• Title/Summary/Keyword: Separation Mechanism

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The Finite Element Analysis and Experiment of Flexible Media Separation Mechanism (유연매체 분리기구의 유한요소해석과 실험)

  • Yoon, You-Hoon;Baek, Yoon-Kil;Yoon, Joon-Hyun
    • Proceedings of the Korean Society for Noise and Vibration Engineering Conference
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    • 2005.05a
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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.

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Functional Verification of the Solar Panel Separation Mechanism for Pico-Class Satellite Applications Using Spring-loaded Pogo-pin (포고핀을 활용한 극초소형 위성용 태양전지판 분리장치의 기능검증)

  • Kim, Su-Hyeon;Jeon, Young-Hyeon;Kim, Hong-Rae;Oh, Hyun-Ung
    • Journal of Aerospace System Engineering
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    • v.12 no.5
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    • pp.69-75
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    • 2018
  • In this study, we proposed a nylon wire cutting-type solar panel separation mechanism for CubeSat applications using spring-loaded pogo-pins, which has been widely used as temporary electrical interface between two separate electronics. The mechanism proposed in this study has great advantages of higher holding capability, ability to constrain along in-plane and out-of-plane directions of solar panels, simplicity in tightening of nylon wire and synchronous separation of multiple panels. In addition, the pogo-pins used for the proposed mechanism act as electrical power interface, separation status switch and separation spring. In this study, the functionality of the proposed mechanism was validated through the separation tests with various number of nylon wire windings.

Analytical Investigation on the Track Separation Mechanism for Tracked Excavator (굴삭기 트랙의 궤도 이탈현상에 관한 해석적 연구)

  • Lee, Yun-Sig;Ok, Jin-Kyu;Kim, Hyo-Joon;Yoo, Wan-Suk
    • Transactions of the Korean Society of Automotive Engineers
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    • v.14 no.6
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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.

Mechanism Design of Cube Satellite for Multi-deployable Structures and Autonomous System Operation after Launcher Separation (복수구조 전개 및 발사체 분리직후 시스템 자동운용을 위한 큐브위성의 메커니즘 설계)

  • Lee, Myoung-Jae;Jung, Hyun-Mo;Oh, Hyun-Ung
    • Journal of Aerospace System Engineering
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    • v.7 no.3
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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.

Selective Separation of Amino Acid Mixture Using H2O-CH2Cl2-H2O Liquid Membrane containing p-Dimethylaminobenzaldehyde, 1-Napthol and Sulfosalicylic acid as a Carrier (II) (p-Dimethylaminobenzaldehyde, 1-Naphtol, Sulfosalicylic acid 등의 Carrier를 함유하는 H2O-CH2Cl2-H2O Liquid Membrane을 이용한 아미노산의 선택적 분리(II))

  • Park, Chung Oh;Hong, Jae Jin
    • Korean Journal of Clinical Laboratory Science
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    • v.36 no.2
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    • pp.115-120
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    • 2004
  • A bulk liquid membrane system was introduced for selective separation of an amino acid mixture. We confirmed p-diamethylaminobenzaldehyde (DAB), sulfosalicylic acid (SSA) and 1-naphtol were very useful carriers for selective separation of an amino acid mixture. As a result, Ala, Leu, Val, Phe and Ile were successfully separated by SSA, 1-naphtol in basic condition, 1-naphtol in weak acidic condition, DAB in strong acidic condition and DAB in strong basic condition. The separation mechanism was proposed by ion pair mechanism in the case of SSA and 1-naphtol and Imine bond formation mechanism was also introduced for DAB.

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SEPARATION CONTROL MECHANISM USING SYNTHETIC JET ON AIRFOIL (익형에서의 synthetic jet을 이용한 박리제어 mechanism)

  • Kim, S.H.;Kim, W.;Hong, W.;Kim, C.
    • 한국전산유체공학회:학술대회논문집
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    • 2007.10a
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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.

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The Interpretation of Separation Mechanism of Ridge-Cut Explosive Bolt Using Software Simulation Program

  • Lee, Y. J.;Kim, D. J.
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2004.03a
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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.

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Design Parameters of A Six-bar Linkage Vibrating Digger (6절 링크를 이용한 진동굴취기의 설계요인)

  • 문학수;강화석
    • Journal of Biosystems Engineering
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    • v.28 no.1
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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.

A Study on the Preparation of a Linear Low Density Polyethylene particles by Thermally Induced Phase Separation (열유도 상분리에 의한 선형 저밀도 폴리에틸렌 입자 제조에 관한 연구)

  • Park, Keun-Ho;Jang, Young-Min
    • Journal of the Korean Applied Science and Technology
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    • v.28 no.4
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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.

Performance Verification of Separation Nut Type Non-explosive Separation Device for Cube Satellite Application (큐브위성 적용을 위한 분리너트형 비폭발식 구속분리장치 인증모델의 성능검증)

  • Oh, Hyun-Ung;Lee, Myeong-Jae
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.41 no.10
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    • pp.827-832
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    • 2013
  • Heating wire cutting type separation mechanism has been widely used for cube satellite applications due to its design constraints such as small size of $10cm{\times}10cm{\times}10cm$ and light weight of less than 1kg. In addition, usage of pyro technic device is not allowed for cube satellite application. The conventional methods have some disadvantages of relatively small mechanical constraint force and the system complexity for the multi-deployable systems. In this paper, a separation nut type non-explosive separation mechanism has been proposed and investigated. The effectiveness of the design has been verified through the qualification tests of the mechanism.