• 제목/요약/키워드: Composite Cantilever Beam

검색결과 120건 처리시간 0.023초

Theoretical analysis of composite beams under uniformly distributed load

  • Daouadji, Tahar Hassaine;Adim, Belkacem
    • Advances in materials Research
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    • 제5권1호
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    • pp.1-9
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    • 2016
  • The bending problem of a functionally graded cantilever beam subjected to uniformly distributed load is investigated. The material properties of the functionally graded beam are assumed to vary continuously through the thickness, according to a power-law distribution of the volume fraction of the constituents. First, the partial differential equation, which is satisfied by the stress functions for the axisymmetric deformation problem is derived. Then, stress functions are obtained by proper manipulation. A practical example is presented to show the application of the method.

면내 및 면외 하중 조건들에 따른 이종 복합 소재를 가진 경사진 이중외팔보에서의 접착계면의 파괴 특성 연구 (A Study on Fracture Property of Adhesive Interface at Tapered Double Cantilever Beam with Inhomogeneous Composite Material due to Loading Conditions of In-plane and Out-plane)

  • 이정호;김재원;전성식;조재웅
    • Composites Research
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    • 제33권6호
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    • pp.401-407
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    • 2020
  • 공학 및 산업 분야에서는 구조적인 부분들에서 경량 복합 소재가 강과 같은 금속 소재를 대체해 오고 있다. 이러한 복합 소재는 리벳, 용접이나 볼트 및 너트를 이용한 체결 방법을 대신하여 접착제 체결 방법을 적용하고 있다. 복합 소재에 접착제 체결 방법을 적용하기 위해서는 접착계면에 대한 강도 특성 연구가 필수적으로 요구된다. 섬유 강화 플라스틱 복합 소재인 CFRP를 용이하게 가공하여 본 연구를 수행하였다. CFRP와 알루미늄(Al6061), 알루미늄 폼(Al-foam)을 가진 이종 복합 소재로 된 경사진 이중외팔보(TDCB) 시험편들로서 면내 전단과 면외 전단의 하중 조건들하에서 정적 실험을 수행하였다. 본 연구 결과를 통하여 이중외팔보들의 파괴 특성과 그 파단 시점을 파악하여 접착계면을 가진 이종 복합 소재 구조물에 관한 내구성을 검토하였다.

알루미늄 합금으로 된 경사진 이중외팔보의 충돌에 대한 실험 및 해석 (Experiment and Analysis on Impact of Tapered Double Cantilever Beam with Aluminum Alloy)

  • 고등;조재웅;전성식
    • Composites Research
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    • 제27권2호
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    • pp.72-76
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    • 2014
  • 본 연구에서는 알루미늄 합금으로 된 경사진 이중외팔보의 충돌에 대해서 각각의 충격속도 2.5m/s, 7.5m/s, 12.5 m/s 별로 실험과 시뮬레이션 해석을 하였다. 접착부분에 발생하는 에너지 해방율과 응력을 평가하여 알루미늄 합금의 기계적 특성을 고찰하였다. 실험상에서는 접착 부분에서 에너지 해방율의 값이 높은 것으로 나타났다. 이는 실험에서 시험편이 분리된 후에도 접착력이 유지되는 특성 때문인 것으로 사료된다. 충격속도와 상관없이 균열이 진전하다가 접착된 부분의 끝에서 높은 응력을 발생하기 때문에 최대 등가응력은 마지막 단계에서는 올라간다. 본 연구에서의 실험 및 해석결과들은 충돌에 의한 균열 진전을 방지할 수 있는 복합재료에 대한 안전설계의 개발에 필요한 자료로 사료된다.

극저온 환경에서 에폭시 접착제의 물성 향상을 위한 나노 보강재의 표면 개질에 관한 연구 (The Effect of the Core-shell Structured Meta-aramid/Epoxy Nanofiber Mats on Interfacial Bonding Strength with an Epoxy Adhesive in Cryogenic Environments)

  • 오현주;김성수
    • Composites Research
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    • 제26권2호
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    • pp.129-134
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    • 2013
  • 극저온 환경에 노출되는 구조체의 접착조인트의 경우 피접착물과 접착물 사이에서 열팽창계수 차이로 인해 계면에서 잔류응력이 발생하게 되는데 이에 의해 접착조인트 내부에 미소균열, 층간분리 등의 형태로 파손이 발생할 우려가 있다. 본 연구에서는 높은 비강성, 낮은 열팽창계수의 특성을 지닌 메타 아라미드 섬유를 에폭시 기지재의 보강재로 사용하였다. 표면처리 공정을 간소화하기 위해 전기방사법의 고분자 혼합법(polymer blend method)으로 코어-쉘 구조의 메타 아라미드/에폭시 나노섬유를 제조하였다. 극저온 환경에서 계면특성이 향상된 코어-쉘 구조의 나노섬유를 보강한 에폭시 접착제의 전단물성을 확인하기 위해 환경챔버를 이용하여 $-150^{\circ}C$의 저온에서 단일 겹치기 실험(single lap joint test)을 진행하였다. 또한, DCB(double cantilever beam) 실험을 통해 파괴인성을 측정하였다. 그 결과, 극저온에서 일반 메타 아라미드 나노섬유에 비해 코어-쉘 구조의 메타 아라미드/에폭시 나노섬유를 보강한 접착제 시편이 우수한 계면특성으로 인해 물성이 크게 향상되었음을 확인하였다.

