• 제목/요약/키워드: kinematic modeling

검색결과 225건 처리시간 0.031초

마그네슘 판재를 위한 온도 의존형 C-H/V 구성 모델에 관한 연구 (The Temperature Dependent C-H/V Constitutive Modeling for Magnesium Alloy Sheet)

  • 박종현;이종길;김헌영
    • 소성∙가공
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    • 제21권4호
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    • pp.221-227
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    • 2012
  • The automotive and electronic industries have seriously considered the use of magnesium alloys because of their excellent properties such as strength to weight ratio, EMI shielding capability, etc. However, it is difficult to form magnesium alloys at room temperature because of the mechanical deformation related to twinning. Hence, magnesium alloys are normally formed at elevated temperatures. In this study, a temperature dependent constitutive model, the C-H/V model, for the magnesium alloy AZ31B sheet is proposed. A hardening law based on nonlinear kinematic and H/V(Hollomon/Voce) hardening model is used to properly characterize the Bauschinger effect and the stabilization of the flow stress. Material parameters were determined from a series of uni-axial cyclic experiments(C-T-C) with the temperature ranging between 150 and $250^{\circ}C$. The developed models are fit to experimental data and a comparison is made.

임펠러의 역공학과 5축가공에 관한 연구 (A Study on Reverse Engineering and 5-axis NC Machining of Impeller)

  • 장동규;신재광;홍성균;이희관;양균의
    • 한국정밀공학회지
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    • 제21권6호
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    • pp.60-68
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    • 2004
  • This paper presents a method fur impeller modeling and 5-axis machining by the reverse engineering. The impeller is composed of pressure surface, suction surface and leading edge, and so on. The surfaces can be modeled by using the characteristic curves such as hub curves, shroud curves and fillet curves. The characteristic curves are extracted from the scanned data and the inspection is performed between the surfaces generated by using the characteristic curves and the scanned data. Then, An impeller is machined by 5-axis mainlining and post-processing with inverse kinematic solution.

The Study of Error Compensation for Repeatability Improvement of Precision Positioning System

  • Lee, Woogeun;Changsoo Han;Park, Hyeunseok;Lee, Kyeyoung
    • 제어로봇시스템학회:학술대회논문집
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    • 제어로봇시스템학회 2001년도 ICCAS
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    • pp.66.6-66
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    • 2001
  • In this paper, we studied the error compensation using an error budget method for repeatability improvement of the precision positioning system. The precision positioning system is developed for micro-pressing machine. We performed the force and displacement analysis about parts of the system. Proposed system determines the position and orientation of the materials manufactured by micro-pressing machine. It is consisted of x-y-z linear stages setting the position, and the gripper system setting the orientation. We executed kinematic and dynamic modeling of the whole precision positioning system. By generalizing the design variables, precision positioning system has the flexibility of material dimension. As we tried an error compensation using ...

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반도체 장비용 고속프레스의 동특성 해석에 관한 연구

  • 국정근;조병관;이우영
    • 한국반도체및디스플레이장비학회:학술대회논문집
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    • 한국반도체및디스플레이장비학회 2005년도 추계 학술대회
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    • pp.155-159
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    • 2005
  • High speed presses with high resolution in semiconductor lead frame manufacturing process are needed . But high speed operation accompanies mechanical vibration. therefore optimized kinematic structure to minimize vibration is required for a high speed press. And the growing competition in the industry asks a press with low cost, high speed, high resolution, and high pressing force, For this purpose a high speed press was modeled with 3D CAD solid modeling system and dynamic analysis were performed with CAE S/W for multibody dynamic analysis, Through these analyses a motor appropriate to a high speed press was selected and link structure for feeding system of the press was modified to reduce vibration. To perform this analysis working Model which is 2D kinematics and dynamic analysis software was used.

