• 제목/요약/키워드: Stacking angle

검색결과 132건 처리시간 0.022초

적층각 변화에 따른 복합재료 기계적 체결부의 파손강도 (Failure Strength of the Composite Mechanical Joint according to the Stacking Angle)

  • 조대현;김철환;최진호
    • Composites Research
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    • 제30권4호
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    • pp.229-234
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    • 2017
  • 일반적인 복합재료 구조물에서 체결부는 가장 취약한 부분이다. 복합재 체결법은 접착 조인트와 기계적 조인트로 크게 나눌 수 있으나, 환경조건에 덜 민감한 부분에는 주로 기계적 조인트가 많이 사용되고 있다. 본 논문에서는 5가지의 적층각 변화를 가지는 복합재료 기계적 조인트의 파손하중을 실험하고 예측하였다. 기계적 조인트에 대한 유한요소 해석을 수행하고 Tsai-Wu와 Yamada-Sun 파손이론을 이용하여 파괴면적지수법(FAI)으로 파손강도를 예측하였으며, 이를 실험 결과와 상호 비교하였다. 실험과 해석결과, 복합재 기계적 체결부는 0도 층의 비율이 낮을수록 파손하중이 저하되었으며, 파괴면적지수법과 Yamada-Sun 파손식으로 13.03% 오차범위 내에서 파손하중을 예측할 수 있었다.

편향각과 전단각이 탄소섬유/에폭시 평직 복합재료의 압축특성에 미치는 영향 (The Effect of Bias and Shear Angles on Compressive Characteristics of Carbon/Epoxy Plain Weave Fabrics)

  • 김성집;장승환
    • 대한기계학회논문집A
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    • 제30권7호
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    • pp.857-864
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    • 2006
  • Various compressive specimens were fabricated using autoclave do-gassing moulding to find out the compressive characteristics of the carbon/epoxy plain weave fabric composites with respect to the bias and shear angles. The stacking angles of the bias specimens are $[0]_{10T,}\;[3]_{10T,}\;[6]_{10T,}\;[9]_{10T,}\;[12]_{10T,}\;[15]_{10T,}\;[30]_{10T,}\;[45]_{10T}$ and those of the sheared specimens are $[{\pm}37]_{10T,}\;[{\pm}32]_{10T,}\;[{\pm}28]_{10T,}\;[{\pm}22]_{10T,}$ respectively. In order to verify the effect of micro-tow structures on compressive strength and modulus of the composites, compressive test specimens of uni-directional carbon/epoxy composites with the same materials and the same stacking conditions were fabricated. The modulus and strength of both types of composite specimens were compared with the prediction results based on the CLPT and a proposed strength formula. The tow deformation and fracture modes were investigated by microscopic observation.

중첩선과 단면형상을 고려한 축류 송풍기 날개의 최적설계 (Optimization of Stacking Line and Blade Profile for Design of Axial Flow Fan Blade)

  • 압두스 사마드;이기상;정상호;김광용
    • 한국전산유체공학회:학술대회논문집
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    • 한국전산유체공학회 2008년도 춘계학술대회논문집
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    • pp.420-423
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    • 2008
  • This present work is to find optimum design of a NACA65 axial fan blade with weighted average surrogate model. The numerical analysis by Reynolds-average Navier-Stokes equations with shear stress turbulence(SST) is discretized by finite volume approximations and solved on hexahedral grids for flow analysis. The blade aerodynamic shape is modified by six design variables for the optimization. The blade profile as well as stacking line is modified to enhance blade total efficiency. Six design variables, airfoil maximum camber, maximum camber location, leading edge radius, trailing edge radius, lean angle at 50% span and lean angle at 100% span, are selected for blade profile to enhance the total efficiency. The PBA model which is basically weighted average of the basis surrogates is used to find the optimal design in the design space from the constructed response surface model for the objective function. By the optimization, the total efficiency is increased by 1.4%.

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초경드릴을 이용한 탄소섬유 에폭시 복합재료의 드릴링 특성에 있어 선단각의 영향 (Effects of the Point Angle on Drilling Characteristics Carbon Fiber Epoxy Composite Materials Using WC-drill Drilling)

  • 김형철
    • 한국정밀공학회:학술대회논문집
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    • 한국정밀공학회 1996년도 춘계학술대회 논문집
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    • pp.85-91
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    • 1996
  • The drilling experiment of carbon fiber epoxy composite material with WC-drill has been done under the various cutting condition in order to minimize the problems occured in the material when being drilled. It has been comfirmed by a frequencyanalysis of the cutting force signals that the variation of cutting force resulted from the periodic variation of the angle between the rotating drill and the stacking angle of the carbon fiber. The drilling experiment has been done with several drills having different point angles and the drilling characteristics, like the effects such that change in the point angle influences the cutting force and the external surface condition, was evaluated.

