• 제목/요약/키워드: Micro chamber

검색결과 242건 처리시간 0.026초

바이오에멀젼 연료의 연소 특성 (Combustion Characteristics of Bio Emulsion Fuel)

  • 김문찬
    • 한국응용과학기술학회지
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    • 제35권4호
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    • pp.1421-1432
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    • 2018
  • 본 연구에서는 바이오매스로서 코코넛 폐기물을 $600^{\circ}C$에서 열분해하여 생성된 수상오일(water soluble oil)을 얻었다. 선박유로 사용되는 MDO(Marine Diesel Oil)와 바이오매스로서 코코넛 폐기물을 열분해하여 생성된 수상오일을 MDO에 15~20% 까지 혼합 후 유화시켜 제조된 바이오에멀젼 연료의 연소 특성에 대하여 연구 하였다. 엔진 배출가스 및 온도, 출력을 측정하기 위하여 엔진 다이나모메터를 사용하였다. 바이오에멀젼 연료는 수분이 함유되어 있어서 연소실내의 기화잠열을 빼앗아가 배출가스의 온도를 낮춰주는 것으로 나타났다. 바이오에멀젼 연료에 함유된 수분이 연소실내에서 미세폭발을 일으켜 연료를 잘게 쪼개어 주어 매연을 감소시키는 것으로 나타났다. 바이오에멀젼 연료의 사용으로 연소실내의 온도 감소는 질소산화물 배출을 저감하는 것으로 나타났다. 바이오오일 함유량이 증가 하면 수분함량도 증가하여 전체 발열량이 줄어들게 된다. 따라서 출력이 바이오에멀젼 연료 사용량에 비례하여 감소하는 특성을 나타내었다. 선박용 연료로 사용되는 중질유는 매연과 질소산화물을 많이 배출한다. 선박용 연료로 바이오에멀젼 연료를 사용하면 매연과 질소산화물 배출을 줄여줄 수 있을 것으로 기대된다.

비드를 이용한 면역분석용 마이크로필터 칩의 제작 (Microfilter Chip Fabrication for Bead-Based Immunoassay)

  • 이승우;안유민;채영규
    • 대한기계학회논문집A
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    • 제28권9호
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    • pp.1429-1434
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    • 2004
  • Immunoassay is one of the important analytical methods for clinical diagnoses and biochemical studies, but needs a long time, troublesome procedures and expensive reagents. In this study, therefore, we propose the micro filter chip with microbeads for immunoassay, which has pillar structures. The advantage of the proposed micro filter chip is to use simple fabrication process and cheap materials. The mold was made by the photolithography technique with Si wafer and negative photoresist SU-8. The replica was made of PDMS, bonded on the pyrex glass. The micro filter chip consists of inlet channel, filter chamber and outlet channel. HBV (Hepatitius B virus) monoclonal antibody (Ag1) labeled with biotin were immobilized onto streptavidin coated beads of 30∼50 $\mu$m size. Fluorescein isothiocyanate (FITC)-labeled HBV monoclonal antibody (Ag8) was used to detect HBsAg (Hebatitis B virus surface Antigen), and fluorescence intensity was monitored by epi-fluorescence microscope. In this study, the immune response of less than 30 min was obtained with with the use of 100 $m\ell$ of sample.

ADHESION PHENOMENON AND ITS APPLICATION TO MANIPULATION FOR MICRO-ASSEBMLY

  • Takahashi, Kunio;Himeno, Hideo;Saito, Shigeki;Onzawa, Tadao
    • 대한용접접합학회:학술대회논문집
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    • 대한용접접합학회 2002년도 Proceedings of the International Welding/Joining Conference-Korea
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    • pp.781-784
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    • 2002
  • Adhesion phenomenon is more significant for smaller objects, because adhesional force is proportional to size of the objects while gravitational force is proportional to the third power of it. For the purpose of microassembly, theoretical understanding is required for the Adhesion phenomenon. Authors have developed a force measurement system in an ultra-high vacuum chamber of Auger electron spectroscopy. The force between arbitrary combination of materials can be measured at a pressure less than 100 nPa after and before Ar ion sputtering and chemical analysis for several atomic layers of the surface. The results are successfully interpreted with a theory of contact mechanics. Since surface energy is quite important in the interpretation, electronic theory is used to evaluate the surface energy. In the manipulation of small objects, the adhesional force is always attractive. Repulsive force is essential for the manipulation. It can be generated by Coulomb interaction. The voltage required for detachment is theoretically analyzed and the effect of boundary conditions on the detachment is obtained. The possibility and limitations of micro-manipulation using both the adhesion phenomenon and Coulomb interaction are theoretically clarified. Its applicability to nano-technology is found to be expected.

