• Structural Engineering and Mechanics
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• 제3권1호
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• pp.49-60
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• 1995

In the present study, a finite strip method for the vibration and stability analyses of anisotropic laminated composite plates is developed according to the higher-order shear deformation theory. This theory accounts for the parabolic distribution of the transverse shear strains through the thickness of the plate and for zero transverse shear stresses on the plate surfaces. In comparison with the finite strip method based on the first-order shear deformation theory, the present method gives improved results for very thick plates while using approximately the same number of degrees of freedom. It also eliminates the need for shear correction factors in calculating the transverse shear stiffness. A number of numerical examples are presented to show the effect of aspect ratio, length-to-thickness ratio, number of plies, fibre orientation and stacking sequence on the natural frequencies and critical buckling loads of simply supported rectangular cross-ply and arbitrary angle-ply composite laminates.

• Current Optics and Photonics
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• 제4권6호
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• pp.545-550
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• 2020

We propose a hole-filling method to solve discontinuous depth representation and to reduce the visible seams and cracks that cause the limitation of the viewing angle of the three-dimensional (3D) image in the multilayer type 3D display system. The occlusion and the disocclusion regions between layers, such as the visible seams and cracks, are a major bottleneck of the multilayer type 3D display system to represent a volumetric 3D image by stacking multiple images. As a result, in the reconstructed 3D image, the visible seams and cracks appear as brighter overlapping and undesirable cut-off. In order to resolve the problems above, we applied the depth-fused effect to the sub-depth map generating algorithm and improve the viewing characteristics of the multilayer type 3D display. The experimental demonstrations are also provided to verify the proposed scheme.

• 한국정밀공학회지
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• 제12권8호
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• pp.27-38
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• 1995

For solving troubles happened during the drilling process with carbon fiber epoxy composite materials(CFRP) by using HSS drill, a few types of diamond gift electroplated drills are manufactured, and machinability of these drills is experimented with a variety of cutting speed and feed rate. These drills have some advantages of good wear resistant and the conception of grinding process. As a result, using of these drills improves both troubles being caused by tool wear and damage of exit surface depending on fiber stacking angle. It is desirable that cutting conditions for the cutting thickness per revolution must be set under 0.01mm when the size of a diamond grit is # 60 .approx. 80.

• Structural Engineering and Mechanics
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• 제88권3호
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• pp.201-208
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• 2023

In this work, the effect of the correction fibers direction on the efficiency of repairing damaged composite plates was highlighted. The composite plates studied in this work consist of eight layers of graphite/epoxy, while the patch used in this repair consists of four layers of the same type. The results obtained in this work, whether with regard to the experimental or analytical side, showed that the fibers orientation affects the repair efficiency, so the closer the angle of fibers inclination is to the tensile strength direction, the performance of the composite material is ideal. Hence, we conclude that the composite materials with longitudinal fibers (Parallel to tensile strength) is the most powerful and efficient material in performance.

• 대한기계학회논문집A
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• 제29권3호
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• pp.455-461
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• 2005

This research studied robust design of composite hand for LTR (LCD glass Transfer Robot). $1^{st}$ DOE (Design of Experiment) was conducted to find out vital few Xs. 108 experiments were performed and their results were statistically analyzed. Pareto chart analysis shows that the geometric parameters (height and width of composite beam) are more important than material parameters $(E_{1},\;E_{2})$ or stacking sequence angle. Also, the stacking sequence of mid-layer is more important than that of outer-layer. The main effect plots shows that the maximum deflection of LTR hand is minimized with increasing height, width of beam and layer thickness. $2^{nd}$ DOE was conducted to obtain RSM (Response Surface Method) equation. 25 experiments were conducted. The CCD (Central Composite Design) technique with four factors was used. The coefficient of determination $(R^{2})$ for the calculated RSM equation was 0.989. Optimum design was conducted using the RSM equation. Multi-island genetic algorithm was used to optimum design. Optimum values for beam height, beam width, layer thickness and beam length were 24.9mm, 186.6mnL 0.15mm and 2402.4mm respectively. An approximate value of 0.77mm in deflection was expected to be a maximum under the optimum conditions. Six sigma robust design was conducted to find out guideline for control range of design parameter. To acquire six sigma level reliability, the standard deviation of design parameter should be con trolled within $2{\%}$ of average design value

• 한국강구조학회 논문집
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• 제26권5호
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• pp.397-405
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• 2014

본 연구에서는 적층복합 T형 보의 휨 해석을 위해 전단에 유연한 보 요소를 제안한다. 1차 전단변형 보 이론을 사용해 유도된 보 요소는 ? 전단변형과 재료의 비등방성 성질에 따른 모든 연계성을 고려한다. 지배방정식의 해를 구하기 위해 절점 당 7개의 자유도를 갖는 2절점, 3절점, 4절점의 세 가지 보 요소를 제안한다. 제안된 보 요소의 활용성과 정확성을 검증하기 위해 등분포하중과 집중하중을 받는 대칭 및 역대칭 앵글프라이 복합 T형 보에 대해 수치해석을 수행한다. 다른 적층순서에 대해 화이버 각과 전단변형의 영향을 조사한다. 적층 복합 T형 보의 휨 해석에 대해 3절점과 4절점 보 요소의 유효성을 입증하였다.

