• 제목/요약/키워드: Contact Impact

검색결과 713건 처리시간 0.027초

Influence of mass and contact surface on pounding response of RC structures

  • Khatiwada, Sushil;Larkin, Tam;Chouw, Nawawi
    • Earthquakes and Structures
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    • 제7권3호
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    • pp.385-400
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    • 2014
  • Pounding damage to bridges and buildings is observed in most major earthquakes. The damage mainly occurs in reinforced concrete slabs, e.g. building floors and bridge decks. This study presents the results from pounding of reinforced concrete slabs. A parametric investigation was conducted involving the mass of the pendulums, the relative velocities of impact and the geometry of the contact surface. The effect of these parameters on the coefficient of restitution and peak impact acceleration is shown. In contrast to predictions from numerical force models, it was observed that peak acceleration is independent of mass. The coefficient of restitution is affected by the impact velocity, total participating mass and the mass ratio of striker and struck block.

Contact Frce Cotrol of Root Hnd using VSS

  • Sim, Kwee-Bo;Hashimoto, Hideki;Harashima, Fumio
    • 제어로봇시스템학회:학술대회논문집
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    • 제어로봇시스템학회 1989년도 한국자동제어학술회의논문집; Seoul, Korea; 27-28 Oct. 1989
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    • pp.1080-1084
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    • 1989
  • The motion of an workpiece to be manipulated is determined by the forces applied to the workpiece. During the contact between the robot hand and the workpiece, impulsive forces may dominate all other forces, and determine the ultimate success or failure of a task. Therefore, one of the important problems in the robot hands is the control of the initial impact force. In this paper, the problem of the force control of robot hand under system with contact force is presented. The principle of energy can be applied in the modelling of the impact force. In order to achieve stable contact and avoid bounces and vibrations, VSS is adopted in the design of the contact force controller. Some simulations are carried out for a pushing operation to control the contact force.

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열차 충돌하중에 대한 콘크리트 일탈방호시설물(DCP)의 해석적 거동 검토 (Analytical Behavior of Concrete Derailment Containment Provision(DCP) according to Train Impact Loading)

  • 이나현;김지환;강윤석
    • 한국산학기술학회논문지
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    • 제19권11호
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    • pp.604-613
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    • 2018
  • 전 세계적으로 철도의 노후화 및 고속화 등으로 인한 열차탈선사고가 증가하고 있으며, 그로인한 인적 물적 피해가 증가하고 있는 실정이다. 특히 철도교량의 경우에는 가드레일 또는 방호벽 등을 설치하고 있으나, 이는 탈선열차차량(train body level)이 방호벽과 충돌함으로써 열차의 탈선운동을 억제하여 정지시키는데 목적이 있다. 이와 같은 차량에 의한 탈선방호는 인명피해 위험성 및 2차 피해발생 가능성이 높다. 그러므로 본 연구에서는 주행레일 사이에 일탈방호시설물(DCP, Derailment Containment Provision)을 설치하여, 차륜 또는 차축(wheel/bogie level)에서 탈선열차를 방호할 수 있는 시설물을 개발하였다. 또한, 기존 철도교량의 일탈방호성능을 확보할 수 있도록 DCP의 급속시공이 가능하도록 설계하였으며, 방호벽에 작용하는 충돌하중과 급곡선부에서의 관성력을 감소시킴으로써 일탈된 열차가 교량 밖으로의 전도 낙하방지 및 반대편 선로의 침입하는 것을 최소화 하고자 하였다. 본 논문에서는 LS-Dyna을 이용하여, 설계한 DCP의 열차 충돌위치 및 콘크리트 궤도 접합조건에 따른 거동에 대하여 해석적으로 변수연구를 수행하였다. 특히 접합조건은 접합재료의 물성치에 따라 끊어짐을 모사하는 Tiebreak contact과 완전 부착되었다고 가정하는 Perfect bond contact으로 나눠 해석적으로 검토하였다. DCP의 변위, 앵커 및 콘크리트의 응력, 변형률을 확인한 결과 Tiebreak contact이 실제 충돌하중에 대한 거동을 보다 유사하게 모사하는 것으로 판단하였다. 또한, 충돌위치에 따른 변위는 접합구간에서 가장 큰 변형이 발생하였으며, DCP 블록의 중앙에 충돌이 가해질 경우, 충돌하중이 가해지는 DCP 배면에서 휨 파괴가 발생하였다. 본 연구에서 수행한 충돌해석은 실제 충돌실험의 어려움에 의해 사전적으로 해석을 수행하였으며, 이를 바탕으로 DCP 앵커 설계변경은 필요할 것으로 판단된다.

