• 한국기계가공학회지
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• 제19권8호
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• pp.50-55
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• 2020

This study investigates the injection molding of a plastic rack gear and focuses on deflections in the part. The causes of deflections were found and resolved through a trade-off study by injection molding analysis. Based on a warpage analysis, the fiber orientation was found to be a dominant factor in the occurrence of deflections. Changes in the part design and various injection conditions were analyzed for their effects in reducing deflections. Based on the trade-off study, a new part bottom design, injection time, and melt temperature were recommended. A trial injection was done for the new plastic rack gear, and measurements showed that its flatness surpassed that of the original part and met the specified requirement. The short injection time, low melt temperature, and symmetric similar configuration of the part contributed to the reduction in deflections. Therefore, optimized gate design and injection conditions as well as a new part design were validated through injection molding analysis in this study.

• 대한기계학회논문집
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• 제16권9호
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• pp.1681-1690
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• 1992

본 연구에서는 유리섬유강화 플라스틱복합재료를 준비하여 이 재료의 섬유방 향에 따른 파괴인성 및 피로 균열성장거동을 평가하였다.

• Composites Research
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• 제12권5호
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• pp.65-79
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• 1999

본 논문은 단순지지된 복합재료 사각판과 원통쉘이 결합된 구조물의 자유진동해석을 위한 해석적 방법에 대하여 기술하였다. 결합전 단순지시된 사각판과 원통쉘의 응답을 얻기 위하여 고전적 판이론과 Love의 얇은 쉘이론에 기초한 에너지법을 적용하였다. 결합구조물의 해석에는 동적응답법을 적용하였고, 길이방향 판과 쉘의 결합부에서의 동적 주기 하중과 모멘트는 Dirac 델타 함수와 정현 함수를 사용하였을 때 연속조건을 만족함을 보였다. 또한 원통쉘의 기하하적 매개변수인 쉘의 길이 대 반경비와 반경 대 두께비에 따른 진동특성의 변화를 고찰하였고, 복합재료의 섬유 방향각과 직교이방성 매개변수가 결합 원통쉘의 기본 진동수에 미치는 영향에 미치는 영향에 대하여 연구하였다.

• Steel and Composite Structures
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• 제33권5호
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• pp.729-746
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• 2019

The nonlinear behavior of single- and multi-story steel plate shear walls (SPSWs) strengthened with three different patterns of fiber reinforced polymer (FRP) laminates (including single-strip, multi-strip and fully FRP-strengthened models) is studied using the finite element analysis. In the research, the effects of orientation, width, thickness and type (glass or carbon) of FRP sheets as well as the system aspect ratio and height are investigated. Results show that, despite an increase in the system strength using FRP sheets, ductility of reinforced SPSWs is decreased due to the delay in the initiation of yielding in the infill wall, while their initial stiffness does not change significantly. The content/type/reinforcement pattern of FRPs does affect the nonlinear behavior characteristics and also the mode and pattern of failure. In the case of multi-strip and fully FRP-strengthened models, the use of FPR sheets almost along the direction of the infill wall tension fields can maximize the effectiveness of reinforcement. In the case of single-strip pattern, the effectiveness of reinforcement is decreased for larger aspect ratios. Moreover, a relatively simplified and approximate theoretical procedure for estimating the strength of SPSWs reinforced with different patterns of FRP laminates is presented and compared with the analytical results.

• Steel and Composite Structures
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• 제34권2호
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• pp.241-260
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• 2020

This article presented a comprehensive model to study static buckling stability and associated mode-shapes of higher shear deformation theories of sandwich laminated composite beam under the compression of varying axial load function. Four higher order shear deformation beam theories are considered in formulation and analysis. So, the model can consider the influence of both thick and thin beams without needing to shear correction factor. The compression force can be described through axial direction by uniform constant, linear and parabolic distribution functions. The Hamilton's principle is exploited to derive equilibrium governing equations of unified sandwich laminated beams. The governing equilibrium differential equations are transformed to algebraic system of equations by using numerical differential quadrature method (DQM). The system of equations is solved as an eigenvalue problem to get critical buckling loads and their corresponding mode-shapes. The stability of DQM in determining of buckling loads of sandwich structure is performed. The validation studies are achieved and the obtained results are matched with those. Parametric studies are presented to figure out effects of in-plane load type, sandwich thickness, fiber orientation and boundary conditions on buckling loads and mode-shapes. The present model is important in designing process of aircraft, naval structural components, and naval structural when non-uniform in-plane compressive loading is dominated.

• Steel and Composite Structures
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• 제52권3호
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• pp.249-271
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• 2024

In this scientific work, an analytical solution for the dynamic analysis of cross-ply and angle-ply laminated composite plates is proposed. Due to technical issues during the manufacturing of composite materials, porosities and micro-voids can be produced within the composite material samples, which can carry on to a reduction in the density and strength of the materials. In this research, the laminated composite plates are assumed to have new distributions of porosities over the plate cross-section. The structure is modeled using a simple integral shear deformation theory in which the transverse shear deformation effect is included. The governing equations of motion are obtained employing the principle of Hamilton's. The solution is determined via Navier's approach. The Maple program is used to obtain the numerical results. In the numerical examples, the effects of geometry, ratio, modulus ratio, fiber orientation angle, number of layers and porosity parameter on the natural frequencies of symmetric and anti-symmetric laminated composite plates is presented and discussed in detail. Also, the impacts of the kinds of porosity distribution models on the natural frequencies of symmetric and anti-symmetric laminated composite plates are investigated.