• 대한기계학회논문집A
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• 제36권1호
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• pp.51-58
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• 2012

본 연구는 외부 수압을 받는 복합재 원통 셸에 대해서 원통 좌굴식 (ASME 2007,NASA SP- 8007)과 유한요소법을 이용하여 좌굴 압력을 예측하기 위함이다. 본 연구에 사용된 모델은 적층 각도 [0/90]$_{12t}$ 이며 복합재 재질은 USN 125 이다. 복합재는 프리프래그 방식으로 제작되었다. 본 논문에 사용된 연구 방법은 원통 셸의 좌굴식, 유한요소해석을 수행하고 이를 실험으로 검증 하였다. 원통 셸의 좌굴식과 유한요소 결과를 비교하기 위하여 $20^{\circ}{\sim}90^{\circ}$까지 $5^{\circ}$씩 변화시켜 도식화 하여 비교하였다. 유한요소해석의 결과는 선형과 비선형은 안전율 0.85~1.0 으로 잘 일치하였다. 좌굴 압력식은 적층각이 증가할수록 좌굴압력이 증가하였다. 유한요소 해석과 비교하면 ASME 2007 식이 NASA SP-8007 식보다 안전율이 더 큰 식임을 알 수 있었다.

• 한국융합학회논문지
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• 제10권1호
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• pp.155-161
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• 2019

복합소재는 기존의 일반적인 소재보다 내구성과 기계적 성질들이 뛰어난 경량 소재이다. 본 연구에서는 경량 복합소재에 주목하여, 접착제를 이용하여 접착한 CFRP 접착구조물의 정적 파괴 특성을 조사하고자 했고 적층 각도를 변수로 한 CFRP 이중외팔보 시험편을 설계하여 정적 파괴 해석을 수행하였다. 본 연구를 위하여 설계된 CFRP 이중외팔보 시험편들의 적층각도들은 각각 $30^{\circ}$와 $45^{\circ}$, $60^{\circ}$이며, 연구 결과로서는 적층 각도 $45^{\circ}$인 시험편이 가장 $30^{\circ}$, $60^{\circ}$의 적층 각도를 가진 시험편들보다 더 좋은 내구성을 보였으며, $30^{\circ}$의 적층 각도를 가진 시험편이 모든 시험편 중에서 내구성이 가장 취약한 것을 확인할 수 있었다. 이와 같은 본 연구 결과를 통하여 적층 각도 별 CFRP 접착구조물의 파손데이터를 확보할 수 있었으며, 본 연구결과를 토대로 얻은 접착 계면의 파손데이터를 활용함으로서 실생활에서의 기계나 구조물에 융합하여 그 미적 감각을 나타낼 수 있다.

• 한국생산제조학회지
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• 제23권3호
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• pp.250-258
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• 2014

Due to recent industrial growth and development, there has been a high demand for light and highly durable materials. Therefore, a variety of new materials has been developed. These new materials include carbon fiber reinforced plastic (CFRP or CRP), which is a wear-, fatigue-, heat-, and corrosion-resistant material. Because of its advantageous properties, CFRP is widely used in diverse fields including sporting goods, electronic parts, and medical supplies, as well as aerospace, automobile, and ship materials. However, this new material has several problems, such as delamination around the inlet and outlet holes at drilling, fiber separation, and tearing on the drilled surface. Moreover, drill chips having a fine particulate shape are harmful to the work environment and engineers' health. In fact, they deeply penetrate into machine tools, causing the reduction of lifespan and performance degradation. In this study, CFRP woven and unidirectional prepregs were formed at $45^{\circ}$ and $90^{\circ}$, respectively, in terms of orientation angle. Using a high-speed steel drill and a TiAIN-coated drill, the two materials were tested in three categories: cutting force with respect to RPM and feed speed; shape changes around the input and outlet holes; and the shape of drill chips.

• 한국강구조학회 논문집
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• 제18권2호
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• pp.161-171
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• 2006

본 논문은 고정과 자유 경계의 다양한 조합을 갖는 직사각형 복합적층판의 고유진동에하고 있다. 본 연구에서는 수학적으로 완전한 특성직교다항식으로 표현되는 근사변위와 Ritz법을 이용하여 Lagrange 범함수의 정상값을 구하였다. 3차원 모델의 정확성이 무차원 진동수의 수렴도를 검토하여 이루어졌으며, 또한 기존 문헌상의 해석결과와의 비교를 통하여 진동수의 정확성을 검토하였다. 본 논문에서 제시된 3차원 진동수의 결과를 이용하여 복합적층판의 기하 및 재료에 관한 매개변수 즉, 형상비(${\mathcal{a/b}}$), 폭두께비(${\mathcal{a/h}}$), 재료의 직교이방성, 플라이 수(${\mathcal{N}}$), 섬유배향각(${\theta}$) 및 적층순서가 미치는 효과를 설명하였다.