• Advances in materials Research
• /
• 제5권1호
• /
• pp.11-20
• /
• 2016

In bonded composite repair of aircraft structures, the damage of the adhesive can thus reduce significantly the efficiency and the durability of the bonded composite repair. The adhesive damage models using critical zone have proven their effectiveness due to simplicity and ap-plicability of the damage criteria in these models. The scope of this study is to analyze the effects of the patch thickness and the adhesive thickness on the damage damage in bonded composite repair of aircraft structures by using modified damage zone theory. The obtained results show that, when the thickness of adhesive increases the damage zone increases and the adhesive loses its rigidity, inversely when the patch is reduced the adhesive damage be-comes more significant.

• Structural Engineering and Mechanics
• /
• 제59권1호
• /
• pp.123-132
• /
• 2016

Many military and commercial aging aircrafts flying beyond their design life may experience severe crack and corrosion damage, and thus lead to catastrophic failures. In this paper, were used in a finite element model to evaluate the effect of corrosion on the adhesive damage in bonded composite repair of aircraft structures. The damage zone theory was implemented in the finite element code in order to achieve this objective. In addition, the effect of the corrosion, on the repair efficiency. Four different patch shapes were chosen to analyze the adhesive damage: rectangular, trapezoidal, circular and elliptical. The modified damage zone theory was implemented in the FE code to evaluate the adhesive damage. The obtained results show that the adhesive damage localized on the level of corrosion and in the sides of patch, and the rectangular patch offers high safety it reduces considerably the risk of the adhesive failure.

• Composites Research
• /
• 제21권4호
• /
• pp.22-28
• /
• 2008

복합재료 체결부는 전체 복합재 구조물의 성능을 결정하는 중요한 부분이므로, 체결부에 대한 해석과 강도평가는 매우 중요하다. 본 논문에서는 복합재 접착 체결부의 강도를 실험적으로 평가하고 분석하였으며, 구조해석으로 평가한 체결부의 강도와 상호 비교하였다. 접착 체결부의 강도예측을 위하여 최대 변형률 이론과 파손영역 이론을 사용하였으며, 비선형 유한요소 해석을 통해 제안된 파손영역비를 기준으로 접착 체결부의 파손강도를 예측할 결과, 최대 22.2% 범위 내에서 파손강도를 예측할 수 있었다.

• Structural Monitoring and Maintenance
• /
• 제10권1호
• /
• pp.43-62
• /
• 2023

Damage monitoring is a prerequisite step to ensure the safety and performance of concrete structures. Smart aggregate (SA) technique has been proven for its advantage to detect early-stage internal cracks in concrete. In this study, a 1-D CNN-based method is developed for autonomously classifying the damage feature in a concrete anchorage zone using the raw impedance signatures of the embedded SA sensor. Firstly, an overview of the developed method is presented. The fundamental theory of the SA technique is outlined. Also, a 1-D CNN classification model using the impedance signals is constructed. Secondly, the experiment on the SA-embedded concrete anchorage zone is carried out, and the impedance signals of the SA sensor are recorded under different applied force levels. Finally, the feasibility of the developed 1-D CNN model is examined to classify concrete damage features via noise-contaminated signals. The results show that the developed method can accurately classify the damaged features in the concrete anchorage zone.

• 한국항공우주학회지
• /
• 제38권2호
• /
• pp.111-118
• /
• 2010

복합재료 구조물에서 조인트 부위는 매우 취약한 부분이다. 본 논문에서는 후판 알루미늄-알루미늄 조인트 및 복합재-알루미늄 조인트를 접착제로 접합하여 제작한 다음, 인장실험을 수행하여 파손형태를 고찰하였다. 또한, 항복 변형률에 기초한 수정 파손영역 이론을 제안하였으며, 파괴모드별 파손하중과 상호 비교하였다. 후판 알루미늄-알루미늄 조인트와 복합재-알루미늄 조인트의 파손강도를 동일한 파손기준값을 적용하여 예측하였으며, 제작된 14종류의 시편에서는 최대 19.3% 오차범위 내에서 파손강도를 예측할 수 있었다.

• 한국전산구조공학회논문집
• /
• 제13권2호
• /
• pp.257-270
• /
• 2000

본 연구는 결함을 지닌 구조체의 거시적인 역학적 거동을 손상역학이론에 근거하여 해석할 수 있는 손상모델을 개발하고 이를 손상을 입은 구조체에 적용하여 손상된 구조체의 전체거동을 해석적으로 규명하는데 그 목적이 있다. 이를 위하여 수정된 2차손상텐서를 이용하였으며, 유효응력을 통해서 산정된 손상응력을 절점에 작용하는 추가의 하중 항으로 고려할 수 있고 균열면의 성질을 반영할 수 있는 유한요소해석 알고리즘을 개발하였다. 개발된 알고리즘은 실험치 및 횡등방성 이론에 의한 이론치와의 비교·검증을 통하여 그 신뢰성을 검토하였다. 선형탄성 가정 하에서 균열을 지닌 구조체에 개발된 알고리즘을 적용하여 해석한 결과, 균열의 방향과 균열군에 따른 손상된 구조체의 거동을 정량적으로 추정할 수 있었다. 개발된 모델을 균열이 존재하는 암반의 굴착문제와 파쇄대를 지니고 있는 지하구조체 문제에 적용해 본 결과, 손상으로 인해 야기되는 구조체의 전체 거동상의 차이를 규명할 수 있었다.