Dynamic analysis of nanotube-based nanodevices for drug delivery in sports-induced varied conditions applying the modified theories

  • Shaopeng Song;Tao Zhang;Zhiewn Zhui
    • Steel and Composite Structures
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    • 제49권5호
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    • pp.487-502
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    • 2023
  • In the realm of nanotechnology, the nonlocal strain gradient theory takes center stage as it scrutinizes the behavior of spinning cantilever nanobeams and nanotubes, pivotal components supporting various mechanical movements in sport structures. The dynamics of these structures have sparked debates within the scientific community, with some contending that nonlocal cantilever models fail to predict dynamic softening, while others propose that they can indeed exhibit stiffness softening characteristics. To address these disparities, this paper investigates the dynamic response of a nonlocal cantilever cylindrical beam under the influence of external discontinuous dynamic loads. The study employs four distinct models: the Euler-Bernoulli beam model, Timoshenko beam model, higher-order beam model, and a novel higher-order tube model. These models account for the effects of functionally graded materials (FGMs) in the radial tube direction, giving rise to nanotubes with varying properties. The Hamilton principle is employed to formulate the governing differential equations and precise boundary conditions. These equations are subsequently solved using the generalized differential quadrature element technique (GDQEM). This research not only advances our understanding of the dynamic behavior of nanotubes but also reveals the intriguing phenomena of both hardening and softening in the nonlocal parameter within cantilever nanostructures. Moreover, the findings hold promise for practical applications, including drug delivery, where the controlled vibrations of nanotubes can enhance the precision and efficiency of medication transport within the human body. By exploring the multifaceted characteristics of nanotubes, this study not only contributes to the design and manufacturing of rotating nanostructures but also offers insights into their potential role in revolutionizing drug delivery systems.

압전 복합재료 작동기 LIPCA를 이용한 보의 진동 제어 (Vibration Control of Beam using Piezoceramic Composite Actuator LIPCA)

  • 아리프수하리요노;구남서;박훈철;윤광준
    • 한국군사과학기술학회지
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    • 제8권4호
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    • pp.130-135
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    • 2005
  • This paper presents application possibility of Lightweight Piezoceramic Composite Actuator(LIPCA) to suppress vibration of dynamic structures as an actuator. LIPCA is composed of a piezoelectric layer, a carbon/epoxy layer and glass/epoxy layers. When compared to the bare piezoelectric ceramic(PZT), LIPCA has advantages such as high performance, durability and reliability. In this study, performances of LIPCA have been estimated in an active vibration control system. Experiments were performed on an aluminum beam with cantilever configuration. In this test, strain gages and single LIPCA are attached on the aluminum beam with epoxy resin. Digital ON-OFF control algorithm is applied into the system to exhibit performance of LIPCA as actuator in active vibration control system. First, we performed static actuation test of bare PZT and LIPCA in order to show the superiority of LIPCA. Secondly, we carried out beam vibration control test using LIPCA. The results showed LIPCA could suppress free vibration of the aluminum beam, which means that LIPCA can be applied as an actuator to control vibration of dynamic structures.

계면처리와 스타칭이 복합적층판의 파괴거동에 미치는 영향 연구 (Study on the Effects of Surface Treatment and Stitching on the Fracture Behavior of Composite Laminates)

  • 홍순영;황운봉;박현철;한경섭
    • 대한기계학회논문집A
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    • 제20권3호
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    • pp.806-815
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    • 1996
  • The interlaminar fracture behavior of woven laminates under static and cyclic loadings has been studied using DCB(double cantilever beam) specimens. The effects of surface treatment and stiching on the fracture behavior of composite laminates are investigated experimentally. Fracture toughness has been improved by surface treatment because the surface treatment can change the fracture mechanism of laminates. SCB(stitched cantilever beam) model has been proposed to quantify the effect of through-thickness resinforcement(stiching) in improving the delamination crack growth resistance. Distributed loads which are transfered to through-thickness fibers can be calculated by the SCB model. And fracture energy increase due to the distributed load can be predicted by a power function of the distributed load. A new parameter agreed well proposed predict fatigue crack growth rate. The predictions using this parameter agreed well with the experimental data.

크림프를 가진 섬유 캔틸레버의 대변형의 일래스티카 해 (Elastica Solution of Large Deformation of Fiber Cantilever with Crimped Shapes)

  • 정재호;강태진
    • 한국복합재료학회:학술대회논문집
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    • 한국복합재료학회 2001년도 춘계학술발표대회 논문집
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    • pp.102-105
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    • 2001
  • In this paper, the solution of two dimensional deflection of circular wavy elastica beam was obtained for one end clamped boundary and concentrated load condition. The beam was regarded as a linear elastic material. Wavy shape was described as a combination of half-circular arc smoothly connected each other with constant curvature of all the same magnitude and alternative sign. Also load direction was taken into account. As a result, the solution was expressed in terms of a series of integral equations. While we found the exact solutions and expressed them in terms of elliptic integrals, the recursive ignition formulae about the displacement and arc length at each segment of circular section were obtained. Algorithm of determining unknown parameters was established and the profile curve of deflected beam was shown compared with initial shape.

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Free vibration analysis of damaged composite beams

  • Cunedioglu, Yusuf;Beylergil, Bertan
    • Structural Engineering and Mechanics
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    • 제55권1호
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    • pp.79-92
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    • 2015
  • In this study, free vibration analyses of symmetric laminated cantilever and simply supported damaged composite beams are investigated by using finite element method (FEM). Free vibration responses of damaged beams are examined using Euler Bernoulli beam and classical lamination theories. A computer code is developed by using MATLAB software to determine the natural frequencies of a damaged beam. The local damage zone is assumed to be on the surface lamina of the beam by broken fibers after impact. The damaged zone is modeled as a unidirectional discontinuous lamina with $0^{\circ}$ orientations in this study. Fiber volume fraction ($v_f$), fiber aspect ratio ($L_f/d_f$), damage length ($L_D$) and its location (${\lambda}/L$), fiber orientation and stacking sequence parameters effects on natural frequencies are investigated. These parameters are affected the natural frequency values significantly.