Nonlinear low-velocity impact of graphene platelet-reinforced metal foam beam with geometrical imperfection

  • Yi-Han Cheng;Gui-Lin She
    • Steel and Composite Structures
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    • 제52권6호
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    • pp.609-620
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    • 2024
  • The impact problem of imperfect beams is crucial in engineering fields such as water conservancy and transportation. In this paper, the low velocity impact of graphene reinforced metal foam beams with geometric defects is studied for the first time. Firstly, an improved Hertz contact theory is adopted to construct an accurate model of the contact force during the impact process, while establishing the initial conditions of the system. Subsequently, the classical theory was used to model the defective beam, and the motion equation was derived using Hamilton's principle. Then, the Galerkin method is applied to discretize the equation, and the Runge Kutta method is used for numerical analysis to obtain the dynamic response curve. Finally, convergence validation and comparison with existing literature are conducted. In addition, a detailed analysis was conducted on the sensitivity of various parameters, including graphene sheet (GPL) distribution pattern and mass fraction, porosity distribution type and coefficient, geometric dimensions of the beam, damping, prestress, and initial geometric defects of the beam. The results revealed a strong inhibitory effect of initial geometric defects on the impact response of beams.

Low velocity impact response and dynamic stresses of thick high order laminated composite truncated sandwich conical shell based on a new TDOF spring-mass-damper model considering structural damping

  • Azizi, A.;Khalili, S.M.R.;Fard, K. Malekzadeh
    • Steel and Composite Structures
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    • 제26권6호
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    • pp.771-791
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    • 2018
  • This paper deals with the low velocity impact response and dynamic stresses of composite sandwich truncated conical shells (STCS) with compressible or incompressible core. Impacts are assumed to occur normally over the top face-sheet and the interaction between the impactor and the structure is simulated using a new equivalent three-degree-of-freedom (TDOF) spring-mass-damper (SMD) model. The displacement fields of core and face sheets are considered by higher order and first order shear deformation theory (FSDT), respectively. Considering continuity boundary conditions between the layers, the motion equations are derived based on Hamilton's principal incorporating the curvature, in-plane stress of the core and the structural damping effects based on Kelvin-Voigt model. In order to obtain the contact force, the displacement histories and the dynamic stresses, the differential quadrature method (DQM) is used. The effects of different parameters such as number of the layers of the face sheets, boundary conditions, semi vertex angle of the cone, impact velocity of impactor, trapezoidal shape and in-plane stresses of the core are examined on the low velocity impact response of STCS. Comparison of the present results with those reported by other researchers, confirms the accuracy of the present method. Numerical results show that increasing the impact velocity of the impactor yields to increases in the maximum contact force and deflection, while the contact duration is decreased. In addition, the normal stresses induced in top layer are higher than bottom layer since the top layer is subjected to impact load. Furthermore, with considering structural damping, the contact force and dynamic deflection decrees.

선형 Magnetostatic 작동기의 정밀 접촉력제어를 위한 최적제어기 설계 (Optimal contact force control for a linear magnetostatic actuator)

  • 강희석
    • 제어로봇시스템학회:학술대회논문집
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    • 제어로봇시스템학회 1997년도 한국자동제어학술회의논문집; 한국전력공사 서울연수원; 17-18 Oct. 1997
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    • pp.272-275
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    • 1997
  • When a manipulator makes contact with an object having position uncertainty, performance measures vary considerably with the control law. To achieve the optimal solution for this problem, an unique objective function that weights time and impact force is suggested and is solved with the help of variational calculus. The resulting optimal velocity profile is then modified to define a sliding mode for the impact and force control. The sliding mode control technique is used to achieve the desired performance. Sets of experiments are performed, which show superior performance compared to any existing controller.

