• International Journal of Precision Engineering and Manufacturing
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• 제4권5호
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• pp.34-40
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• 2003

This paper presents the inertial force problem of ultrahigh-speed injection molding machine using linear motors, and presents its solutions. To make very thin products by injection molding, very high injection speed is required, and linear motors are used for this purpose. However, direct drive by linear motors may cause brief nozzle separation from the sprue bushing because of the inertia force which is as large as the total output thrust of the linear motors, and this momentary separation can cause molten plastic to leak. In this paper, two solutions are proposed for this inertia force problem. One is the mechanical cancellation of the inertia force, and the other is to increase the nozzle contact force. With the latter solution, the stationary platen bending worsens, so a new nozzle contact mechanism is also proposed, which can prevent the stationary platen bending.

• International Journal of Aeronautical and Space Sciences
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• 제7권2호
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• pp.86-103
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• 2006

Using a combination of force transducer measurement to quantify net lift force, high frame rate camera to quantify and subtract inertial contributions, and Digital Particle Image Velocimetry (DPIV) to calculate aerodynamic contributions in the spanwise plane, the contribution of spanwise flow to the generation of lift force in wings undergoing a pure flapping motion in hover is shown as a function of flapping angle throughout the flapping cycle. These experiments were repeated at various flapping frequencies and for various wing planform sizes for flat plate and span wise cambered wings. Despite the previous identification of the importance of span wise fluid structures in the generation of lift force in flapping wings throughout the existing body of literature, the direct contribution of spanwise flow to lift force generated has not previously been quantified. Therefore, in the same manner as commonly applied to investigate the chordwise lift distribution across an airfoil in flapping wings, spanwise flow due to bulk flow and rotational fluid dynamic mechanisms will be investigated to validate the existence of a direct component of the lift force originating from the flapping motion in the spanwise plane instead.

• 한국정밀공학회지
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• 제19권10호
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• pp.171-177
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• 2002

This paper presents the inertial force problem of ultrahigh-speed injection molding machine using linear motors, and presents its solutions. To make very thin products by injection molding, very high injection speed is required, and linear motors are used for this purpose. But direct drive by linear motors may cause brief nozzle separation from the sprue bushing because of the inertia force as large as the total output thrust of the linear motors, and this momentary separation can cause molten plastic leakage. In this paper, two solutions are proposed for this inertia force problem. One is the mechanical cancellation of the inertia force, and the other to increase the nozzle contact force. With the latter solution, the stationary platen bending worsens, so a new nozzle contact mechanism is also proposed, which can prevent the stationary platen bending.

• 제어로봇시스템학회논문지
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• 제7권2호
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• pp.160-167
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• 2001

This paper presents control and evaluation of a new haptic device with a 6-DOF parallel mechanism for interfacing with virtual reality. This haptic device has low inertial, high bandwidth compactness, and high output force capability mainly due to of base-fixed motors. It has also wider orientation workspace mainly due to a RRR type spherical joint. A control method is presented with gravity compensation and with force feedback by an F/T sensor to compensate for the effects of unmodeled dynamics such as friction and inertia. Also, dynamic performance has been evaluated by experiments. for force characteristics such as maximum applicable force, static-friction force, minimum controllable force, and force bandwidth Virtual wall simulation with the developed haptic device has been demonstrated.

• 한국해양공학회지
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• 제29권6호
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• pp.436-444
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• 2015

A submerged body is sensitive to changes in the roll moment because of the small restoring moment and moment of inertia. Thus, a method for predicting the roll-related hydrodynamic coefficients is important. This paper describes a deduction method for the hydrodynamic coefficients based on the results of a coning motion test. A resistance test, static drift test, and coning motion test were performed to obtain the coefficients in the towing tank of Seoul National University. The sum of the hydrodynamic force, inertial force, gravity, and buoyancy was measured in the coning motion test. The hydrodynamic force was deduced by subtracting the inertial force, gravity, and buoyancy from the measured force. The hydrodynamic coefficients were deduced using the regression method.

• 한국해양학회지
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• 제17권2호
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• pp.41-50
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• 1982

수평적으로 무한히 넓은 천해에 시간에 따라 크기와 방향이 바뀌는 바람이 불 때의 해수의 유량transports)에 대한 이론적인 계산을 할 수 있는 모델을 만들 었다. 이 모델에서 사용하는 선형화된 이론식은 가속력, 편향력(Coriolis force), 바람의 응력(wind stress) 및 저면 마찰력을 포함하고 있으며, 이 모델로부터 해수 유량에 대한 다음과 같은 결과를 얻었다. 일정한 바람이 계속 불 때의 해수유량은 해저면 마찰로 인하여 바람 오른쪽 방향 90 보다 작다. 바람이 불기 시작한 후의 천이상태(transient state)의 유량은 정상류적(steady)인 에크만류( Ekman current) 에다가 시간이 지남에 따라서 크기가 감소하는 관성진동(inertial oscillation)과의 합성으로 나타난다. 바람의 크기가 정현적(sinrsoidal)으로 바뀌는 경우는 유량 벡터 는 바람 변화의 주기와 같은 시간동안 일주회전을 하는 유량타원(transport ellipse) 을 그린다. 바람의 방향이 바뀔 경우 해수유량은 자유관성진동(free inertial oscillation)과 강제진동의 합으로 나타나는데, 이 경우 강제진동의 주기는 바람 방향의 회전주기(rotation period)와 같다. 이 이론적인 해수유량모델은 해에서 시간에 따라 바람이 바뀔 경우 해수와 영양염의 이동에 대한 해석을 하는데 유용 하다.

