• Advances in aircraft and spacecraft science
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• 제11권1호
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• pp.83-103
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• 2024

Adhesive bonding is currently widely used in many industrial fields, particularly in the aeronautics sector. Despite its advantages over mechanical joints such as riveting and welding, adhesive bonding is mostly used for secondary structures due to its low peel strength; especially if it is simultaneously exposed to temperature and humidity; and often presence of bonding defects. In fact, during joint preparation, several types of defects can be introduced into the adhesive layer such as air bubbles, cavities, or cracks, which induce stress concentrations potentially leading to premature failure. Indeed, the presence of defects in the adhesive joint has a significant effect on adhesive stresses, which emphasizes the need for a good surface treatment. The research in this field is aimed at minimizing the stresses in the adhesive joint at its free edges by geometric modifications of the ovelapping part and/or by changing the nature of the substrates. In this study, the finite element method is used to describe the mechanical behavior of bonded joints. Thus, a three-dimensional model is made to analyze the effect of defects in the adhesive joint at areas of high stress concentrations. The analysis consists of estimating the different stresses in an adhesive joint between two 2024-T3 aluminum plates. Two types of single lap joints(SLJ) were analyzed: a standard SLJ and another modified by removing 0.2 mm of material from the thickness of one plate along the overlap length, taking into account several factors such as the applied load, shape, size and position of the defect. The obtained results clearly show that the presence of a bonding defect significantly affects stresses in the adhesive joint, which become important if the joint is subjected to a higher applied load. On the other hand, the geometric modification made to the plate considerably reduces the various stresses in the adhesive joint even in the presence of a bonding defect.

• 실천공학교육논문지
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• 제15권1호
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• pp.119-126
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• 2023

오늘날 자동차의 연비 향상 과 동적 거동 향상을 위해서 자동차 부품의 경량화 및 간소화 시대가 형성되고 있다. 설계와 제작의 간소화를 위해 제품 형상을 다양한 부품의 일체화로 진행되고 있다. 예를 들어 3개의 제품을 1개의 제품화 시키기 위해서 아주 협소한 부분까지 제품 가공하는 일이 발생되고 있다. 기존의 부품의 경우 가공의 편의성을 위해 정밀 다이캐스팅 또는 주물 생산으로 가공 후 조립하는데 다중 조립체(multi-piece) 방식은 공정수가 많이 필요로 하며, 부품의 정밀도와 강도를 저하시키는 요인이 된다. 가공 공정을 단순화 시키고 부품의 강도를 확보하기 위해서 일체형으로 제작하는 것이 단점을 극복하는데 매우 유리하지만 깊고 좁은 포켓 부분을 가공 할 경우 장비 자체 스핀들로는 가공이 불가능하다. 문제점을 해결하고자 절삭가공에 대한 연구가 활발하게 진행되고 있으며, 다축 복합가공 기술은 이러한 문제점을 해결할 뿐만 아니라, 지금까지 하나의 공작기계로 여러 공정에 따른 유연한 절삭가공이 어려웠던 복합 형상에도 절삭가공이 가능하다는 등 많은 장점을 가지고 있다. 하지만 고가의 장비로 인하여 제조경비 상승과 기계를 운영할 수 있는 기술자가 부족한 것이 현실이다. 5축 절삭 가공기에서는 깊고 협소한 구간의 제품을 생산할 때 공구의 간접으로 제품 생산에 사이클 타임이 늘어남은 물론 가공상에 문제점들이 많이 발생된다. 따라서 전용 공작기계 및 다축 복합가공기를 사용해야 한다. 그 대안으로 3축 머시닝센터에서 5축 이상의 다축 복합가공을 할 수 있는 특수 공구로서의 앵글 스핀들(angle spinde)이 사용될 수 있다. 앵글 스핀들 사용함으로 가공 진동 흡수, 낮은 열 발생과 작동 안정성, 우수한 치수 안정성, 강도 확보와 같은 분야에서 다양하고 지속적인 연구가 필요하다.

