• 한국소음진동공학회:학술대회논문집
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• 한국소음진동공학회 2005년도 춘계학술대회논문집
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• pp.322-325
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• 2005

The separation mechanism is installed to separate a note one by one from the stacked notes and the overlap type, one of separation mechanism, has been used a lot in financial equipments like ATM. This paper has compared and estimated analysis results using finite element method with experimental results over various parameters such as conditions of note, overlap value, roller shapes, which affect the friction force (resistance) exerting on notes between rollers. Consequently, the effect of various parameters on the performance of overlap type separation mechanism can be known and optimal shape and overlap value can be obtained.

• 항공우주시스템공학회지
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• 제12권5호
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• pp.69-75
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• 2018

본 논문에서는 전기 접속부 역할을 하는 포고핀을 활용한 극초소형 위성용 나일론선 절단방식 태양전지판 분리장치를 제안하였다. 제안된 분리장치는 종래 나일론선을 이용한 분리장치에 비해 높은 체결력 및 횡/종방향 동시구속이 가능하고, 체결작업이 용이하며, 또한 다수의 태양전지판의 동시분리가 가능한 장점을 갖는다. 또한 제안된 분리장치에 적용된 포고핀은 전력공급을 위한 전기 접속부 기능과 함께 전개 상태 스위치 및 태양전지판의 분리 스프링 역할이 동시에 가능하다. 본 논문에서는 제안된 포고핀 분리장치의 기능성 입증을 위해 체결횟수에 따른 분리 기능시험을 통해 기능성을 검증하였다.

• 한국자동차공학회논문집
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• 제14권6호
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• pp.66-72
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• 2006

In this paper, an analytical investigation on the track separation mechanism for tracked excavator was studied. Relative motions of track links, sprocket, idler and support rollers are very important in the driving of an excavator The interference and friction between each components lead to noise and vibration. And also this has a great influence on the life for tracked excavator. RecurDyn program was used for the three dimensional modeling of the track assembly. Investigating the interference between sprocket and track links, the mechanism of the track separation was analyzed.

• 항공우주시스템공학회지
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• 제7권3호
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• pp.20-25
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• 2013

In case of cube satellite, it is difficult to realize the same performance as commercial satellite due to its highly restricted unit accommodation space. To maximize the performance of the cube satellite, design concept considering the multi-function of satellite is required. In this paper, mechanism design of cube satellite which is applicable for the holding and release of multi-deployable structures has been proposed and investigated. In addition, a switch mechanism design for the autonomous system operation just after the cube satellite separation from P-POD has also been proposed. The effectiveness of the mechanism design for holding and release of multi-deployable structures has been demonstrated by EM test of the holding and release mechanism.

• 대한임상검사과학회지
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• 제36권2호
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• pp.115-120
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• 2004

혼합 amino acid의 선택적 분리를 위해 bulk liquid membrane system을 이용하였으며, p-diamethylaminobenzaldehyde(DAB), sulfosalicylic acid (SSA), 1-naphtol이 amino acid의 선택적 분리를 위한 효과적인 carrier로 사용될 수 있음을 확인하였다. 그 결과 sulfosalicylicacid에 대해서 Ala에 대한 선택성을 관찰할 수 있었으며, 1-naphtol에 대해서는 염기성 상태에서 Leu을 약산성 및 중성상태에서는 Val을 선택적으로 분리할 수 있었다. DAB에 대해서는 강산성에서 Phe을, 강알카리 조건에서 Ile를 선택적으로 분리할 수 있었다. Separation mechanism은 SSA와 1-naphtol의 경우에는 ion pair mechanism으로, DAB의 경우에는 imine 결합의 생성반응으로 설명할 수 있었다. 따라서, Liquid membrane을 이용한 생체시료 내의 아미노산을 선택적으로 분리함에 유용성이 클 것으로 사료된다.