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Stability analysis of infinite rock slopes with varying disturbances based on the Hoek-Brown failure criterion

  • Dowon Park
    • Geomechanics and Engineering
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    • 제33권1호
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    • pp.53-63
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    • 2023
  • Rock disturbance caused by blasting and stress relaxation is commonly observed during excavation. As the distance from the source of disturbance increases, the degree of disturbance decreases, and rock at a large depth does not experience disturbance. However, in stability analyses, a single value of disturbance is often applied to the entire rock mass, which leads to underestimated results. In this study, this modeling mistake is addressed by considering realistically varying rock disturbance. The safety of infinite slopes in a disturbed rock mass with a strength governed by the Hoek-Brown failure criterion is investigated based on the kinematic approach of limit analysis. The maximum disturbance is assigned to the outermost slope face because it is directly exposed to blasting damage and dilation, and the disturbance progressively decays with distance in the rock mass. The safety analysis results indicate that the assumption of uniform disturbance in the entire rock mass leads to underestimation of the rock strength and safety on infinite rock slopes. A critical slip surface appears to be within the disturbed rock layer as well as the interface between the disturbed upper rock and undisturbed lower rock.

준 실시간 정밀 위성궤도결정을 위한 이론적 고찰 (A Preliminary Study of Near Real-time Precision Satellite Orbit Determination)

  • 배태석
    • 한국측량학회지
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    • 제27권1호
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    • pp.693-700
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    • 2009
  • 장기선 네트워크 RTK(Real-Time Kinematic) 측량, 정밀단독측위(precise point positioning) 및 전리층/대류권 지연 모니터링등 GPS를 이용한 실시간 데이터 처리를 위해서는 IGS(International GNSS Service)에서 제공하는 정밀궤도 수준의 정확도가 시간지연 없이 확보되어야 한다. 본 연구는 준 실시간 위성궤도결정을 위한 선행연구로서 일반적인 위성궤도 결정 방법, 특히 동역학적 방법에 대한 이론적 고찰과 가속도 적분을 위한 지구기준/관성좌표계 변환 방법에 대한 테스트를 수행하였다. IAU 1976/1980 세차/장동모델은 IAU 2000A 모델과 0.05mas 수준의 허용범위 내 차이를 보였다. IAU 2000A 모델은 기본적으로 복잡한 장동모델로 인해 변환행렬 계산에 많은 시간이 소요된다. IAU 2000A 모델에 기존 변환 방법을 사용하는 경우가 NRO(non-rotating origin) 방법에 비해 2배정도 빠른 결과를 보인 반면 회전행렬의 실질적인 차이는 없는 것으로 나타났다.

자동차 가상생산 기술 적용(VII) : 프레스 디지털 가상공장의 구축과 활용 (Virtual Manufacturing for an Automotive Company(VII) : Construction and Application of a Virtual Press Shop)

  • 국승호;이상석;소순일;노상도;김희선;심경보;김주열
    • 산업공학
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    • 제21권3호
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    • pp.322-332
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    • 2008
  • Digital Virtual Manufacturing is a technology to facilitate effective product developments and agile productions by digital model representing the physical and logical schema and the behavior of real manufacturing system, and it includes product, resources, processes and plant. For successful applications of this technology, a digital virtual factory as a well-designed and integrated environment is essential. In this research, we constructed a sophisticated digital virtual factory of a Korean automotive company's press shop. For efficient constructions of a digital virtual factory useful to kinematic simulations and visualizations, we analyzed entire business process and detailed activities of press engineering. Also, we evaluated geometries, structures, characteristics and motions of a plant and machines in press shop. The geometric model and related data of a virtual press shop are built and managed by a modeling standard defined in this paper. The virtual manufacturing simulation of press machines is conducted to evaluate kinematic motions, cycle time and locations of components using geometric models and related data. It's for interference checks and productivity improvements. We expect that this virtual press shop helps us to achieve great savings in time and cost in many manufacturing preparation activities in the new car development process of automotive companies.