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마이크로 터빈 연소기 주연소영역의 저 NOx 생성 특성 (The Low NOx Characteristics of the Primary Zone in Micro Turbine Combustor)

  • 손민규;안국영;이헌석;윤정중
    • 대한기계학회:학술대회논문집
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    • 대한기계학회 2001년도 추계학술대회논문집B
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    • pp.155-160
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    • 2001
  • The low NOx characteristics have been investigated to develop the combustor for micro turbine. The lean premixed combustion technology was applied to reduce the NOx emission. The test was conducted at the condition of high temperature and ambient pressure. The combustion air which has the temperature of $450\sim650K$ were supplied to the combustor through the air preheater. The temperature and emissions of NOx and CO were measured at the exit of combustor, The exit temperature and NOx were increased and CO was decreased with increasing inlet air temperature. The premixing chamber can be operated very lean condition of equivalence ratio around 0.35. The NOx was decreased with decreasing the equivalence ratio. The CO was decreased with decreasing the equivalence ratio, but the CO was increased with decreasing the equivalence ratio below 0.4. But, at the very lean condition of equivalence ratio below 0.35 both NOx and CO were increased because of the flame unstability. The NOx was decreased and CO was increased with increasing inlet air flowrate. This results can be used to determine the size of combustor. Consequently the performance of combustor shows the possibility of the application to the gas turbine system.

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초소형 고체 추진제 추력기의 내탄도 성능연구 (Internal Ballistic Analysis of Solid Propellant Micro-Thruster)

  • 양준서;이종광;권세진
    • 한국추진공학회:학술대회논문집
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    • 한국추진공학회 2007년도 제29회 추계학술대회논문집
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    • pp.215-218
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    • 2007
  • 고체추진제를 사용한 초소형 추력기의 내탄도 모델링과 성능예측에 관하여 기술하였으며, 특히 초소형화 되면서 고려해야하는 연소실 내의 열손실을 고려하였다. 추진제는 일반 HTPB-AP계열을 선택하였으며, 계산 모델은 간단한 1차원 축대칭 end-burner 모델로 정하였다. 연소실내의 화염에 노출되는 표면과 체적에 대한 비율을 변화시키면서 연소실 가스 온도, 압력, 추력을 계산하여 본 논문의 경우 열손실효과로 약 3%의 총역적 감소가 있음을 확인하였다.

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Flow Visualization of Flowfield Structures around an Aerospike Nozzle using LIF and PSP

  • NIIMI Tomohide;MORI Hideo;TANIGUCHI Mashio
    • 한국가시화정보학회:학술대회논문집
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    • 한국가시화정보학회 2004년도 Proceedings of 2004 Korea-Japan Joint Seminar on Particle Image Velocimetry
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    • pp.75-80
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    • 2004
  • Aerospike nozzles have been expected to be used for an engine of a reusable space shuttle to respond to growing demand for rocket-launching and its cost reduction. In this study, the flow field structures in any cross sections around clustered linear aerospike nozzles are visualized and analyzed, using laser induced fluorescence (LIF) of nitrogen monoxide seeded in the carrier gas of nitrogen. Since flow field structures are affected mainly by pressure ratio, the clustered linear aerospike nozzle is set inside a vacuum chamber to carry out the experiments in the wide range of pressure ratios from 75 to 200. Flow fields are visualized in several cross-sections, demonstrating the complicated three-dimensional flow field structures. Pressure sensitive paint (PSP) of PtTFPP bound by poly- IBM -co-TFEM is also applied to measurement of the complicated pressure distribution on the spike surface, and to verification of contribution of a truncation plane to the thrust. Finally, to examine the effect of the sidewalls attached to the aerospike nozzle, the flow fields around the nozzle with the sidewalls are compared with those without sidewalls.

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미세 연소기 개발 (II) - 미세동력 장치용 미세 전극의 제작과 성능평가 - (Design and Development of Micro Combustor (II) - Design and Test of Micro Electric Spark discharge Device for Power MEMS -)

  • 권세진;이대훈;박대은;윤준보;한철희
    • 대한기계학회논문집B
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    • 제26권4호
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    • pp.524-530
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    • 2002
  • Micro electric spark discharge device was fabricated on a FOTURAN glass wafer using MEMS processing technique and its performance of electron discharge and subsequent formation of ignition kernel were tested. Micro electric spark device is an essential subsystem of a power MEMS that has been under development in this laboratories. In a combustion chamber of sub millimeter scale depth, spark electrodes are formed by electroplating Ni on a base plate of FOTURAN glass wafer. Optimization of spark voltage and spark gap is crucial for stable ignition and endurance of the electrodes. Namely, wider spark gaps insures stable ignition but requires higher ignition voltage to overcome the spark barrier. Also, electron discharge across larger voltage tends to erode the electrodes limiting the endurance of the overall system. In the present study, the discharge characteristics of the proptotype ignition device was measured in terms of electric quantities such as voltage and currant with spark gap and end shape as parameters. Discharge voltage shows a little decrease in width of less than 50㎛ and increases with electrode gap size. Reliability test shows no severe damage over 10$\^$6/ times of discharge test resulting in satisfactory performance for application to proposed power MEMS devices.