• 한국결정성장학회:학술대회논문집
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• 한국결정성장학회 1996년도 The 9th KACG Technical Annual Meeting and the 3rd Korea-Japan EMGS (Electronic Materials Growth Symposium)
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• pp.179-200
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• 1996

The intrinsic instabilities of fluid flow occurred in the melt of the Czochralski crystal growth system Czochralski method, asymmetric flow patterns and temperature profiles in the melt have been studied by many researchers. The idea that the non-symmetric structure of the growing equipment is responsible for the asymmetric profiles is usually accepted at the first time. However further researches revealed that some intrinsic instabilities not related to the non-symmetric equipment structure in the melt could also appear. Ristorcelli had pointed out that there are many possible causes of instabilities in the melt. The instabilities appears because of the coupling effects of fluid flow and temperature profiles in the melt. Among the instabilities, the B nard type instabilities with no or low crucible rotation rates are analyzed by the visualizing experiments using X-ray radiography and the 3-D numerical simulation in this study. The velocity profiles in the Silicon melt at different crucible rotation rates were measured using X-ray radiography method using tungsten tracers in the melt. The results showed that there exits two types of fluid flow mode. One is axisymmetric flow, the other is asymmetric flow. In the axisymmetric flow, the trajectory of the tracers show torus pattern. However, more exact measurement of the axisymmetrc case shows that this flow field has small non-axisymmetric components of the velocity. When fluid flow is asymmetric, the tracers show random motion from the fixed view point. On the other hand, when the observer rotates to the same velocity of the crucible, the trajectory of the tracer show a rotating motion, the center of the motion is not same the center of the melt. The temperature of a point in the melt were measured using thermocouples with different rotating rates. Measured temperatures oscillated. Such kind of oscillations are also measured by the other researchers. The behavior of temperature oscillations were quite different between at low rotations and at high rotations. Above experimental results means that the fluid flow and temperature profiles in the melt is not symmetric, and then the mode of the asymmetric is changed when rotation rates are changed. To compare with these experimental results, the fluid flow and temperature profiles at no rotation and 8 rpm of crucible rotation rates on the same size of crucible is calculated using a 3-dimensional numerical simulation. A finite different method is adopted for this simulation. 50×30×30 grids are used. The numerical simulation also showed that the velocity and flow profiles are changed when rotation rates change. Futhermore, the flow patterns and temperature profiles of both cases are not axisymmetric even though axisymmetric boundary conditions are used. Several cells appear at no rotation. The cells are formed by the unstable vertical temperature profiles (upper region is colder than lower part) beneath the free surface of the melt. When the temperature profile is combined with density difference (Rayleigh-B nard instability) or surface tension difference (Marangoni-B nard instability) on temperature, cell structures are naturally formed. Both sources of instabilities are coupled to the cell structures in the melt of the Czochralski process. With high rotation rates, the shape of the fluid field is changed to another type of asymmetric profile. Because of the velocity profile, isothermal lines on the plane vertical to the centerline change to elliptic. When the velocity profiles are plotted at the rotating view point, two vortices appear at the both sides of centerline. These vortices seem to be the main reason of the tracer behavior shown in the asymmetric velocity experiment. This profile is quite similar to the profiles created by the baroclinic instability on the rotating annulus. The temperature profiles obtained from the numerical calculations and Fourier transforms of it are quite similar to the results of the experiment. bove esults intend that at least two types of intrinsic instabilities can occur in the melt of Czochralski growing systems. Because the instabilities cause temperature fluctuations in the melt and near the crystal-melt interface, some defects may be generated by them. When the crucible size becomes large, the intensity of the instabilities should increase. Therefore, to produce large single crystals with good quality, the behavior of the intrinsic instabilities in the melt as well as the effects of the instabilities on the defects in the ingot should be studied. As one of the cause of the defects in the large diameter Silicon single crystal grown by the