• 제목/요약/키워드: microchannel reactor

검색결과 13건 처리시간 0.016초

DNA의 제한효소 반응 및 전기영동 검출용 PDMS/유리 마이크로바이오칩 (PDMS/Glass Based DNA Microbiochip for Restriction Enzyme Reaction and Electrophoresis Detection)

  • 최준영;안유민;황승용
    • 대한기계학회논문집A
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    • 제30권1호
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    • pp.26-31
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    • 2006
  • This paper reports low-cost PDMS/glass based DNA microbiochip for the restriction enzyme reaction and its products detection using the capillary electrophoresis. The microbiochip ($25mm{\times}75mm$) has the heater integrated reactor ($5{\mu}{\ell}$) for DNA restriction enzyme reaction at $37^{\circ}C$ and the microchannel ($80\;{\mu}m{\times}100\;{\mu}m{\times}58mm$) for the capillary electrophoresis detection. It is experimentally confirmed that the digestion of the plasmid ($pGEM^{(R)}-4Z$) by the enzyme (Hind III and Sca I) is performed for less than 10 min and its electrophoresis detection is able to sequentially on the fabricated microbiochip.

Fabrication, Estimation and Trypsin Digestion Experiment of the Thermally Isolated Micro Teactor for Bio-chemical Reaction

  • Sim, Tae-Seok;Kim, Dae-Weon;Kim, Eun-Mi;Joo, Hwang-Soo;Lee, Kook-Nyung;Kim, Byung-Gee;Kim, Yong-Hyup;Kim, Yong-Kweon
    • JSTS:Journal of Semiconductor Technology and Science
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    • 제5권3호
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    • pp.149-158
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    • 2005
  • This paper describes design, fabrication, and application of the silicon based temperature controllable micro reactor. In order to achieve fast temperature variation and low energy consumption, reaction chamber of the micro reactor was thermally isolated by etching the highly conductive silicon around the reaction chamber. Compared with the model not having thermally isolated structure, the thermally isolated micro reactor showed enhanced thermal performances such as fast temperature variation and low energy consumption. The performance enhancements of the micro reactor due to etched holes were verified by thermal experiment and numerical analysis. Regarding to 42 percents reduction of the thermal mass achieved by the etched holes, approximately 4 times faster thermal variation and 5 times smaller energy consumption were acquired. The total size of the fabricated micro reactor was $37{\times}30{\times}1mm^{3}$. Microchannel and reaction chamber were formed on the silicon substrate. The openings of channel and chamber were covered by the glass substrate. The Pt electrodes for heater and sensor are fabricated on the backside of silicon substrate below the reaction chamber. The dimension of channel cross section was $200{\times}100{\mu}m^{2}$. The volume of reaction chamber was $4{\mu}l$. The temperature of the micro reactor was controlled and measured simultaneously with NI DAQ PCI-MIO-16E-l board and LabVIEW program. Finally, the fabricated micro reactor and the temperature control system were applied to the thermal denaturation and the trypsin digestion of protein. BSA(bovine serum albumin) was chosen for the test sample. It was successfully shown that BSA was successfully denatured at $75^{\circ}C$ for 1 min and digested by trypsin at $37^{\circ}C$ for 10 min.

Liquid phase hydrogen peroxide decomposition for micro-propulsion applications

  • McDevitt, M. Ryan;Hitt, Darren L.
    • Advances in aircraft and spacecraft science
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    • 제4권1호
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    • pp.21-35
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    • 2017
  • Hydrogen peroxide is being considered as a monopropellant in micropropulsion systems for the next generation of miniaturized satellites ('nanosats') due to its high energy density, modest specific impulse and green characteristics. Efforts at the University of Vermont have focused on the development of a MEMS-based microthruster that uses a novel slug flow monopropellant injection scheme to generate thrust and impulse-bits commensurate with the intended micropropulsion application. The present study is a computational effort to investigate the initial decomposition of the monopropellant as it enters the catalytic chamber, and to compare the impact of the monopropellant injection scheme on decomposition performance. Two-dimensional numerical studies of the monopropellant in microchannel geometries have been developed and used to characterize the performance of the monopropellant before vaporization occurs. The results of these studies show that monopropellant in the lamellar flow regime, which lacks a non-diffusive mixing mechanism, does not decompose at a rate that is suitable for the microthruster dimensions. In contrast, monopropellant in the slug flow regime decomposes 57% faster than lamellar flow for a given length, indicating that the monopropellant injection scheme has potential benefits for the performance of the microthruster.