• Title/Summary/Keyword: shock Load

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A Quality Stability Estimation of Shock-absorber Tube for automatic drawer (자동서랍함용 완충기 튜브의 품질 안정성 예측)

  • Son, Jae-Hwan;Kim, Young-Suk;Han, Chang-Woo
    • Journal of the Korea Academia-Industrial cooperation Society
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    • v.12 no.7
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    • pp.2919-2924
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    • 2011
  • The automatic drawer is used to absorb the movement shock and adjust its velocity when it opens and closes. The tube in shock-absorber is the cylindrical case which surrounds its parts and is made of acetal. The purpose of this study is to determine the quality stability of the tube in the shock-absorber in injection molding process. The tube which had been manufactured in the process with 4 cavity cooling unit was used. In this study, the analysis and test are carried out to determine its quality stability. Which are the quality analysis with numerical simulation and performance tests of the tube compared with one of foreign make. It is calculated that the injection press is 87.6 MPa and the deflections in X, Y, Z directions are ranged in 0.07~1.00 mm. When the researched tube is compared with the foreign made tube, the maximum bending compressive load is 231 kgf higher, average axial compressive load is 0.05 kgf higher, and the roughness(Ra) on the inner surface is $0.02\;{\mu}m$. lower. In the result, it is known that the quality of researched tube in injection mold process is stable and its performance is superior.

Compensation of Inclined Rotating Axis Using Unsymmetric Groove Patterns (비대칭 Groove를 이용한 FDB 회전축의 기울기 보상)

  • Lee, Nam-Hun;Han, Jae-Hyuk;Oh, Dong-Ho;Kim, Chul-Soon;Byun, Yong-Kyu;Koo, J.C.
    • Proceedings of the Korean Society for Noise and Vibration Engineering Conference
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    • 2004.11a
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    • pp.582-585
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    • 2004
  • Most of hard disk drives currently employ fluid dynamic bearing (FDB) for their rotor support. Stiffness of the FDB is affected by many design factors such as bearing clearance, fluid viscosity, and rotational speed. For the high rotating speed HDDs stiffness of the rotor is normally high enough to accomodate load disturbances. However small form factor HDDs that are to be operated in low power consumption are often designed with low stiffness rotors. Although the low stiffness rotor clearly benefits low power operation, it could damage the entire motor structure or head disk interface even by a light mechanical load disturbance such as shock or vibration. In addition, since a single channel HDD does not provide gram load equilibrium in axial direction the rotor could be tilted and make a hard contact to stator. A non-symmetric groove pattern could successfully compensate the tilted rotor angle during operation.

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자동차용 충격흡수기의 튜브 스피닝 공정 해석

  • 김영호;박재우;조호성
    • Journal of the Korean Society for Precision Engineering
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    • v.17 no.3
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    • pp.33-38
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    • 2000
  • In process of tube spinning far shock absorber on vehicles, the selection of feed rate and rounding radius of forming roller and revolution speed of tube and forming roller, forming gap between die and forming roller are very important factors to obtain the optimal process result. In this paper, rigid-plastic FEM and UBET analysis are applied to verify effect of each factors by forming load. We can obtain the optimal conditions to prevent defects during processing.

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A Study of the Control System for a Auto Loadsharing of the ship (선내 자동 부하분담 제어시스템에 관한 연구)

  • Lee, Hyo-Sung;Lim, Yong-Kon;Lee, Heung-Ho
    • Proceedings of the KIEE Conference
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    • 2005.07d
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    • pp.3025-3027
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    • 2005
  • As the energy and manpower saving in ship have been prominent figures since oil shock, resonable operation modes of propulsion and generating plants were made a through study for the practical use. Through the results of it, advanced countries developed the load-sharing system for the generator automation and could be realized the energy and manpower saving in ship.

