• Journal of Radiation Protection and Research
• /
• 제9권1호
• /
• pp.11-18
• /
• 1984

Well type 전리함과 미세전류 측정희로를 사용하여 표준 감마선 전리함 장치를 개발하였다. 미세전류는 automatic Townsend balance with stepwise compensation방법을 사용하여 측정하였다. $^{226}Ra$을 기준 선원으로 택하여 감마 방출핵종인 $^{241}Am,\;^{133}Ba,\;^{60}Co,\;^{134}Cs,\;^{137}Cs^{22}Na$에 대한 비교 교정인자를 산출하였으며, 감마에너지의 함수로서 검출 효율 곡선을 구하였다.

• 한국자동차공학회논문집
• /
• 제10권6호
• /
• pp.90-99
• /
• 2002

The main purpose of this study lies on the development of micro dilution tunnel based on the Sierra Dilution chamber model. As a primary examination, characteristics of flow and temperature distributions during the steady dilution process in dilution chamber are observed with numerical analysis. The penetration of dilution air through porous tube as well as wall temperature and temperature gradient inside porous tube are examined. The thermophoretic velocity in terms of temperature behavior inside porous tube are defined and examined. Based on the ratio of penetration and thermophoretic velocities, all part of porous tube are shown to be safe from the particulate depositions. However, The inlet portion of porous tube in addition to the portion of impinging of dilution air are marginally safe from the particulate depositions. Generally the safer design against particulate deposition is required in provision f3r steady dilution process and for transient process as well.

• 한국추진공학회:학술대회논문집
• /
• 한국추진공학회 2003년도 제20회 춘계학술대회 논문집
• /
• pp.270-273
• /
• 2003

The characteristic of constant volume micro combustor was investigated experimentally. The shape of micro combustor was cylindrical and has row aspect ratio or has relatively large diameter compared with chamber height. Diameter and chamber height was varied to investigate the geometric effect of combustor on the flame propagation. Diameter of 15 mm and 7.5 mm was designed while chamber height was designed to be 1mm, 2mm, and 3mm. The effect of initial pressure was also investigated parametrically from 1bar to 3bar. The gas used in this study was stoichiometric mixture of methane and air. The maximum pressure achieved in down scaled combustors was lower than that of conventional combustor because heat loss to wall was dominant as expected. The maximum pressure responded favorably with the change of height of combustor and the initial pressure, the maximum pressure was also increased. The flame propagation was possible when the specific condition was satisfied. Although the quenching distance of stoichiometric mixture of CH4 and Air is 2.5 mm, the flame could propagate even under quenching distance as the initial pressure increased.

• Journal of Advanced Marine Engineering and Technology
• /
• 제33권5호
• /
• pp.637-645
• /
• 2009

The main purpose of this study lies on the improvement of micro dilution tunnel based on the typical porous tube type chamber. The characteristics of flow and temperature fields for steady state has been obtained by numerical analysis using FLUENT. Three different geometrical variations of the porous tube; a) increase of thickness at center, b) step increase of thickness at center and downstream, c) tapered increase of thickness, have been proposed. Accordingly results are obtained and compared in terms of penetration velocity and velocity ratio to therrmophoretic velocity for improvement against particulate deposition inside the tube. The penetration velocity and velocity ratio distributions in the upstream portion and portion of impinging of dilution air are apparently shown to be improved for the case of the step and tapered change of porous tube. The tapered change of tube thickness addition are shown to be the most effective among three geometrical changes. In addition, the considerable improvement against deposition are shown that its thickness should be at least 2mm.

• 대한기계학회논문집B
• /
• 제26권1호
• /
• pp.74-81
• /
• 2002

Combustion phenomena in a sub-millimeter scale combustor have been investigated. To evaluate scale effect on flame propagation characteristics, a cylindrical combustion chamber with variable depth was built in-house. The combustor was charged with premixed gas of hydrogen and air and ignited electronically. A piezo electric pressure transducer recorded transient pressure after the ignition. Measurements were made at different test conditions specified with chamber depth and initial pressure as parameters. Visual observation was made through a quartz glass window on top side of the combustion chamber using high speed digital video camera. From the pressure data, available work was estimated and compared with energy input required for stable ignition. The preliminary results suggested that the net thermal energy release is sufficient to generate power and enables a combustor of the size in the present study to be used as the energy source of a micro power devices .