랩온어칩 내부 미세유동제어를 위한 새로운 유동제어기법 (A New Flow Control Technique for Handling Infinitesimal Flows Inside a Lab-On-a-Chip)

  • 한수동;김국배;이상준
    • 대한기계학회논문집B
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    • 제30권2호
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    • pp.110-116
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    • 2006
  • A syringe pump or a device using high electric voltage has been used for controlling flows inside a LOC (lab-on-a-chip). Compared to LOC, however, these microfluidic devices are large and heavy that they are burdensome for a portable ${\mu}-TAS$ (micro total analysis system). In this study, a new flow control technique employing pressure regulators and pressure chambers was developed. This technique utilizes compressed air to control the micro-scale flow inside a LOC, instead of a mechanical actuator or an electric power supply. The pressure regulator controls the output air pressure by adjusting the variable resistor attached. We checked the feasibility of this system by measuring the flow rate inside a capillary tube of $100{\mu}m$ diameter in the Re numbers ranged from 0.5 to 50. In addition, the performance of this flow control system was compared with that of a conventional syringe pump. The developed flow control system was found to show superior performance, compared with the syringe pump. It maintains automatically the: air pressure inside a pressure chamber whether the flow inside the capillary tube is on or off. Since the flow rate is nearly proportional to the resistance, we can control flow in multiple microchannels precisely. However, the syringe pump shows large variation of flow rate when the fluid flow is blocked in the microchannel.

다공배플 두께가 마이크로 연소기의 유동 및 혼합특성에 미치는 영향 (Effects of Multi-hole Baffle Thickness on Flow and Mixing Characteristics of Micro Combustor)

  • 김원현;박태선
    • 대한기계학회논문집B
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    • 제41권9호
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    • pp.623-629
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    • 2017
  • 다공배플을 가진 마이크로연소기에 레이놀즈응력 난류모형을 이용하여 난류유동 및 혼합특성에 대한 수치해석 연구를 수행하였다. 다공배플은 연소실 내부에 다수의 3차원 와유동을 발생시키는 기하학적 특징을 가지고 있다. 그러한 형상특징 중에서 배플두께를 변화시킬 경우 와유동구조의 다양한 변화가 얻어졌다. 여러 와유동중에서 연료유동으로부터 생성된 와유동은 혼합도 증가에 결정적 역할을 하였다. 연소실 내부의 3차원 와유동구조는 배플두께 변화에 따른 유동의 발달상태에 의존하였다. 특히, 배플두께가 연료유입구 직경보다 작을수록 배플구멍 제트유동의 속도분포는 포물선형태에서 안장모양의 형태로 변하였다. 연소실내부의 재순환영역크기 및 혼합도는 이러한 제트유동구조에 밀접한 상관관계를 가졌다.

고선량률 근접조사치료용 이리듐-192 방사성동위원소의 교정방법 비교연구 (Comparison of Calibration Methods of $^{192}\textrm{Ir}$ Sources for High Dose Rate Brachytherapy)

  • 허현도;박성용;이레나;신동오;권수일;노준규;최진호
    • 한국의학물리학회지:의학물리
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    • 제15권4호
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    • pp.192-196
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    • 2004
  • 본 연구는 국내에서 이용되고 있는 고선량률 근접치료기에 사용되는 Ir-192 선원에 대하여 Farmer type전리함과 우물형 전리함을 이용하여 선원의 세기를 측정하여 제조사에서 제공된 값과의 오차를 확인하고 두 증기간의 오차를 비교하였다. 동일한 Ir-192가 장착되어 가동 중인 6개의 병원의 고선량률 근접치료기(microSelctron, Nucletron, Netherlands)를 대상으로 선원의 모델별로 구분하여 상품화된 교정 Jig와 우물형 전리함 시스템을 이용, 선원의 세기를 측정하고 제조사에서 제공된 값과 비교하여 오차를 구하였다. 교정용 Jig를 이용한 선원 세기의 오차범위는 -2.40~+3.12%이고 우물형 전리함의 경우 오차범위는 -3.31~0.00%를 나타내었다. 측정 결과 두 장비 모두 제조사에서 제공된 값과 비교하였을 때 ${\pm}5%$의 오차를 넘지 않았으므로 임상 적용에는 문제가 없다. 외국의 사고 사례 보고에 따르면 계산 값에 의존하지 말고 새로운 선원이 교체될때 반드시 치료에 사용되기 전에 측정 도구를 이용하여 방사능의 세기를 측정하고 계산된 값과 비교하여 오차범위 내에서 일치하는지에 대한 확인 절차과정을 거치는 것이 필요하다.

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