• 제목/요약/키워드: static structure

검색결과 2,002건 처리시간 0.027초

고감쇠 주축 시스템을 위한 베어링의 복합배열에 관한 연구 (A Combined Bearing Arrangement for High Damping Spindle Systems)

  • Lee, C.H.
    • 한국정밀공학회지
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    • 제13권10호
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    • pp.139-145
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    • 1996
  • The machining accuracy and performance is largely influenced by the static, dynamic and thermal characteristics of spindle systems in machine tools, because the spindle system is a intermedium for cutting force from tool and machine powef from motor. Large cutting force and power are transmitted by bearing with a point or line contact. So, the spindle system is the static and dynamic weakest point in machine structure. For improvement of static stiffness of spindle system can be changed design parameters, such as diameter of spindle, stiffness of bearing and bearing span. But for dynamic stiffness, the change of the design parameters are not useful. In this paper, the combined bearing arrangement is suggested for high damping spindle system. The combined bearing arrangement is composed of tandem double back to back arrangement type ball bearins and a high damping hydrostatic bearing. The variation of static deflection and amplitude in first natural frequency is evaluated with the location of hydrostatic bearing between front and rear ball bearing. The optimized location of hydrostatic bearing for high static and dynamic stiffness is determined rapidly and exactly using the mode shape and transfer function of spindle. The calculation of damping effect on vibration by unbalance of grinding wheel and pulley in optimized spindle system is carried out to verify the validity of the combined bearing arrangement. Finally, the simulation of grinding process show that the surface roughness of workpiece with high damping spindle system is 60% better than with ball bearing spindle system.

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등가정하중을 이용한 접합날개의 구조최적설계 (Structural Optimization of a Joined-Wing Using Equivalent Static Loads)

  • 이현아;김용일;박경진;강병수
    • 대한기계학회논문집A
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    • 제30권5호
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    • pp.585-594
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    • 2006
  • The joined-wing is a new concept of the airplane wing. The fore-wing and the aft-wing are joined together in a joined-wing. The range and loiter are longer than those of a conventional wing. The joined-wing can lead to increased aerodynamic performance and reduction of the structural weight. In this research, dynamic response optimization of a joined-wing is carried out by using equivalent static loads. Equivalent static loads are made to generate the same displacement field as the one from dynamic loads at each time step of dynamic analysis. The gust loads are considered as critical loading conditions and they dynamically act on the structure of the aircraft. It is difficult to identify the exact gust load profile. Therefore, the dynamic loads are assumed to be (1-cosine) function. Static response optimization is performed for the two cases. One uses the same design variable definition as dynamic response optimization. The other uses the thicknesses of all elements as design variables. The results are compared.

Dynamic and static structural displacement measurement using backscattering DC coupled radar

  • Guan, Shanyue;Rice, Jennifer A.;Li, Changzhi;Li, Yiran;Wang, Guochao
    • Smart Structures and Systems
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    • 제16권3호
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    • pp.521-535
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    • 2015
  • Vibration-based monitoring is one approach used to perform structural condition assessment. By measuring structural response, such as displacement, dynamic characteristics of a structure may be estimated. Often, the primary dynamic responses in civil structures are below 5 Hz, making accurate low frequency measurement critical for successful dynamic characterization. In addition, static deflection measurements are useful for structural capacity and load rating assessments. This paper presents a DC coupled continuous wave radar to accurately detect both dynamic and static displacement. This low-cost radar sensor provides displacement measurements within a compact, wireless unit appropriate for a range of structural monitoring applications. The hardware components and operating mechanism of the radar are introduced and a series of laboratory experiments are presented to assess the performance characteristics of the radar. The laboratory and field experiments investigate the effect of factors such as target distance, motion amplitude, and motion frequency on the radar's measurement accuracy. The results demonstrate that the radar is capable of both static and dynamic displacement measurements with sub-millimeter accuracy, making it a promising technology for structural health monitoring.

정적 시험을 사용한 CFTA거더의 제조시 강성 결함 탐색 (Detection of Manufacturing Defects in Stiffness of CFTA Girder using Static Loading)

  • 김두기;나뎀 파레즈;취진타오;박경훈
    • 한국전산구조공학회논문집
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    • 제25권1호
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    • pp.109-116
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    • 2012
  • 새로운 형태의 교량 거더인 CFTA(Concrete filled and tied tubular steel arch) 거더의 비선형 거동에 대해 고찰한 후, CFTA 거더의 대량 공장 생산시 콘크리트 충진 불량으로 발생할 수 있는 결함인 거더 안의 빈 공간을 탐지하는 새로운 방법을 제안하였다. CFTA 거더 안의 비대칭성 콘크리트 충진 불량 결함을 구조물의 대칭 거동을 이용하여 탐색하였으며, 수치해석과 실험을 통해 제안된 방법을 검증하였다. 제안된 방법을 수치적으로 검증하기 위해 3차원 유한요소모델을 사용하였으며, 실험적으로 검증하기 위해 CFTA거더의 정적 실험자료를 사용하였다.