• 대한방사선치료학회지
• /
• 제18권1호
• /
• pp.1-5
• /
• 2006

목 적: 세기조절 방사선치료의 환자별 정도관리는 이온전리함을 이용한 일정 지점에서의 절대 선량 측정과 필름을 이용한 상대 선량측정의 두 단계로 구성된다. 이온전리함을 이용한 절대 선량 측정은 동일한 지점에서 치료계획상의 점선량과 실제 측정 점선량 간의 일치도에 대한 정보를 제공한다. 일반적으로 정확한 점선량을 측정하기 위해 volume이 작은 0.015 cc 이온전리함(pin point chamber, PTW, Germany)을 사용하고 있다. 그러나 이 경우 이온전리함의 볼륨이 작아 선량의 오차가 크게 나타나는 경우도 있어, 적합한 볼륨의 이온전리함 사용이 권고되기도 한다. 따라서 볼륨이 다른 세 가지의 이온전리함을 이용하여 점선량을 측정하여 치료계획상의 점 선량과 비교해 보고, 0.015 cc 이온전리함을 이용한 세기조절 방사선치료에서의 절대 점선량 측정의 유효성을 평가해 보고자 한다. 대상 및 방법: 두경부(Head & Neck) 종양의 세기조절 방사선치료가 요구되는 환자 6명을 대상으로 Sliding-window 방법의 IMRT 치료계획을 수립하였으며 치료기는 21EX(Varian, USA) 선형가속기의 6 MV 광자선을 사용하였다. 측정 조건은 120 millenium MLC를 이용하여 Gantry 0도에서 300 MU/min의 선량률로 선원-이온전리함(source-axis-distance)거리를 100 cm, 고체팬텀의 표면으로부터 5 cm 깊이에 이온전리함을 위치시켰다. 치료계획용 컴퓨터(CAD-Plan, USA)에서 결정된 결과를 0.015 cc(pin point, type 31014, PTW, Germany), 0.125 cc(micro type 31002, PTW, Germany ), 0.6 cc(famer type 30002, PTW, Germany) 전리함에 각각 조사하여 측정치를 비교 분석하였다. 측정점은 선량값의 변화가 상대적으로 적은 선량 저변동 영역(Low-gradient area)에 위치시켰다. 결 과: 각각의 이온전리함을 이용하여 측정한 결과 0.015 cc의 경우 평균 ${\pm}0.91%$, 0.125 cc의 경우 ${\pm}0.52%$, 0.6 cc의 경우 ${\pm}0.76%$로 0.125 cc 이온전리함의 경우가 모든 측정조건에서 가장 적은 오차를 보였다. 결 론: 세기조절 방사선치료에 있어서 선량의 평가는 매우 중요하다. 방사선치료가 정밀해지는 만큼 정확한 선량평가가 이루어져야 한다. 점선량을 평가하기 위해 제작된 0.015 cc 이온전리함은 작은 출력신호와 큰 신호 대 잡음비가 절대 선량 측정 시 선량오차를 발생시키는 큰 요인으로 작용할 수 있다. 반면에 이온전리함의 볼륨이 큰 경우 출력신호가 크므로 정확한 선량을 반영할 수 있으나, 작은 측정점에 이온전리함을 정확히 위치시키기 어려워 절대 점선량을 측정하기 어려운 단점이 있다. 따라서 본 연구의 결과에서 본 바와 같이 세기조절 방사선치료의 절대 점선량 측정에는 오차가 상대적으로 적은 0.125 cc 이온전리함의 사용이 고려되어야 한다.