• 한국지반공학회논문집
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• 제38권6호
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• pp.17-28
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• 2022

동적 하중 재하시 지반-구조물 상호작용 확인을 위해 진동대 실험이 많이 시행됐으나, 대부분 단자유도 상부 구조물과 단말뚝을 적용한 진동대 실험이 주를 이루고 있다. 이에 본 연구에서는 다자유도 구조물과 군말뚝을 적용한 대형진동대 실험을 통해, 상부 구조물의 관성 상호작용 영향을 분석하였다. 실험 결과, 단일 진동수에서의 증폭 경향을 나타내는 단자유도 구조물과는 다르게 다자유도 구조물에서는 다수의 진동수 구간에서 시간-가속도 발생 경향 및 응답 주파수의 유사성과 증폭 경향이 나타났다. 또한, 벽체 구조물에 비하여 기둥 구조물에서의 기초판과 상부 구조물과의 증폭현상이 더 크게 발생하여 기둥 구조물에 의한 관성 상호작용 효과가 더 큰 것으로 판단된다. 그리고 기초판에서의 전단력 및 관성력 관계, 상대 수직 변위 및 상대 수평 변위 관계와 심도별 동적 p-y 곡선에 대한 분석을 수행하였다. 분석 결과, 다자유도 구조물에서는 단자유도 구조물과는 상이한 거동을 나타내고 있으며, 벽체보다 기둥 구조물의 관성 상호작용의 효과가 더 큰 것으로 나타났다.

• Wind and Structures
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• 제9권4호
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• pp.315-330
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• 2006

Flow and scalar dispersion around Cheomseongdae are numerically investigated using a three-dimensional computational fluid dynamics (CFD) model with the renormalization group (RNG) $k-{\varepsilon}$ turbulence closure scheme. Cheomseongdae is an ancient astronomical observatory in Gyeongju, Korea, and is chosen as a model obstacle because of its unique shape, that is, a cylinder-shaped architectural structure with its radius varying with height. An interesting feature found is a mid-height saddle point behind Cheomseongdae. Different obstacle shapes and corresponding flow convergences help to explain the presence of the saddle point. The predicted size of recirculation zone formed behind Cheomseongdae increases with increasing ambient wind speed and decreases with increasing ambient turbulence intensity. The relative roles of inertial and eddy forces in producing cavity flow zones around an obstacle are conceptually presented. An increase in inertial force promotes flow separation. Consequently, cavity flow zones around the obstacle expand and flow reattachment occurs farther downwind. An increase in eddy force weakens flow separation by mixing momentum there. This results in the contraction of cavity flow zones and flow reattachment occurs less far downwind. An increase in ambient wind speed lowers predicted scalar concentration. An increase in ambient turbulence intensity lowers predicted maximum scalar concentration and acts to distribute scalars evenly.

• 한국소음진동공학회:학술대회논문집
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• 한국소음진동공학회 2005년도 추계학술대회논문집
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• pp.744-749
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• 2005

In this paper, a lens actuator for mobile devices is proposed using stack type piezoelectric materials. In general, the deformation of PZT actuators is not enough for lens motion when the allowed voltage is applied. The small stroke problem can be solved by accumulating a lot of small displacements in high frequency. In this paper, a new inch-worm type model for focusing actuator is suggested based on the interaction of inertial and frictional forces. Theoretical analysis and simulation using ANSYS are performed to verify the feasibility of the inch-worm PZT actuator model. Various types of clamps are considered to determine the effect of frictional force on the motion, and appropriate clamp-actuator models are proposed. The proposed models are experimentally verified and the experimental results show high correspondence with theoretical and simulated values. The inch-worm type focusing actuator enable a large stroke with 7.79 mm/sec with 10kHz and 10V.

• Structural Engineering and Mechanics
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• 제81권5호
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• pp.633-645
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• 2022

The active tuned mass damper (ATMD) is an efficient and reliable structural control system for mitigating the dynamic response of structures. The inertial force that an ATMD exerts on a structure to attenuate its otherwise large kinetic energy and undesirable vibrations and displacements is proportional to its excursion. Achieving a balance between the inertial force and excursion requires a control law or feedback mechanism. This study presents a technique for the optimum design of a sliding mode controller (SMC) as the control law for ATMD-equipped structures subjected to earthquakes. The technique includes optimizing an SMC under an artificial earthquake followed by testing its performance under real earthquakes. The SMC of a real 11-story shear building is optimized to demonstrate the technique, and its performance in mitigating the displacements of the building under benchmark near- and far-fault earthquakes is compared against that of a few other techniques (proportional-integral-derivative [PID], linear-quadratic regulator [LQR], and fuzzy logic control [FLC]). Results indicate that the optimum SMC outperforms PID and LQR and exhibits performance comparable to that of FLC in reducing displacements.