• 한국콘크리트학회:학술대회논문집
• /
• 한국콘크리트학회 1997년도 가을 학술발표회 논문집
• /
• pp.552-557
• /
• 1997

In this study, a quantitative analysis technique for the damage process of reinforced concrete beams under repeated shear loading is proposed, which can express the progressively increasing strain and stiffness reduction. The analysis technique is mainly based on the modified compression field theory and scalar damage concept. which describe the strain and stress configuration in the shear zone by considering the 2-dimensional effect, and express the degradation of principal compressive strut by cyclic strain increment, secant modulus decrement, and modifying the parabolic stress strain relationship. The analysis of the response of RC beams under repeated shear-flexure loading has been carried out and compared with the experimental results. The present theory may efficiently be used to evaluate the deflection and strain accumulation under repeated loadings.

• Structural Engineering and Mechanics
• /
• 제53권3호
• /
• pp.481-495
• /
• 2015

Many hydropower stations in southwest China are located in regions of brittle rock mass with high geo-stresses. Under these conditions deep fractured zones often occur in the sidewalls of the underground caverns of a power station. The theory and methods of fracture and damage mechanics are therefore adopted to study the phenomena. First a flexibility matrix is developed to describe initial geometric imperfections of a jointed rock mass. This model takes into account the area and orientation of the fractured surfaces of multiple joint sets, as well as spacing and density of joints. Using the assumption of the equivalent strain principle, a damage constitutive model is established based on the brittle fracture criterion. In addition the theory of fracture mechanics is applied to analyze the occurrence of secondary cracks during a cavern excavation. The failure criterion, for rock bridge coalescence and the damage evolution equation, has been derived and a new sub-program integrated into the FLAC-3D software. The model has then been applied to the stability analysis of an underground cavern group of a hydropower station in Sichuan province, China. The results of this method are compared with those obtained by using a conventional elasto-plastic model and splitting depth calculated by the splitting failure criterion proposed in a previous study. The results are also compared with the depth of the relaxation and fracture zone in the surrounding rock measured by field monitoring. The distribution of the splitting zone obtained both by the proposed model and by the field monitoring measurements are consistent to the validity of the theory developed herein.

• Composites Research
• /
• 제22권2호
• /
• pp.7-13
• /
• 2009

복합재료가 항공기 구조물 및 기계 부품 등에 폭 넓게 적용됨에 따라, 복합재료 구조들에서 가장 취약한 복합재료 체결부의 설계는 매우 중요한 연구분야로 대두되긴 있다. 본 논문에서는 접착 체결구조와 기계적 체결구조의 조합으로 되어 있는 하이브리드 조인트의 파손강도를 평가하고 예측하였다. 피착제의 두께, w/d, e/d가 서로 다른 10가지 하이브리드 조인트 시험편을 제작하여 평가하였다. 접착 체결구조와 기계적 체결구조의 파손 판정을 위해 파손영역법과 파괴면적지수법이 각각 적용 되었으며, 두 체결부위 중 어느 한족이 먼저 파손기준에 도달할 경우, 하이브리드 조인트가 파손되었다고 가정하였다. 이상의 실험과 해석결과로부터, 하이브리드 조인트 시편의 파손강도는 25.5%, 오차 범위 내에서 예측할 수 있었다.

• 한국복합재료학회:학술대회논문집
• /
• 한국복합재료학회 2005년도 춘계학술발표대회 논문집
• /
• pp.240-244
• /
• 2005

In this study a simple model is developed that predicts impact damage in a composite laminate using an analytical model. The model uses a non-linear approximation method (Rayleigh-Ritz) and the large deflection plate theory to predict the number of failed plies and damage area in a quasi-isotropic composite circular plate (axisymmetric problem) due to a point impact load at its centre. It is assumed that the deformation due to a static transverse load is similar to that occurred in a low velocity impact. It is found that the model, despite its simplicity, is in good agreement with FEM predictions and experimental data for the deflection of the composite plate and gives a good estimate of the number of failed plies due to fibre breakage. The predicted damage zone could be used with a fracture mechanics model developed by the second investigator and co-workers to calculate the compression after impact strength of such laminates. This approach could save significant running time when compared to FEM solutions.