• 한국추진공학회:학술대회논문집
• /
• 한국추진공학회 2007년도 제29회 추계학술대회논문집
• /
• pp.225-228
• /
• 2007

마이크로 고체 추진제 추력기는 현재의 MEMS 기술로 가장 실현 가능성이 높은 마이크로 추력기이다. 마이크로 고체 추진제 추력기의 기본 요소로는 마이크로 노즐, 마이크로 점화기, 연소 챔버 그리고 고체 추진제이다. 마이크로 노즐과 연소 챔버는 감광유리의 이방성 식각을 통해 제작이 되었다. 마이크로 점화기는 마이크로 유리 박막 백금 히터를 사용하였다. 요소들의 제작 공정을 확립 후, 요소들을 통합하여 추력기를 개발하였다. 추력기의 연소 실험을 수행하여 성공적으로 연소가 일어남을 확인하였다.

• 설비공학논문집
• /
• 제17권6호
• /
• pp.544-551
• /
• 2005

The flow characteristics have been numerically investigated for various shapes of the diffuser/nozzles which are used for a valveless micro-pump. The important parameters considered in this study are the throat width ($15\~120\mu$m), the taper angle ($3.15\~25.2^{\circ}$), and the diffuser length ( $600\~4,800\mu$m), and the size of the middle chamber ($1\~16mm^2$). To find the optimal values for these parameters, steady state calculations have been performed assuming the constant pressure difference between the inlet and exit of the flow For the taper angle and the throat width, it is found that there exists an optimum at which the net flow rate is the greatest. The optimal taper angle is in the range of $10\~20^{\circ}$ for all the pressure differences; and the throat width indicates an optimal value near $75\mu$m for the case of 35 kPa pressure difference. The net flow rate is also influenced by the size of the middle chamber. With decreasing chamber size, the net flow rate is reduced because of the interference between two streams flowing into the middle chamber. The unsteady pulsating flow characteristics for a micro-pump with a given diffuser/nozzle shape have been also investigated to show the validity of the steady state parametric study.

• 한국추진공학회:학술대회논문집
• /
• 한국추진공학회 2017년도 제48회 춘계학술대회논문집
• /
• pp.757-763
• /
• 2017

본 연구에서는 50 mN급 마이크로 추력기를 활용하여, ADN 기반 추진제인 LMP-103S의 연소 실험을 수행하였다. 마이크로 추력기는 MEMS 공정 과정을 거쳐 감광유리로 제작하였다. LMP-103S 분해용 촉매로 $Pt/{\gamma}-Al_2O_3$를 사용하였다. 연소 실험 초기에 촉매 예열을 위해 90 wt.% 과산화수소를 주입하였으며, 이후 LMP-103S를 주입하여 연소 실험을 수행하였다. 실험 결과 백금 촉매 환경에서 LMP-103S의 점화가 이루어짐을 확인하였으며, 연소실 온도는 $650^{\circ}C$로 형성되었다.

• 대한기계학회:학술대회논문집
• /
• 대한기계학회 2004년도 추계학술대회
• /
• pp.1196-1200
• /
• 2004

Micropump is very useful component in micro/nano fluidics and bioMEMS applications. In this study, a bubble-powered micropump was fabricated and tested. The micropump consists of two-parallel micro line heaters, a pair of nozzle-diffuser flow controller and a 1 mm in diameter, 400 ${\mu}m$ in depth pumping chamber. The two-parallel micro line heaters with 20 ${\mu}m-width$ and 200 ${\mu}m-length$ were fabricated to be embedded in the silicon dioxide layer of a wafer which serves as a base plate for the micropump. The pumping chamber, the pair of nozzle-diffuser unit and microchannels including the liquid inlet and outlet port were fabricated by etching through another silicon wafer. A glass wafer (thickness of $525{\pm}15$ ${\mu}m$) having two holes of inlet and outlet ports of liquid serve as upper plate of the pump. Finally the silicon wafer of the base plate, the silicon wafer of pumping chamber and the glass wafer were aligned and bonded (Si-Si bonding and anodic bonding). A sequential photograph of bubble nucleation, growth and collapse was visualized by CCD camera. Clearly liquid flow through the nozzle during the period of bubble growth and slight back flow of liquid at the end of collapsing period can be seen. The mass flow rate was found to be dependent on the duty ratio and the operation frequency. As duty ratio increases, flow rate decreases gradually when the duty ratio exceeds 60%. Also as the operation frequency increases, the flow rate of the micropump decreases slightly.