• 한국전산유체공학회:학술대회논문집
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• 한국전산유체공학회 2007년도 추계 학술대회논문집
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• pp.60-66
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• 2007

Separation control has been performed using synthetic jets on airfoil at high angle of attack. Computed results demonstrated that stall characteristics and control surface performance could be substantially improved by resizing separation vortices. It was observed that the actual flow control mechanism and flow structure is fundamentally different depending on the range of synthetic jet frequency. For low frequency range, small vortices due to synthetic jet penetrated to the large leading edge separation vortex, and as a result, the size of the leading edge vortex was remarkably reduced. For high frequency range, however, small vortex did not grow up enough to penetrate into the leading edge separation vortex. Instead, synthetic jet firmly attached the local flow and influenced the circulation of the virtual airfoil shape which is the combined shape of the main airfoil with the separation vortex. Theses results show the characteristic of unsteady flow of single synthetic jet. Beside, we researched on multi-array synthetic jet to obtain applicable synthetic jet velocity. Multi-location synthetic jet is proposed to eliminate small vortex on suction surface of airfoil. With the results, we concluded that the flow around airfoil is stable by high frequency synthetic jet with elimination of small vortex and confirmation of stable flow. Moreover, performance of multi-array/multi-location synthetic jet can be improved by changing phase angle of multi-location synthetic jet.

• 한국추진공학회:학술대회논문집
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• 한국추진공학회 2004년도 제22회 춘계학술대회논문집
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• pp.532-543
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• 2004

The present work have been developed the interpretation processor including the behavior of material failure and the separation phenomena under transient dynamic loading (the operation of explosive bolt) using AUTODYN V4.3, SoildWork 2003 and TrueGrid V2.1 programs. It has been demonstrated that the interpretation in ridge-cut explosive bolt under dynamic loading condition should be necessary to the appropriate failure model and the basic stress of bolt failure is the principal stress. The use of this interpretation processor developing the present work could be extensively helped to design the shape and the amount of explosives in the explosive bolt having a complex geometry. It is also proved that the interpretation processor approach is an accurate and effective analysis technique to evaluate the separation mechanism in explosive bolts.

• Journal of Biosystems Engineering
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• 제28권1호
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• pp.19-26
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• 2003

An oscillating digger mechanism was designed, constructed. and tested. The mechanism is consisted of a six-bar linkage, one four-bar linkage was fer the digger blade and the other one fur variable soil-crop separation. Experimental variables were amplitude(3, 6, 9 mm). frequency(11.2, 14.9. 17.0 Hz), and forward speed of tractor(0.91, 1.13, 1.56 km/h). Each combination of these variables was replicated three times to measure the draft and torque for power requirement evaluation. and the broken-up soil height on the soil separation sieve mechanism. Four parameters λ(the ratio of vibration speed to forward velocity), p(the ratio of vibration acceleration to forward velocity), K(the ratio of vibration acceleration to gravitational acceleration), and T(the product of λ and K) were induced from three experimental variables: amplitude, frequency, and tractor speed. And the power requirement and soil separation ability were analyzed by regression. Though λ and K were known to be the representative parameters. T was the most moderate one to explain draft. torque. and soil separation in this study. It was estimated that the T equal to or greater than 2.4 was the minimum recommended value. Figure 18 would be useful fir the selection of amplitude. frequency, or operating tractor speed once any two variables are known.

• 한국응용과학기술학회지
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• 제28권4호
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• pp.386-392
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• 2011

We are crystallized to the linear low density polyethylene(LLDPE) particles by a thermally induced phase separation(TIPS). TIPS process based on the phase separation mechanism was performed for the LLDPE system which undergoes liquid-solid phase separation. The linear low density polyethylene particle formation occurred by the nucleation and growth mechanism in the metastable region. Although the growth rates depended on the experimental conditions such as the polymer concentration and temperature, the particles were larger when the polymer concentration was higher or temperature was higher. The particles were observed by SEM. The LLDPE particle size distribution became broader when the polymer concentration was higher.

• 한국항공우주학회지
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• 제41권10호
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• pp.827-832
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• 2013

극초소형 위성으로 분류되는 큐브위성의 경우, 1U를 기준으로 $10cm{\times}10cm{\times}10cm$의 크기, 1kg 이하의 중량제한을 비롯해 폭발식 구속분리장치의 적용이 불가한 설계요구조건으로 인하여 열선 작동시 나일론선의 절단과 함께 구속을 해제하는 구속분리 방식이 일반적으로 적용되고 있으나 낮은 체결력과 다수 구조물의 구속 시 다수의 열선 적용을 필요로 하는 등 시스템 복잡화의 단점이 존재한다. 본 논문에서는 기존의 큐브위성에 적용되는 열선 절단방식의 단점을 극복하기 위하여 열선절단방식을 적용한 분리너트형 비폭발식 구속분리장치를 고안하였으며, 인증모델의 기능시험, 정하중시험 및 충격시험을 통해 설계 유효성을 입증하였다.