• 제목/요약/키워드: Stacking Configuration

검색결과 34건 처리시간 0.025초

CFRP로 구성된 CT시험편의 섬유설계에 의한 적층구조에 따른 인장 특성 연구 (A Study on Tensile Property due to Stacking Structure by Fiber Design of CT Specimen Composed of CFRP)

  • 황규완;조재웅
    • 예술인문사회 융합 멀티미디어 논문지
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    • 제7권11호
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    • pp.447-455
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    • 2017
  • 현대 산업에서 복합재료를 폭넓게 사용하고 있다. 특히 섬유를 기반으로 하여 레진으로 경화시킨 섬유 강화 플라스틱의 재료는 우수하면서도 비강도, 비강성이 뛰어난 경량화 소재로 주목받고 있다. 이 중에서도 탄소섬유를 이용한 탄소섬유강화 플라스틱은 다른 섬유와 달리 뛰어난 기계적 특성을 지녀 차량과 항공기 등 고강도와 경량성을 동시에 필요로 하는 곳에 쓰이고 있다. 본 논문에서는 탄소섬유강화 플라스틱으로 구성된 CT시험편으로 섬유 설계에 따른 인장특성을 해석적 연구를 통해 규명한다. 구멍을 가진 CFRP복합재료의 응력해석에 있어서, 인장환경에서의 파괴경향을 파악한다. 또한 적층각도에 따른 결과를 통하여 해석결과 값에 있어 적층각도 60°로 구성된 해석모델에서 가장 낮은 응력값이 발생함과 사전크랙의 변형에너지 가장 낮음을 알 수 있었다. 본 연구 결과를 토대로 실제 실험으로 적용된 구조물에서의 파괴형상을 예측하기 위한 기반데이터를 제공할 수 있을 것으로 사료된다.

공작기계를 위한 보와 평판의 샌드위치 구조 설계에 관한 파라메트릭 연구 (Parametric Study on the Design of Sandwich Beams and Plates for Machine Tool Structures)

  • 김대일;장승환
    • 한국공작기계학회논문집
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    • 제15권1호
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    • pp.39-48
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    • 2006
  • In this paper, polymer composites based sandwich structures like beams and plates are optimised by using parametric study. The structures are composed of fibre reinforced composites for facial material and resin concrete and PVC foam for core materials. The stacking sequences and thickness of the composites are controlled as major parameters to find out the optimal condition for machine tool components. For the plate structure of machine tool bed composites-skined sandwich structure which has several ribs are proposed to enhance bending stiffnesses in two major directions at the same time. Dynamic robustness of a machine tool structure is investigated using modal analysis. From the results optimal configuration and materials for high precesion machine tools are proposed. And the plate was made of fiber reforced composite material and PVC foam.

최적 단면 치수를 가지는 복합재료 U-Beam의 설계 (Design of composite channel section beam for optimal dimensions)

  • 이헌창;전흥재;박지상;변준형
    • 한국복합재료학회:학술대회논문집
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    • 한국복합재료학회 2002년도 추계학술발표대회 논문집
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    • pp.276-279
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    • 2002
  • A problem formulation and solution for design optimization of laminated composite channel section beam is presented in this study. The objective of this study is the determination of optimum section dimensions of composite laminated channel section beam which has equivalent flexural rigidities to flexural rigidities of steel channel section beam. The analytical model is based on the laminate theory and accounts for the material coupling for arbitrary laminate stacking sequence configuration. The model is used to determine the optimal section dimensions of composite channel section beam. The web height, flange width and thickness of the beam are treated as design variables. The solutions described are found using a global search algorithm, Genetic Algorithms (GA).

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위성체 유연 보 구조물의 열 안정성 해석 (Thermal Stability Analysis of Flexible Beam Spacecraft Appendage)

  • 윤일성;송오섭
    • 한국소음진동공학회:학술대회논문집
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    • 한국소음진동공학회 2001년도 춘계학술대회논문집
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    • pp.399-406
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    • 2001
  • Thermally induced vibration response of composite thin walled beams is investigated. The thin-walled beam model incorporates a number of nonclassical effects of transverse shear, primary and secondary warping, rotary inertia and anisotropy of constituent materials. Thermally induced vibration response characteristics of a composite thin walled beam exhibiting the circumferentially uniform system(CUS) configuration are exploited in connection with the structural bending-torsion coupling resulting from directional properties of fiber reinforced composite materials and from ply stacking sequence. A coupled thermal structure analysis that includes the effects of structural deformations on heating and temperature gradient is investigated.

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착탈결구식 연결구조 복합소재 데크의 거동특성 분석 (Structural Characteristics of 스냅핏 Type Composite Deck Panel)

  • 이성우;정규상;조성환;심영식
    • 한국전산구조공학회:학술대회논문집
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    • 한국전산구조공학회 2006년도 정기 학술대회 논문집
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    • pp.719-724
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    • 2006
  • Owing to its special features of light weight, high durability, corrosion-resistant, composite material used in civil infrastructure can not only solve fundamental problems of deterioration and corrosion, but also reduce both construction and maintenance cost significantly. Composite deck panels of 스냅핏 type connection previously designed and fabricated have been redesigned herein. The sensitivity of gaps between snap-fits and tip angles was investigated. Stacking sequence of plies was scrutinized in order to facilitate pultrusion process. Deck panels of redesigned configuration due to bending has been analyzed. A comparison between the preliminary and modified deck design has been made.

