• Proceedings of the Korean Vacuum Society Conference
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• 2013.08a
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• pp.120.1-120.1
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• 2013

우주 궤도환경은 $10^{-5}$ torr 이하의 고진공 및 $100^{\circ}C$의 고온과 $150^{\circ}C$이하의 극저온 환경으로 특징지어지며, 위성체 및 위성체 부품은 이와 같은 우주 궤도환경에서의 성능검증이 필수적이다. 지상에서 이와 같은 환경을 모사하기 위해서는 열진공챔버가 사용되며, 열진공 챔버는 진공배기계와 열제어 시스템으로 구성된다. 특히 위성체 또는 위성부품의 열환경을 모사하기 위해 기체 질소를 이용한 폐회로 열제어 시스템이 사용된다. 폐회로 열제어 시스템은 슈라우드, 극저온 블로워, 히터 등으로 구성이 된다. 열제어 시스템의 신뢰성을 높이기 위해서는 핵심 부품인 극저온 블로워의 이중화가 필요하다. 본 논문에서는 위성체 및 위성체 부품의 열진공 시험에 사용되는 열진공 챔버 열제어 시스템의 핵심인 극저온 블로워의 이중화를 위한 기구 설계 및 제어로직 설계 등이 포함되어 있다.

• Journal of the Korean Society of Propulsion Engineers
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• v.18 no.1
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• pp.58-64
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• 2014

Hydraulic dual chamber, as the simulator for a dual pulse rocket motor, was tested by a high pressure device with various orifice-hole size being applied. Pressure difference occurs between 1st chamber and 2nd chamber depending on area ratio of the orifice to nozzle throat. Studying a design configuration of the orifice is essential to the motor development because pressure difference severely affects the rocket motor performance. It is noticed in this study that energy dissipation is caused by the vortex flow originating from the orifice as the 2nd chamber is operated. The flow field is simulated by a commercial computational fluid dynamics program, ANSYS FLUENT V14.5.

• Proceedings of the Korean Society for Noise and Vibration Engineering Conference
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• 2013.10a
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• pp.815-824
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• 2013

Pneumatic exciters can be good replacements of electrodynamic, piezoelectric and hydraulic exciters owing to simple structure and large exciting force. One problem to be solved is a slow response caused by compressibility of air. Desirable frequency response characteristics of exciter are constant magnitude and zero degree phase, because users want no time delay between input signal and output force. For this reason, frequency range of pneumatic exciters is limited about 0~1 Hz. Therefore, expansion of frequency range is an important issue when designing the pneumatic exciter. In this paper, the pneumatic exciter which has same structure with active pneumatic isolator is dealt with. The dynamic characteristics are presented, and its limitation of expanding frequency range is shown based on analytical studies. Then the pneumatic exciter with dual-chamber is suggested to overcome this problem. Based on simulation study, a design method is presented.

• Proceedings of the Korean Vacuum Society Conference
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• 2010.02a
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• pp.469-469
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• 2010

공정 플라즈마에서 가장 중요한 요소 중 하나는 챔버 내 균일도 제어이다. 챔버 내 플라즈마 상태가 공간적으로 불균일한 경우 과에칭, 미증착 등의 문제가 웨이퍼의 특정 영역에 나타나게 되어 공정 수율이 감소된다. 이 연구에서는 2차원 평면 탐침을 챔버 내에 삽입하여 플라즈마 전자온도, 밀도, 이온 전류량 등의 상태변수를 측정 가능한 방법을 연구하였다. 기존의 2차원 평면 탐침과 달리, 측정 회로와 계산 모듈을 모두 삽입하여 외부의 컨트롤러가 필요 없어 반도체나 디스플레이의 플라즈마 공정의 사이사이에 삽입되어서 플라즈마 상태변수를 측정할 수 있는 장점을 가지고 있다. 본 임베디드 2차원 평면 탐침은 측정회로가 외부와 단절되어 전기적으로 절연되어 있어, 측정 방법으로 이중 탐침법을 응용하였다. 이중탐침에 정현파 전압을 인가하고 이 경우 들어오는 전류의 제 1 고조파와 제 3 고조파를 크기를 측정하는 방법으로 플라즈마 변수 계산이 가능하다. 이 측정 방법은 플라즈마 공정에서 쉽게 관찰할 수 없었던 공간적인 상태변수의 분포를 알 수 있고 플라즈마 균일도 제어에 기여할 수 있을 것이다.

