• 대한기계학회:학술대회논문집
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• 대한기계학회 2003년도 춘계학술대회
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• pp.381-388
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• 2003

The material deficiencies in the form of pre-existing defects can initiated cracks and fractures. The stress distribution and fatigue crack initiation life of engineering materials may be associated with the size, the shape and the relative location of defects contained in the component. The objective of this study is to investigate the effect of arbitrarily located hole defect around the rivet hole of a wing section in monolithic aluminum and Al/GFRP laminates under cyclic bending moment during a service load. The stress distribution and the fatigue crack initiation behavior near a rivet hole of on the relationships between stress concentration factor ($K_t$) and relative position of defects were considered. The test results indicated the features of different stress field. Therefore, the stress concentration factor ($K_t$) and the fatigue crack initiation behavior was illustrated different behavior according to each position of hole defect around the rivet hole in monolithic aluminum and Al/GFRP laminates.

• 한국복합재료학회:학술대회논문집
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• 한국복합재료학회 2005년도 춘계학술발표대회 논문집
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• pp.121-124
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• 2005

This paper was about experimental test properties by mechnical joint of CF1263/Epoxy Al honeycomb panels. In case of mechanical joint using screw, nut shall be secured over than minimize third screw pitch. In case of insert backsheet for increase of joint force, increase weight for assemble by screw pitch. In case of insert backsheet with CF1263/Epoxy, predominant save weight and minimazer of displacement by tensile weight moreover predominant strength. In case of mechanical joint by rivet, rivet of Monobolt has over-hole in hole of CF1263/Epoxy but rivet of PROTRUDING has predominant of mechanical joint.

• 비파괴검사학회지
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• 제21권4호
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• pp.398-405
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• 2001

리벳이음은 응력집중 등에 의한 피로균열 발생 가능성이 높은 구조특성을 가지므로 구조물의 안전성 확보를 위하여 비파괴 평가 방법에 의하여 리벳홀 주위 균열에 대한 평가가 요구되고 있다. 유도 초음파의 일종인 Lamb파는 판형상의 구조물의 비파괴 평가에 적합하며, 신경회로망은 비파괴 평가 기술에서 결합의 크기 및 종류 인식에 관하여 가장 효율적인 기법으로 많은 연구자들에 의해 적용되어 왔다. 본 연구에서는 항공기의 스킨재료로 적용되는 A12024-T3판재에 대하여 유도초음파의 일종인 판파를 적용하여 리벳홀 주위 균열 신호를 검출하였으며, 또한 리벳홀 주위 균열의 크기 평가를 위하여 백프로퍼게이션 알고리즘을 적용한 신경회로망을 적용하였다. 이때, 초음파 트랜스듀서와 시험편 사이의 불균일 접촉에 의한 오차를 줄이기 위하여 초음파 파형에서 시간 및 주파수 성분의 특성을 추출하여 신경회로망에 적용하였다. 그리고 이들 판파신호에서 추출한 시간 및 주파수 성분의 특성은 균열 크기 결정에 유용하게 적용될 수 있음을 증명하였다.

• 한국해양공학회지
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• 제15권1호
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• pp.52-56
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• 2001

This study were looks at the effect of the initial cut length or stress concentration level, on the wave forms produced by crack propagation. The signals were collected, then classified visually for each type of sample. They were put into three classes according to their shapes in the time and frequency domain. Each class should domain signals which could be correlated to a certain micro-failure mechanism that occurs during the fatigue process. Classes of these signals compared, with each sample. To see if there were any classes common to the three samples. The fatigue test attempted to determine if the initial cut length has any influence on the type of signals.

• 한국정밀공학회지
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• 제33권2호
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• pp.121-128
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• 2016

The mechanical jointing method is very important in the machine parts and structure. They are used by the bolts and rivet because it is very convenient to replace the parts and the structure. However, the mechanical jointing methods using the bolt and rivet needed the open hole. The machine parts life cycle is reduced because this open hole created the stress concentration. Therefore, the measurement methods are needed to evaluate phenomenon of the stress concentration. This paper discusses the development of the measurement algorithm using the digital image correlation methods to measure the strain distribution of the open hole. To implement the measurement algorithm using the DIC, the LabVIEW 2010 programming tool was used. To measure the strain distribution of the open hole, the tensile specimens having an open hole are made by using the aluminum 6061-T6. To secure the reliability of measurement result using the DIC, the DIC measurement results and FEM analysis results were compared.

• 소성∙가공
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• 제29권6호
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• pp.331-337
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• 2020

Blind rivet nuts (BRNs) are increasingly used in automotive industry because unlike conventional bolt fastening, BRN fastening requires access from one side only. Generally, fastening is conducted using automated units, but manual fastening may be resorted to in case of small quantities. Since the fastening direction is not exactly perpendicular to the sheet metal, the BRN axis is tilted with respect to the plate and may result in damage or incomplete fastening. As the tilt angle (clamping angle α) increases, undesired plate deformation occurs and the contact area of the plate with the BRN fastening area decreases, reducing the clamping effect. In this study, the reduction of the clamping effect with the α was investigated to ensure stable fastening force. M6 BRNs were used in the tests. The fastening force was measured as follows: the plate was cut in half through the center of the hole; the BRN was inserted into the hole and fastened; and the clamping angle a was measured (values, 0° ≤ α ≤ 9°). The force leading to the separation of the halves was measured using a universal testing machine (UTM). The maximum α range, in which the fastening force remains stable, was determined. Finite element (FE) analysis confirmed that the fastening force decreases approximately linearly with increasing α. Based on the experiment and FE analysis using various α, the fastening force was found to decrease with α. Further, the maximum tolerance for α that provides secure fastening without damage is suggested.