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Experimental Study on Various Ramp Profiles during Unloading Process (초소형 HDD의 언로딩 과정에서 램프 형상에 대한 실험 연구)

  • Lee, Young-Hyun;Park, Kyoung-Su;Park, No-Cheol;Yang, Hyun-Seok;Park, Young-Pil
    • Proceedings of the Korean Society for Noise and Vibration Engineering Conference
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    • 2005.11a
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    • pp.314-317
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    • 2005
  • There are many benefits such as increased areal density, reduced power consumption, applied smaller size and improved shock resistance in Load/Unload(L/UL) mechanism. It has been the key technology of developing small form factor hard disk drive used in portable digital devices. The main objectives of L/UL are no slider-disk contact and faster L/UL process. For realizing those, we must consider many design parameters in L/UL systems. In this paper, we focus on the effects of ramp profile. We can investigate dynamic characteristics of suspension tap and slider on ramp during unloading process experimentally. In special, we examine the effects of vortical velocities, ramp slopes and disk vibrations. As the result of these experiments, we propose design criteria of advanced ramp profile for good unloading performance.

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Effect of magnetic field and gravity on thermoelastic fiber-reinforced with memory-dependent derivative

  • Mohamed I.A. Othman;Samia M. Said;Elsayed M. Abd-Elaziz
    • Advances in materials Research
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    • v.12 no.2
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    • pp.101-118
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    • 2023
  • The purpose of this paper is to study the effects of magnetic field and gravitational field on fiber-reinforced thermoelastic medium with memory-dependent derivative. Three-phase-lag model of thermoelasticity (3PHL) is used to study the plane waves in a fiber-reinforced magneto-thermoelastic material with memory-dependent derivative. A gravitating magneto-thermoelastic two-dimensional substrate is influenced by both thermal shock and mechanical loads at the free surface. Analytical expressions of the considered variables are obtained by using Laplace-Fourier transforms technique with the eigenvalue approach technique. A numerical example is considered to illustrate graphically the effects of the magnetic field, gravitational field and two types of mechanical loads(continuous load and impact load).

Structural Design of Planar Synthetic Aperture Radar (SAR) Antenna for Microsatellites

  • Dong-Guk Kim;Sung-Woo Park;Jong-Pil Kim;Hwa-Young Jung;Yu-Ri Lee;Eung-Noh You;Hee Keun Cho;Jin Hyo An;Goo-Hwan Shin
    • Journal of Astronomy and Space Sciences
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    • v.40 no.4
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    • pp.225-235
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    • 2023
  • This paper presents the structural design of a planar synthetic aperture radar (SAR) antenna applied to a microsatellite. For micro-satellite applications, the SAR antenna structure must be lightweight, flat, and designed to withstand the launch environment. To satisfy these conditions, our novel antenna structure was designed using aluminium (AL) alloy. Structural analysis was performed for quasi-static load, random vibration, and shock load to verify its robustness in the launch environment, and the results are presented here.

Indirect Load Identification for the Operational Load Analysis (동작중 작용부하 분석을 위한 간접적 부하규명)

  • Cho M. S.
    • Journal of Biomedical Engineering Research
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    • v.24 no.6 s.81
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    • pp.501-507
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    • 2003
  • Medical devices for helping the rehabilitation of the patients such as orthoses and prostheses should be designed to be strong enough. For the strength design, operational load should be identified first. Furthermore. medical devices are susceptible to dynamic load or shock frequently due to its characteristics. These type of the load may be identified by installing the sensors directly. However, it can modify the natural properties of the structures. Therefore, operational load should be identified indirectly from the system characteristics and responses such as vibrations. In this paper, the basic formulation of the indirect load identification is reviewed and the problems of conventional approach are checked. Then, the new approach based upon the principal component analysis is proposed and the validity of the proposed method is demonstrated using experiments.

Performance Prediction of Landing Gear Considering Uncertain Operating Parameters (운용 파라미터의 불확실성을 고려한 착륙장치 완충성능 해석)

  • Kim, Tae Uk
    • Transactions of the Korean Society of Mechanical Engineers A
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    • v.37 no.7
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    • pp.921-927
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    • 2013
  • The performance estimation of a landing gear with uncertain parameters is presented. In actual use, many parameters can have certain degrees of variations that affect the energy absorbing performance. For example, the shock strut gas pressure, oil volume, tire pressure, and temperature can deviate from their nominal values. The objective function in this study is the ground reaction during touchdown, which is a function of the abovementioned parameters and time. To consider the uncertain properties, convex modeling and interval analysis are used to calculatethe objective function. The numerical results show that the ground reaction characteristics are quite different from those of the deterministic method. The peak load, which affects the efficiency and structural integrity, is increases considerably when the uncertainties are considered. Therefore, it is important to consider the uncertainties, and the proposed methodology can serve as an efficient method to estimate the effect of such uncertainties.