탄소섬유/에폭시 면재, 알루미늄 허니컴 코어 샌드위치 복합재 구조의 압입 손상에 의한 잔류강도 연구 (A Study on Residual Strength of Carbon/Epoxy Face Sheet and Honeycomb Core Sandwich Composite Structure after Quasi Static Indentation Damage)

  • 공창덕;박현범;이승현
    • Composites Research
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    • 제22권2호
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    • pp.24-29
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    • 2009
  • 본 연구에서는 알루미늄 허니컴 코어와 카본 면재가 적용된 샌드위치 복합재 구조에 대해 준정적 압입 손상 이후의 잔류 강도 평가에 대한 연구를 수행하였다. 3점 굽힘 시험과 압축 시험을 통해 시편의 강도를 확인하고 시편에 손상을 모사하기 위하여 준정적 압입 손상을 가하였다. 손상된 시편을 손상 전 시편과 동일한 시험을 통해 손상 전의 강도와 비교하였다. 압입 손상 이후 압축 강도와 굽힘 강도는 압입 깊이의 증가에 따라 강도가 감소하였고 손상 단계에 따른 잔류 강도 정도를 확인하였다.

비동기 파이프라인 구조를 위한 정적 래치 DCVSL 회로 (A Static Latched DCVSL Circuits for Asynchronous Pipeline Scheme)

  • 김영우;김수원
    • 대한전자공학회:학술대회논문집
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    • 대한전자공학회 1998년도 추계종합학술대회 논문집
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    • pp.759-762
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    • 1998
  • In this paper, a SL-DCVSL (static latched differential cascode voltage switch logic) circuit for the asynchronous pipeline is proposed. The proposed SL-DCVSL circuit is a slightly modified version of the DCVSL circuit, and used to improve the storage capability of the precharged functional blocks. The proposed SL-DCVSL has more robust storage characteristics compared to the conventional LDCVSL (latched DCVSL〔2〕). The operation of the proposed circuit is verified by simulating the asynchronous FIFO (First-In First-Out) structure.

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철근콘크리트뼈대 구조물의 정적 비선형 해석에 관한 연구 (A Study on the Nonlinear Analysis of R/C Frames Structures subjected to Static Loads)

  • 심종성;조민수
    • 한국콘크리트학회:학술대회논문집
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    • 한국콘크리트학회 1992년도 가을 학술발표회 논문집
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    • pp.196-201
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    • 1992
  • The purpose of this study is to develop the computer software for the nonlinear analysis of R/C frame structure under static loads. For this purpose, strain-rate dependant material model and physical element model considering both flexural and shear deformation are adopted and they are connected with 'TWO-D'which is commerical software for elastic structural analysis. The analytical results using the developed software are compared to the experiment results and they are generally satisfactory.

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빌딩 자동화를 위한 무선 센서 네트워크 라우팅 프로토콜 (Routing Algorithm of Wireless Sensor Network for Building Automation System)

  • 노덕래;홍승호
    • 대한전자공학회:학술대회논문집
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    • 대한전자공학회 2009년도 정보 및 제어 심포지움 논문집
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    • pp.45-47
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    • 2009
  • Wireless Sensor Network(WSN) has been very popular in unattended surveillance systems recently. For Applying WSN into Building Automation system(BAS), a novel hierarchial network structure and static routing algorithm which eliminates the scalability limitation of Zigbee are proposed in this paper. The static routing algorithm relying on the hierarchial network address reduces the computational complexity to a great extent and has a real-time performance which satisfies urgent applications well.

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유연 날개의 확률기반 최적 설계 (Reliability Based Design Optimization of the Flexible Wing)

  • 이재훈;김수환;권장혁
    • 한국전산유체공학회:학술대회논문집
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    • 한국전산유체공학회 2005년도 춘계 학술대회논문집
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    • pp.187-190
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    • 2005
  • In this study, the reliablility based design optimization is peformed for an aircraft wing. The flexiblility of the wing was assumed by considering the interaction modeled by static aeroelasticity between aerodynamic forces and the structure. For a multidisciplinary design optimization the results of aerodynamic analysis and structural analysis were included in the optimization formulation. The First Order Reliability Method(FORM) was employed to consider the uncertainty of the designed points.

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A TRUST REGION METHOD FOR SOLVING THE DECENTRALIZED STATIC OUTPUT FEEDBACK DESIGN PROBLEM

  • MOSTAFA EL-SAYED M.E.
    • Journal of applied mathematics & informatics
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    • 제18권1_2호
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    • pp.1-23
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    • 2005
  • The decentralized static output feedback design problem is considered. A constrained trust region method is developed that solves this optimal control problem when a complete set of state variables is not available. The considered problem is interpreted as a non-linear (non-convex) constrained matrix optimization problem. Then, a decentralized constrained trust region method is developed for this problem class exploiting the diagonal structure of the problem and using inexact computations. Finally, numerical results are given for the proposed method.