• Transactions of the Korean Society for Noise and Vibration Engineering
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• v.23 no.10
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• pp.909-919
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• 2013

Pneumatic exciters can be good replacements of electrodynamic, piezoelectric and hydraulic exciters owing to simple structure and large exciting force. One problem to be solved is a slow response caused by compressibility of air. Desirable frequency response characteristics of exciter are constant magnitude and zero degree phase, because users want no time delay between input signal and output force. For this reason, frequency range of pneumatic exciters is limited about 0~1 Hz. Therefore, expansion of frequency range is an important issue when designing the pneumatic exciter. In this paper, the pneumatic exciter which has same structure with active pneumatic isolator is dealt with. The dynamic characteristics are presented, and its limitation of expanding frequency range is shown based on analytical studies. Then the pneumatic exciter with dual-chamber is suggested to overcome this problem. Based on simulation study, a design method is presented.

• Journal of the Korean Society of Propulsion Engineers
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• v.25 no.4
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• pp.53-58
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• 2021

Based on surrogate model, a hydrocarbon mixture was analyzed by visualizing the impinging break up mechanism in subcritical and supercritical conditions. Decane and methylcyclohexane with different critical pressures and temperatures were selected as experimental fluids. The impinging injector was installed inside the chamber, and the spray was visualized through a speed camera in subcritical and supercritical conditions. The injection condition of the mixture and chamber was kept constant at Pr(P/P_c) = 1, and Tr(T/T_c) was increased from 0.48 to 1.02. As Tr increased, the spray angle increased, and the sheet length decreased as the properties of the mixture reached each critical point. In addition, when the mixture approached the near critical point, it was shown that the change in density gradient was largely observed out of the impinging break up mechanism.

• Transactions of the Korean Society for Noise and Vibration Engineering
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• v.18 no.1
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• pp.110-122
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• 2008

Pneumatic vibration isolator typically consisting of dual-chamber pneumatic springs and a rigid table are widely employed for proper operation of precision instruments such as optical devices or nano-scale equipments owing to their low stiffness- and high damping-characteristics. As environmental vibration regulations for precision instruments become more stringent, it is required to improve further the isolation performance. In order to facilitate their design optimization or active control, a more accurate mathematical model or complex stiffness is needed. Experimental results we obtained rigorously for a dual-chamber pneumatic spring exhibit significantly amplitude dependent behavior, which cannot be described by linear models in earlier researches. In this paper, an improvement for the complex stiffness model is presented by taking two major considerations. One is to consider the amplitude dependent complex stiffness of diaphragm necessarily employed for prevention of air leakage. The other is to employ a nonlinear model for the air flow in capillary tube connecting the two pneumatic chambers. The proposed amplitude-dependent complex stiffness model which reflects dependency on both frequency and excitation amplitude is shown to be very valid by comparison with the experimental measurements. Such an accurate nonlinear model for the dual-chamber pneumatic springs would contribute to more effective design or control of vibration isolation systems.

• Proceedings of the Korean Society for Bio-Environment Control Conference
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• 1999.11a
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• pp.225-228
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• 1999

기내 조직배양묘의 생육에 가장 큰 영향을 미치는 주요 환경 요인으로 광, 온도, $CO_2$, 배지 등이 있다. 이중 광, 온도 및 $CO_2$ 가스는 기외로 부터 공급을 받거나 제어 할 수 있는 요인으로써 배양체의 생육에 있어 매우 중요하다. 배양 챔버내의 환경 제어는 용이하지만, 배양체에 직접적인 영향을 주는 용기내의 환경 계측은 용이하지 않다. 실제 배양체의 생육에 가장 큰 영향을 미치는 용기 내 환경과 배양 챔버의 환경은 큰 차이를 나타내기 때문에 조직배양용기내의 미기상 환경에 대한 분석은 필요하다. (중략)

• Journal of the Korean Society of Propulsion Engineers
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• v.15 no.3
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• pp.22-30
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• 2011

There is a many way of LPRE throttling methods, high-pressure-drop systems, dual-manifold injector, gas injection, multiple chambers, pulse modulation and movable injector components. Especially dual-manifold injector is essentially combines two fixed-area injectors into a common structure, with independent feed systems controlling flow to each injector manifold. In this paper, using indirect photography and liquid film thickness measurement with various injection pressure and tangential entry diameter to decide stability of spray over a wide thrust range in dual manifold injector.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.39 no.9
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• pp.877-882
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• 2011

In this paper, thermal deformation of a double ring structure using digital image correlation technique (DIC) was measured. The double ring structure consisted of two parts; the inner ring was aluminium which had a large thermal expansion coefficient and the outer ring was titanium which had a small thermal expansion coefficient. We heated the double ring structure from $50^{\circ}C$ to $200^{\circ}C$ in a chamber and at the same time, two cameras captured surface images of the double ring structure. Initially, there was a 21 ${\mu}m$ gap between the inner ring and outer ring. The gap was closed at around $80^{\circ}C$ and after that, two rings expanded together. In order to compare the experimental results with analysis results, a finite element analysis was performed using ANSYS. The results of DIC measurement and ANSYS analysis were compared and agreed well.