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곡률을 가진 적층복합재 구조에서의 저속충격손상 평가 (Damage Assessment of Curved Composite Laminate Structures Subjected to Low-Velocity Impact)

  • 전정규;권오양
    • 한국복합재료학회:학술대회논문집
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    • 한국복합재료학회 2001년도 춘계학술발표대회 논문집
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    • pp.69-73
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    • 2001
  • Damage induced by low-velocity impact on the curved composite laminates was experimentally evaluated for CFRP cylindrical shells with the radius of curvatures of 50, 150, 300, and 500 mm. The result was then compared with that of flat laminates. The radius of curvatures and the effective shell stiffness appeared to considerably affect the dynamic impact response of curved shells. Under the same impact energy level, the maximum contact force increased with the decreasing radius of curvatures, with reaching 1.5 times that for plates at the radius of curvature of 50 mm. Since the maximum contact force is directly related to the impact damage, curved laminates can be more susceptible to delamination and less resistant to the low-velocity impact damage. The distribution of delamination along the thickness direction of curved laminates are also different from that of flat plates. Delamination was distributed rather even]y at each interface along the thickness direction of curved laminates. This implies that the effect of curvatures has to be considered for the design of a curved composite laminate.

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볼 충격을 받는 유리의 콘크랙형성에 대한 경계조건의 영향 (The Effects of Boundary Condition in Cone Crack Formation of Soda-lime Glass by Ball Impact)

  • 김문생;허진;이현철;김호종
    • 대한기계학회논문집A
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    • 제27권6호
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    • pp.981-986
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    • 2003
  • In order to investigate the possibility of processing of brittle material by ball impact, the effects of boundary conditions about impact damage of soda-lime glass by small spheres were evaluated experimentally. It was investigated that crack appearance developed in soda-lime glass with boundary conditions of without sealing, single-sealing and double-sealing by impact velocity. The double-sealing was most effective in the development of perfect cone than other boundary condition. In case of double-sealing condition, PVC and Polyurethane sealing were more effective in producing a perfect cone formation than other sealing materials. The impact velocity range over which perfect cones were formed was influenced by both the contact area and diameter of impact particle.

Nonlinear low-velocity impact response of graphene platelets reinforced metal foams doubly curved shells

  • Hao-Xuan Ding;Yi-Wen Zhang;Yin-Ping Li;Gui-Lin She
    • Steel and Composite Structures
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    • 제49권3호
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    • pp.281-291
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    • 2023
  • Due to the fact that the nonlinear low-velocity impact response of graphene platelets reinforced metal foams (GPLRMF) doubly curved shells have not been investigated in the existing works, this paper aims to solve this issue. Using Reddy's high-order shear deformation theory (HSDT), the nonlinear governing equations of GPLRMF doubly curved shells are obtained by Euler-Lagrange method, discretized by Galerkin principle, and solved by the fourth-order Runge-Kutta method to obtain the impact force and central deflection. The nonlinear Hertz contact law is applied to determine the contact force. Finally, the impacts of graphene platelets (GPLs) distribution pattern, porosity distribution form, porosity coefficient, damping coefficient, impact parameters (radius and initial velocity), GPLs weight fraction, pre-stressing force and different shell types on the low-velocity impact curves are analyzed. It can be found that, among the four shell structures, the impact resistance of spherical shell is the best, while that of cylindrical shell is the worst.

이족 보행 로봇을 위한 빠르고 안전한 접촉 생성 전략 (Fast and Safe Contact Establishment Strategy for Biped Walking Robot)

  • 이호상;정재석;안준휘;박재흥
    • 로봇학회논문지
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    • 제16권2호
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    • pp.147-154
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    • 2021
  • One of the most challenging issues when robots interact with the environment is to establish contact quickly and avoid high impact force at the same time. The proposed method implements the passive suspension system using the redundancy of the torque-controlled robot. Instead of utilizing the actual mechanical compliance, the distal joints near the end-effector are controlled to act as a virtual spring-damper system with low feedback gains. The proximal joints are precisely controlled to push the mid-link, which is defined as the boundary link between the proximal and distal joints, towards the environment with high feedback gains. Compared to the active compliance methods, the contact force measurements or estimates are not required for contact establishment and the control time delay problems do not occur correspondingly. The proposed method was applied to the landing foot control of the 12-DoF biped robot DYROS-RED in the simulations. In the results, the impact force during landing was significantly reduced at the same collision speed.