이 수행되고 있다. 본 연구에서는 벨트 컨베이어 시스템을 집중질량모델(lumped mass model)로 근사하여 모델링하는 방법을 도입하여 세부요소에 대한 운동방정식을 유도하고, 각 요소 모델링을 결합하여 전체 운동방정식을 수립하였으며, 예제 시스템에 적용하여 동적거동을 해석하였다. 예제 시스템에 있어서 기동시의 구동입력을 두 가지 형태의 입력을 이용하였고, 정지시에는 구동부 브레이크가 없는 경우로 정상운전상태에서 순간적으로 구동부의 동력을 제거하는 방법을 적용하였다. 시뮬레이션 결과를 통하여 기동시의 구동입력을 적절히 제어하므로 벨트 속도와 장력의 변화를 줄일 수 있는 입력형태를 결정할 수 있었고, 이 때의 테이크업의 운동도 구할 수 있었다.

• Transactions of the Korean Society of Automotive Engineers
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• v.6 no.4
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• pp.24-31
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• 1998

In this study, a procedure is presented for the dynamic analysis of a multibody tracked vehicle system. The planar vehicle model used in this investigation is assumed to consist of two kinematically decoupled subsystems. i.e., the chassis subsystem and track subsystem. The chassis subsystem includes the chassis frame, sprocket, idler and rollers, while the track subsystem is represented as a closed kinematic chain consisting of rigid links interconnected by revolute joints. The nonlinear contact force modules describing the interaction between track links, and sprocket, idler, rollers and ground will be developed.

• Journal of the Korean Society for Precision Engineering
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• v.19 no.2
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• pp.140-150
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• 2002

The planar tracked vehicle model used in this investigation consists of two kinematically decoupled subsystems, i.e., the chassis subsystem and the track subsystem. The chassis subsystem includes the chassis frame, sprocket, idler and rollers, while the track subsystem is represented as a closed kinematic chain consisting of rigid links interconnected by revolute joints. In this study, the recursive kinematic and dynamic formulation of the tracked vehicle is used to find the vertical terce and the distance of an arbitrary track moved in the driving direction along the track. These distances and vertical forces obtained are used to get the deformation and sinkage of a terrain. The FEM(Finite Element Method) is adopted to analyze the interaction between tracked vehicle and terrain. The terrain is represented by a system of elements wish specified constitutive relationships and considered as a piecewise linear elastic, plastic and isotropic material. When the tracked vehicle is moving with different speeds on the terrain, the elastic and plastic deformations and the maximum sinkage for the four different types of isotropic soils are simulated.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2003.10a
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• pp.257-260
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• 2003

Dynamic simulation program for a smart UAV turbojet engine was developed. The transient simulation program utilized the CMP(Constant Mass flow) method and Euler integration method for integration of excess torque. The transient performance analysis was carried out by increasing from the idle to the maximum rotational speed of the gas generator. To observe engine dynamic behavior, fuel flow was monitored through a step and a ramp increase. When the fuel was increased as a step function the overshoot of the turbine inlet temperature exceeded the limit temperature.