초고강도 강판 성형 시의 스프링백 해석 및 금형 소재 적합성 검토 (Analysis of Springback and Die Material Suitability in the UHSS Sheet Forming Process)

  • 오인석;윤동렬;조준행;이명규;김헌영;김형종
    • 소성∙가공
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    • 제29권4호
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    • pp.203-210
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    • 2020
  • In this study, formability and springback behavior of 1.5 GPa grade ultra-high strength steel (UHSS) sheet were predicted through the finite element simulation, and structural stability of the forming dies was verified by the coupled forming-structural analysis. Uniaxial tension and uniaxial tension-compression tests were performed to obtain experimental data for modeling the springback properties of the sheet material. The springback values predicted by simulation were compared with those from actual measurements. The results calculated from the kinematic hardening model were found to be much more accurate than those from the isotropic hardening model. Deformation of the forming die and springback of the product were calculated by the coupled forming-structural analysis. The higher the strength of the die material, the smaller the surface displacement of the die and the springback of the product. The internal stresses of the dies made of three materials, FC300, FCD550 and STD11 were compared with the yield stress of each material. The results provided a basis for determining the most suitable material for each part of the die set. As a result, simulation techniques have been established for predicting formability and springback in the UHSS sheet forming process.

Flight Dynamics Analyses of a Propeller-Driven Airplane (I): Aerodynamic and Inertial Modeling of the Propeller

  • Kim, Chang-Joo;Kim, Sang Ho;Park, TaeSan;Park, Soo Hyung;Lee, Jae Woo;Ko, Joon Soo
    • International Journal of Aeronautical and Space Sciences
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    • 제15권4호
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    • pp.345-355
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    • 2014
  • This paper focuses on aerodynamic and inertial modeling of the propeller for its applications in flight dynamics analyses of a propeller-driven airplane. Unsteady aerodynamic and inertial loads generated by the propeller are formulated using the blade element method, where the local velocity and acceleration vectors for each blade element are obtained from exact kinematic relations for general maneuvering conditions. Vortex theory is applied to obtain the flow velocities induced by the propeller wake, which are used in the computation of the aerodynamic forces and moments generated by the propeller and other aerodynamic surfaces. The vortex lattice method is adopted to obtain the induced velocity over the wing and empennage components and the related influence coefficients are computed, taking into account the propeller induced velocities by tracing the wake trajectory trailing from each of the propeller blades. Aerodynamic forces and moments of the fuselage and other aerodynamic surfaces are computed by using the wind tunnel database and applying strip theory to incorporate viscous flow effects. The propeller models proposed in this paper are applied to predict isolated propeller performances under steady flight conditions. Trimmed level forward and turn flights are analyzed to investigate the effects of the propeller on the flight characteristics of a propeller-driven light-sports airplane. Flight test results for a series of maneuvering flights using a scaled model are employed to run the flight dynamic analysis program for the proposed propeller models. The simulations are compared with the flight test results to validate the usefulness of the approach. The resultant good correlations between the two data sets shows the propeller models proposed in this paper can predict flight characteristics with good accuracy.

5절 평면형 메커니즘의 동적 포복에 관한 연구 (Study on Dynamic Crawling of The Five-bar Planar Mechanism)

  • 이정헌;임남식;김희국;이병주
    • 한국정밀공학회:학술대회논문집
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    • 한국정밀공학회 2005년도 춘계학술대회 논문집
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    • pp.1045-1049
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    • 2005
  • In this paper, the dynamic crawling of a five-bar planar mechanism is investigated. One complete cycle of the crawling selected in this study consists of four different steps, i) sliding at one contact point between the mechanism and the ground, ii) changing its configuration without sliding at two contact points, iii) sliding at the other contact point, and iv) again changing its configuration without sliding at two contact points. In this type of crawling, the crawling mechanism maintains the shape of the parallel structure throughout a complete crawling cycle. The modeling algorithm for serial manipulators proposed by M. Thomas and et al.[1] is employed by introducing imaginary joints and links which represent the contact interfaces between the one end of the mechanism and the ground, while the other end of the mechanism is regarded as an end-effector of the imaginary serial manipulator which treats the reaction force and torque at the contact point as external forces. Then, a complete cycle of dynamic crawling of the mechanism is investigated through various computer simulations. The simulation result show that the stable crawling characteristics of the mechanism could be secured when the proper configurations depending on specified frictional constraints are met.

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