• Title/Summary/Keyword: 마이크로 노즐

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Electrohydrodynamic Process Supplemented by Multiple-Nozzle and Auxiliary Electrodes for Fabricating PCL Nanofibers (멀티노즐/보조전극-Electrohydrodynamic 공정을 통한 PCL 나노파이버 제작)

  • Yoon, Hyeon;Kim, Geun-Hyung;Kim, Wan-Doo
    • Polymer(Korea)
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    • v.32 no.4
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    • pp.334-339
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    • 2008
  • Recently electro spinning is a widely used simple technique to prepared micro- to nanometer-sized fiber of various polymers. In general, a normal multiple-nozzle electro spinning system has been difficult to achieve high production-rate fabricating micro/nanofibers due to the interference of electric field between individual nozzles in the process. To reduce the interference effect of electric field between nozzles, we developed a multi-nozzle electrospinning system supplemented with auxiliary electrodes. Poly($\varepsilon$-carprolactone)(PCL), which has good mechanical property and biocompatibility, was electrospun by the multi-nozzle electro spinning system. Electrospinnability, product rate, and size uniformity of spun fibers for the system with and without auxiliary electrodes were characterized. As a result, the multi-nozzle electrospinning system supplemented with auxiliary electrodes provides excellently stable processability and showed high mass productivity of PCL-nanofibers relative to a normal multi-nozzle electro spinning system.

Computational and Experimental Investigation of Thermal Flow Field of Micro Turbojet Engine with Various Nozzle Configurations (노즐 형상 변경에 따른 마이크로 터보제트 엔진의 열유동장에 관한 전산해석 및 실험적 연구)

  • Lee, Hyun-Jin;Lee, Ji-Hyun;Myong, Rho-Shin;Kim, Sun-Mi;Choi, Sung-Man;Kim, Won-Cheol
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.46 no.2
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    • pp.150-158
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    • 2018
  • Numerical simulation and experimental study on the thermal flow field of the micro turbojet engine have been carried out for the purpose of developing infrared reduction technology for aircraft. A circular basic nozzle and five rectangular nozzles with different aspect ratio were considered. The conditions for CFD analysis were derived from the analysis of the engine performance. The temperature distribution of the nozzle plume was measured using a temperature sensing system. The thrust of the rectangular nozzle with the aspect ratio 5 was reduced about 1.8% compared to the circular nozzle, and the thrust decreased with increasing the aspect ratio of the nozzle. In the case of thermal flow field, it was observed that, as the aspect ratio increases, the exhaust plume in the experiment was formed wider than in the CFD analysis.

Painless Microjet Injector Using Laser Pulse Energy (레이저 펄스 에너지를 이용한 무통증 마이크로젯 약물전달시스템)

  • Yoh, Jai-Ick;Han, Tae-Hee;Hah, Jung-Moo
    • Transactions of the Korean Society of Mechanical Engineers B
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    • v.35 no.5
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    • pp.547-550
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    • 2011
  • We have developed a laser-based needle-free liquid drug-injection device. A laser beam is focused inside the liquid contained in the rubber chamber of a micro-scale. The focused laser beam causes explosive bubble growth, and the sudden volume increase in a sealed chamber drives a microjet of liquid drug through the micronozzle. The exit diameter of a nozzle is less than 100 ${\mu}m$, and we verify that the injected microjet is fast enough to penetrate soft human tissue. In the experiment, the microjet penetrated a 5% gelatin-water solution that replicates the human thrombus and pork-fat tissue.

Study on the Characteristics of Long Wave Infrared Signal by Water Injection around the Exhaust Plume of the Micro-jet Engine (마이크로 제트엔진 배기플룸 주위 물 분사에 따른 장파장 적외선 신호특성 연구)

  • Yu, Gunwon;Choi, Seongman
    • Journal of the Korean Society of Propulsion Engineers
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    • v.26 no.2
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    • pp.28-39
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    • 2022
  • An experimental study was carried out to understand the characteristics of the long wave infrared signal emitted from the exhaust plume when water is sprayed around it. The micro-jet engine was used to generate the exhaust plume, and eight water spray nozzles were installed around the exhaust nozzle. Two water injection angles were applied, one is sparying parallel to the exhaust plume, and the other is spraying water into the exhaust plume. The measurement results are as follows. When spraying water parallel to the exhaust plume, the long wave infrared signal is decreased with water spray flow rate. When spraying water the exhaust plume, the long wave infrared signal shows a larger value than plume only.

DI water Nozzle Design for Effective Removal of the Particles Generated during Wafer-sawing (Wafer-Sawing시 발생하는 particle을 효과적으로 제거하기 위한 DI water 노즐의 최적 설계)

  • 김병수;이기준;이성재
    • Journal of the Microelectronics and Packaging Society
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    • v.10 no.4
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    • pp.53-60
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    • 2003
  • CCD(Charge-Coupled Device) wafers, with a layer of micro lenses on top, usually are not passivated with dielectric films. Micro lenses, in general, are made of polymer material, which usually has a large affinity for particles generated in the various chip fabrication processes, most notably the wafer sawing for chip-dicing. The particles deposited on the micro lens layer either seriously attenuate or deflect the incoming light and often lead to CCD failure. In this study we introduce new type of saws which would significantly reduce the particle-related problems found in conventional type of saws. In the new saws, the positions and diverging angles of side and center nozzles have been optimized so as to flush the particles effectively. In addition, an independent nozzle is added for the sole purpose of flushing the generated particles. The test results show that, with the new saws. the ratio of the particle-related CCD chip failures has been dropped drastically from 9.1% to 0.63%.

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Design and Fabrication method of combustor for micro solid propellant thruster (MEMS 고체 추진제 추력기의 추진제실 설계와 구조체 가공 방법)

  • Lee, Jong-Kwang;Kwon, Se-Jin
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2006.11a
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    • pp.251-254
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    • 2006
  • Micro thruster is a key technology in the micro/nano satellite. MSPT has been attracted attention as a one of possible solution for micro thruster MSPT as a systems four components. It is composed of nozzle, igniter, combustion chamber and propellant. This paper surveys varioud MSPTs which have been reported. The model of MSPT arrays for total impulse of 1 mNs is proposed. Combustion chamber is designed and fabricated.

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Micropattern Arrays of Polymers/Quantum Dots Formed by Electrohydrodynamic Jet (e-jet) Printing (이젯 프린터를 사용한 고분자/퀀텀닷 마이크로 패터닝 공정)

  • Kim, Simon;Lee, Su Eon;Kim, Bong Hoon
    • Journal of the Korean Institute of Electrical and Electronic Material Engineers
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    • v.35 no.1
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    • pp.18-23
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    • 2022
  • Electrohydrodynamic jet (e-jet) printing, a type of direct contactless microfabrication technology, is a versatile fabrication process that enables a wide range of micro/nanopattern arrays by applying a strong electric field between the nozzle and the substrate. In general, the morphology and the thickness of polymers/quantum dot micropatterns show a systematic dependence on the diameter of the nozzle and the ink composition with a fully automated printing machine. The purpose of this report is to provide typical examples of e-jet printed micropatterns of polymers/quantum dots to explain the effect of each process variable on the result of experiments. Here, we demonstrate several operating conditions that allow high-resolution printing of layers of polymers/quantum dots with a precise control over thickness and submicron lateral resolution.