• 한국항공우주학회지
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• 제32권7호
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• pp.29-36
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• 2004

본 연구에서는 전진비행시 무힌지 로터 블레이드의 허브하중에 대한 복합재료 연성의 영향을 고찰하였다. 무힌지 복합재료 로터 블레이드를 단일 상자형 보로 모델링 하였으며, 전단 변형 및 비틀림 워핑과 같은 비고전적 효과를 고려하였다. 운동방정식은 해밀턴의 원리를 이용하여 구성하였으며, 로터 블레이드의 공간 및 시간차원에서의 유한요소법을 적용하여 완전평형해석을 수행하였다. 블레이드에 작용하는 공기력은 2 차원 준정상 공기력 이론을 바탕으로 하여 역류 및 압축성 효과를 고려하였다. MSC/NASTRAN을 이용하여 피치 -플랩 및 피치-래그와 같은 탄성 연성의 크기를 구하고, 고전적인 기하학적 연계와 비교하였다. 탄생 연성은 $N_b/rev$ 허브하중의 특성에 적지 않은 영향을 미침을 확인하였다 블레이드 복합재료의 적층각을 적절히 변화시킬 경우 약 10-40%의 허브하중을 감소시킬 수 있음을 보였다.

• 한국강구조학회 논문집
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• 제10권2호통권35호
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• pp.201-209
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• 1998

강섬유보강 적층복합구조물에서 온도의 변화는 구조물의 응답에 중요한 영향을 미칠수 있다. 온도의 급작스런 변화는 재료의 강도와 성질을 현저히 저하시켜 구조물의 대변형, 좌굴, 고응력상태를 유발하는 중요한 인자가 된다. 본 연구에서는 등분포로 재하된 온도하중에 의한 적층복합판의 온도좌굴에 관한 해석을 수행하였다. 전단변형의 효과를 정확히 고려하기위해 5개의 변수로 구성된 고차전단변형이론을 적용하였다. 적층판의 배열각도, 적층판의 수, 폭-두께비의 변화, 형상비의 변화에 따른 임계좌굴온도를 구하여 1차전단변형이론에 의한 결과와 고전적이론에 의한 결과와 비교분석하였다.

• Steel and Composite Structures
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• 제47권2호
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• pp.217-238
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• 2023

In this study, a parametric study was performed considering material properties of concrete, material properties of steel, the number of longitudinal reinforcement (reinforcement ratio), CFRP ply orientations, a number of layers as variables by using ABAQUS. Firstly, the parameters used in the Hashin failure criteria were verified using four coupon tests of CFRP. Secondly, the numerical models of the beams strengthened by CFRP were verified using five experimental data. Finally, eighty numerical models and eighty analytic calculations were developed to investigate the effects of the aforementioned variables. The results revealed that in the case of using fibrous polymer to prevent shear failure, the variables related to reinforced concrete significantly affected the behavior of specimens, whereas the variables related to CFRP composite have a slight effect on the behavior of the specimens. As a result of numerical analysis, while the increase in the longitudinal tensile and compression reinforcement, load bearing capacity increases between 23.6%-70.7% and 5.6%-12.2%, respectively. Increase in compressive strength (29 MPa to 35 MPa) leads to a slight increase in the load-carrying capacity of the specimens between 4.6% and 7.2%. However, the decrease in the compressive strength (29 MPa to 20 MPa) significantly affected (between 6.4% and 8.1% decrease observed) the behavior of the specimens. As the yield strength increases or decreases, the capacity of specimens increase approximately 27.1% or decrease 12.1%. The effects of CFRP ply orientation results have been obtained as a negligible well approximately 3.7% difference. An increasing number of CFRP layers leads to almost no effect (approximately 2.8%) on the behavior of the specimen. Finally, according to the numerical analysis, the ductility values obtained between 4.0 and 6.9 indicate that the beams have sufficient ductility capacity.

• 접착 및 계면
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• 제9권3호
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• pp.7-13
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• 2008

열전도도가 유사한 입자형 필러인 silicon carbide (SiC)와 섬유형 필러인 carbon fiber (CF)를 polyetheretherketone (PEEK) 고분자에 첨가하여 복합재료의 열확산도에 미치는 영향을 연구하였다. 전자현미경을 통해 얻은 단면사진으로부터 SiC와 CF가 PEEK 매트릭스 안에 균일하게 분산되어 있고 필러들이 부분적으로 서로 네트워크를 형성한 것을 관찰하였다. 레이저 섬광법을 이용하여 상온에서 $200^{\circ}C$까지 PEEK/SiC와 PEEK/CF 복합재료의 열확산도를 측정하였으며, 열확산도는 온도가 상승함에 따라 PEEK-필러와 필러-필러 계면에서의 포논산란 증가에 의하여 감소하였다. 필러함량이 증가함에 따라 복합재료의 열확산도가 증가하였으며, 2상계에 대하여 유도된 Maxwell 및 Nielson 예측식을 실험값과 비교함으로써 매트릭스 내의 필러 분포, 방향성, 종횡비 및 필러간의 상호작용 등을 유추할 수 있었다. Nielson 예측식은 PEEK/SiC 복합재료에 대하여 열전도도를 잘 예측하였다. 입자형 필러인 SiC에 비하여 섬유형 필러인 탄소섬유가 동일한 함량에서 열확산에 기여하는 필러 네트워크를 효과적으로 형성하여 높은 열확산도를 가지는 것으로 추정된다.