• Structural Engineering and Mechanics
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• 제31권4호
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• pp.439-451
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• 2009

The paper deals with the problem related to the modelling of riveted assemblies for crashworthiness analysis of full-scale complete aircraft structures. Comparisons between experiments and standard FE computations on high-energy accidental situations onto aluminium riveted panels show that macroscopic plastic strains are not sufficiently localised in the FE shells connected to rivet elements. The main reason is related to the structural embrittlement caused by holes, which are currently not modelled. Consequently, standard displacement FE models do not succeed in initialising and propagating the rupture in sheet metal plates and along rivet rows as observed in the experiments. However, the literature survey show that it is possible to formulate super-elements featuring defects that both give accurate singular strain fields and are compatible with standard displacement finite elements. These super-elements can be related to the displacement model of the hybrid-Trefftz principle of the finite element method, which is a kind of domain decomposition method. A feature of hybrid-Trefftz finite elements is that they are mainly used for elastic computations. It is thus proposed to investigate the possibility of formulating a hybrid displacement finite element, including the effects of a hole, dedicated to crashworthiness analysis of full-scale aeronautic structures.

• 한국멀티미디어학회논문지
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• 제13권4호
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• pp.512-525
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• 2010

PDP(Plasma Display Panel) 프레임은 PDP의 핵심 부품으로 매월 수 십 만개 이상을 생산하고 있다. 대량생산 과정에서 제품의 검사 과정은 매우 중요한 공정 단계이며 제품의 신뢰성을 높이기 위해 모든 부품과 완제품에 대한 전수 검사가 종종 요구되고 있다. 본 논문에서 구현 하고자 하는 시각 검사 공정의 자동화는 생산 현장에서 컴퓨터 비전 기술을 이용하여 PDP 부품의 일부인 프레임의 결함을 검사한다. 본 논문은 PDP 프레임에 있는 홀(Hole), 탭홀(Tab), 스터드(STUD), 리벳(Rivet)의 결함을 검사하는 시스템을 설계하고 구현 하였다. 본 시스템은 다양한 종류의 PDP 프레임을 학습하고 검사 할 수 있다. 모든 제품에 대한 신속하고 정확하게 100% 검사를 함으로써 공정의 효율성을 높이고 검사결과의 데이터베이스화로 신속한 결함의 원인파악과 조치가 가능하도록 하였다. 시스템을 산업체에 적용한 결과 신속하고 정확한 검사가 가능함을 보였다.

• 한국전산구조공학회논문집
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• 제29권6호
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• pp.491-498
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• 2016

리벳이나 볼트가 결합되는 구멍은 항공기, 선박 및 기타 구조물에 사용되는 판재의 응력 집중을 유발한다. 과도한 응력 집중 현상이 지속되면 종래에는 파단이 일어날 수 있으므로 설계 단계에서 응력 집중 현상의 명확한 해석이 중요하다. 이 논문에서는 판재위에 리벳을 배치하는 간단한 최적화 방법이 제시되었다. 첫째로 응력 집중 현상 해석에서 FEM 구조 해석이 얼마나 정확한지 검증하였다. 평판 위에 존재하는 단일 구멍의 반경을 바꿔가며 응력 집중 계수의 변화를 분석하였다. 같은 방법으로 일렬로 존재하는 구멍들 사이에서의 응력 집중 계수를 수치 해석하였다. 각각의 응력 집중 계수를 이론값과 비교하여 정확도를 확인하였다. 마지막으로 두 응력 집중 현상을 독립적으로 적용하는 최적화 방법을 확인 및 검증하였다. 이 결과들은 이론적인 예측과 밀접한 경향성을 보여 앞으로의 리벳 배치 최적화에도 활용될 수 있을 것으로 예상된다.

• Advances in aircraft and spacecraft science
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• 제4권1호
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• pp.1-19
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• 2017

Fatigue life prediction of a multi-row countersunk riveted lap joint was performed numerically. The stress and strain conditions in a highly stressed substructure of the joint were analysed using a global/local finite element (FE) model coupling approach. After validation of the FE models using experimental strain measurements, the stress/strain condition in the local three-dimensional (3D) FE model was simulated under a fatigue loading condition. This local model involved multiple load cases with nonlinearity in material properties, geometric deformation, and contact boundary conditions. The resulting stresses and strains were used in the Smith-Watson-Topper (SWT) strain life equation to assess the fatigue "initiation life", defined as the life to a 0.5 mm deep crack. Effects of the rivet-hole clearance and rivet head deformation on the predicted fatigue life were identified, and good agreement in the fatigue life was obtained between the experimental and the numerical results. Further crack growth from a 0.5 mm crack to the first linkup of two adjacent cracks was evaluated using the NRC in-house tool, CanGROW. Good correlation in the fatigue life was also obtained between the experimental result and the crack growth analysis. The study shows that the selected methodology is promising for assessing the fatigue life for the lap joint, which is expected to improve research efficiency by reducing test quantity and cost.