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위성체 유연구조물의 진동 해석 (Thermally Induced Vibration Analysis of Flexible Spacecraft Appendages)

  • 윤일성;김규선;송오섭
    • 한국소음진동공학회:학술대회논문집
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    • 한국소음진동공학회 2000년도 춘계학술대회논문집
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    • pp.1216-1221
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    • 2000
  • Thermally induced vibration response of composite thin walled beams is investigated. The thin-walled beam model incorporates a number of nonclassical effects of transverse shear, primary and secondary warping, 'rotary inertia' and anisotropy of constituent materials. Thermally induced vibration response characteristics of a composite thin walled beam exhibiting the circumferentially uniform system(CUS) configuration are exploited in connection with the structural coupling resulting from directional properties of fiber reinforced composite materials and from ply stacking sequence. A coupled thermal structure analysis that includes the effects of structural deformations on heating and temperature gradient is investigated.

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압전재료를 이용한 위성체 구조물의 열 진동 제어 (Thermally Induced Vibration Control of Flexible Spacecraft Appendages Using by Piezoelectric Material)

  • 윤일성;송오섭;김규선
    • 한국소음진동공학회:학술대회논문집
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    • 한국소음진동공학회 2002년도 춘계학술대회논문집
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    • pp.303-310
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    • 2002
  • The bending vibration and thermal flutter instability of spacecraft booms modeled as circular thin-walled beams of closed cross-section and subjected to thermal radiation loading is investigated in this paper. Thermally induced vibration response characteristics of a composite thin walled beam exhibiting the circumferantially uniform system(CUS) configuration are exploited in connection with the structural flapwise bending-lagwise bending coupling resulting from directional properties of fiber reinforced composite materials and from ply stacking sequence. The numerical simulations display deflection time-history as a function of the ply-angle of fibers of the composite materials, damping factor, incident angle of solar heat flux, as well as the boundary of the thermal flutter instability domain. The adaptive control are provided by a system of piezoelectric devices whose sensing and actuating functions are combined and that an bonded or embedded into the host structure.

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섬유강화 복합재료, 고분자 포움 및 레진 콘크리트로 구성된 샌드위치 구조 설계를 위한 파라메트릭 연구 (Parametric study on design of sandwich structures composing of fibre reinfoced composites, polymer foam and resin concrete)

  • 김대일;장승환
    • 한국공작기계학회:학술대회논문집
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    • 한국공작기계학회 2005년도 춘계학술대회 논문집
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    • pp.429-434
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    • 2005
  • In this paper sandwich structures like beams and plates are optimised by using parametric study. The structures are composed of fibre reinforced composites for facial material and resin concrete and PVC foam for core materials. The stacking sequences and thickness of the composites are controlled as major parameters to find out the optimal condition for machine tool components. For the plate structure for machine tool bed composites-skined sandwich structure which has several ribs are proposed to enhance both directional bending stiffnesses at the same time. From the results optimal configuration and materials for high precesion machine tools are proposed.

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Package-Platformed Linear/Circular Polarization Reconfigurable Antenna Using an Integrated Silicon RF MEMS Switch

  • Hyeon, Ik-Jae;Jung, Tony J.;Lim, Sung-Joon;Baek, Chang-Wook
    • ETRI Journal
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    • 제33권5호
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    • pp.802-805
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    • 2011
  • This letter presents a K-band polarization reconfigurable antenna integrated with a silicon radio frequency MEMS switch into the form of a compact package. The proposed antenna can change its state from linear polarization (LP) to circular polarization (CP) by actuating the MEMS switch, which controls the configuration of the coupling ring slot. Low-loss quartz is used for a radiating patch substrate and at the same time for a packaging lid by stacking it onto the MEMS substrate, which can increase the system integrity. The fabricated antenna shows broadband impedance matching and exhibits high axial ratios better than 15 dB in the LP and small axial ratios in the CP, with a minimum value of 0.002 dB at 20.8 GHz in the K-band.

박벽 복합재료 보의 횡-비틀림 좌굴 해석 (Lateral-torsional buckling analysis of thin-walled composite beam)

  • 김영빈;이재홍
    • 한국전산구조공학회:학술대회논문집
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    • 한국전산구조공학회 2002년도 봄 학술발표회 논문집
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    • pp.489-496
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    • 2002
  • The lateral buckling of a laminated composite beam is studied. A general analytical model applicable to the lateral buckling of a composite beam subjected to various types of loadings is derived. This model is based on the classical lamination theory, and accounts for the material coupling for arbitrary laminate stacking sequence configuration and various boundary conditions. The effects of the location of applied loading on the buckling capacity are also included in the analysis. A displace-based one-dimensional finite element model is developed to predict critical loads and corresponding buckling modes for a thin-walled composite beam with arbitrary boundary conditions. Numerical results are obtained for thin-walled composites under central point load, uniformly distributed load, and pure bending with angle-ply and laminates. The effects of fiber orientation location of applied load, and types of loads on the critical buckling loads are parametrically studied.

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