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CFRP 사교적층판의 핀 베어링강도에 관한 연구 (A Study on the Pin Bearing Strength of Angle Ply CFRP Composites)

  • 전진탁
    • 수산해양기술연구
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    • 제34권3호
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    • pp.339-345
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    • 1998
  • The purpose of this paper is to investigate the effect of the specimen geometries on the pin bearing strength of the angle ply carbon fiber reinforced composites. The effect of the edge distance and the specimen width on the pin bearing strength of angle ply CFRP composites are experimentally investigated in this paper. As results, the failure mode and pin bearing strength of mechanical joints turned out to depends on the stacking sequence and specimen geometries such as the edge distance and the specimen width. The higher pin bearing strength obtained for the angle ply CFRP composites is attributed to a combination of debonding, pull out, buckling and breakage of fiber and also the matrix cracking.

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Enhancement of Seismic Stacking Energy with Crossdip Correction for Crooked Survey Lines

  • Kim, Ji Soo;Lee, Sun Jung;Seo, Yong Seok;Ju, Hyeon Tae
    • 지질공학
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    • 제24권2호
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    • pp.171-178
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    • 2014
  • In seismic reflection data processing, the crossdip correction effectively focuses the stacking energy near the sharp bends of a crooked survey line. Additionally, approximate 3-D information on the reflector (e.g., true crossdip angle and lateral continuity) are locally investigated as a by-product of the crossdip correction procedure. Improvement of the signal-to-noise ratio and estimation of reflector crossdip attitude are tested, in terms of both common midpoint bin direction and processing-line type, using synthetic seismic reflection data. To effectively image the reflection energy near bends in seismic survey lines, straight-line binning is preferred to slalom-line binning.

Geometrically nonlinear analysis of thin-walled open-section composite beams

  • Vo, Thuc Phuong;Lee, Jae-Hong
    • 한국공간구조학회:학술대회논문집
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    • 한국공간구조학회 2008년도 춘계 학술발표회 논문집
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    • pp.113-118
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    • 2008
  • This paper presents a flexural-torsional analysis of thin-walled open-section composite beams. A general geometrically nonlinear model for thin-walled composite beams and general laminate stacking sequences is given by using systematic variational formulation based on the classical lamination theory. The nonlinear algebraic equations of present theory are linearized and solved by means of an incremental Newton-Raphson method. Based on the analytical model, a displacement-based one-dimensional finite element model is developed to formulate the problem. Numerical results are obtained for thin-walled composite beams under general loadings, addressing the effects of fiber angle, laminate stacking sequence and loading parameters.

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고속 공기 주축부를 위한 복합재료 주축의 최적 설계 (Optimal Design of a High Speed Carbon Composite Air Spindle)

  • 방경근;이대길
    • 대한기계학회논문집A
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    • 제25권11호
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    • pp.1767-1776
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    • 2001
  • For the stable operation of high speed air spindle, the low rotational inertia and high damping ratio of spindle shafts as well as high fundamental natural frequency are indispensable. Conventional steel spindles are net appropriate for very high speed operation because of their high rotational inertia and low damping ratio. In this study, a high speed spindle composed of carbon fiber epoxy composite shaft and steel flange was designed for maximum critical speed considering minimum static deflection and radial expansion due to bending load and centrifugal force during high speed relation. The stacking angle and the stacking thickness of the composite shaft and the adhesive bonding length of the 7teel flange were selected through vibrational analysis considering static and thermal loads due to temperature rise.

탄소섬유 에폭시 복합재료의 평면 연삭온도 특성에 관한 연구 (A Study on the Surface Grinding Temperature Characteristics of the Carbon Fiber Epoxy Composite Materials)

  • 한흥삼
    • 한국공작기계학회:학술대회논문집
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    • 한국공작기계학회 2000년도 춘계학술대회논문집 - 한국공작기계학회
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    • pp.441-446
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    • 2000
  • Although the net-shape molding of composites is generally recommended, molded composites frequently required cutting or grinding due to the dimensional inaccuracy for precision machine elements. During the composite machining operations such as cutting and grinding, the temperature at the grinding area may increase beyond the allowed limit due to the low thermal conductivity of composites, which might degrade the matrix of composite. Therefore, in this work, the temperature at the grinding point during surface grinding of carbon fiber epoxy composite was measured. The grinding temperature and surface roughness were also measured to investigate the surface grinding characteristics of the composited. The experiments were performed both under dry and wet grinding conditions with respect to cutting speed, feed speed, depth of cut and stacking angle. From the experimental investigation, the optimal conditions for the composite plain grinding were suggested.

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탄소섬유 에폭시 복합재료 연삭온도에 의한 연삭특성 (A Study on the Grinding Characteristics of the Carbon Fiber Epoxy Composite Material Grinding Temperature)

  • 한흥삼;이동주
    • 한국생산제조학회지
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    • 제9권6호
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    • pp.65-70
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    • 2000
  • Although the net-shape molding of composites is generally recommended, molded composites frequently requires cutting or grinding due to the dimensional inaccuracy for precision machine elements. During the composite machining operations such as cutting and grinding, the temperature at the grinding area may increase beyond the allowed limit due to the low thermal conductivity of composites, which might degrade the matrix of composite. Therefore, in this work, the temperature at the grinding point during surface grinding of carbon fiber epoxy composite was measured. The grinding temperature and surface roughness were also measured to investigate the surface grinding characteristics of the composites. The experiments were performed both under dry and wet grinding conditions with respect to cutting speed, feed speed, depth of cut and stacking angle. From the experimental investigation, the optimal conditions for the composite surface grinding were suggested.

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