• 제목/요약/키워드: Tip-off

검색결과 141건 처리시간 0.026초

전향 스윕 축류형 팬에서의 팁 누설 유동 구조 (Structure of Tip Leakage Flow in a Forward-Swept Axial-Flow Fan)

  • 이공희;백제현
    • 유체기계공업학회:학술대회논문집
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    • 유체기계공업학회 2002년도 유체기계 연구개발 발표회 논문집
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    • pp.131-136
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    • 2002
  • A computational analysis using Reynolds stress model in FLUENT is conducted to give a clear understanding of the effect of blade loading on the structure of tip leakage flow in a forward-swept axial-flow fan at design condition ($\phi$=0.25) and off-design condition ($\phi$=0.21 and 0.30). The roll-up of tip leakage flow starts near the minimum static wall pressure position, and the tip leakage vortex developes along the centerline of the pressure trough within the blade passages. Near tip region, a reverse flow induced by tip leakage vortex has a blockage effect on the through-flow. As a result, high momentum region is observed below the tip leakage vortex. As the blade loading increases, the reverse flow region is more inclined toward circumferential direction and the onset position of the rolling-up of tip leakage flow moves upstream. Because the casing boundary layer becomes thicker, and the mixing between the through-flow and the leakage jet with the different flow direction is enforced, the streamwise vorticity decays more fast with blade loading increasing. The computational results show that a distinct tip leakage vortex is observed downstream of the blade trailing edge at $\phi$=0.30, but it is not observed at $\phi$=0.21 and 0.25.

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입사각 변화에 따른 터빈 블레이드에서의 열전달 특성 변화 (I) - 블레이드 끝단면 - (Effect of Incidence Angle on Turbine Blade Heat Transfer Characteristics (I) - Blade Tip -)

  • 이동호;조형희
    • 대한기계학회논문집B
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    • 제31권4호
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    • pp.349-356
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    • 2007
  • The present study investigated local heat/mass transfer characteristics on the tip of the rotating turbine blade with various incoming flow incidence angles. The experiments are conducted in a low speed annular cascade with a single stage turbine. The blade has a flat tip with a mean tip clearance of 2.5% of the blade chord. The incoming flow Reynolds number is $1.5{\times}10^5$ at design condition. To examine the effect of off-design condition, the experiments with various incidence angles ranging between $-15^{\circ}$ and $+7{\circ}$ were conducted. A naphthalene sublimation method is used to measure detailed mass transfer coefficient on the blade. The results indicated that the incidence angle strongly affects the behavior of tip leakage flow around the blade tip and consequently plays an important role in determining heat transfer characteristics on the tip. For negative incidence angles, the heat/mass transfer in the upstream region on the tip decreases by up to 20%. On the contrary, for positive incidence angles, much higher heat transfer coefficients are observed even with small increase of incidence angle.

유량에 따른 축류홴의 익단누설와류 특성 (Flow Characteristics of a Tip Leakage Vortex at Different Flow Rates in an Axial Flow Fan)

  • 장춘만;김광용
    • 대한기계학회:학술대회논문집
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    • 대한기계학회 2004년도 추계학술대회
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    • pp.1383-1388
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    • 2004
  • The flow characteristics in the blade passage of a low speed axial flow fan have been investigated by experimental analysis using a rotating hot-wire sensor for design and off-design operating conditions. The results show that the tip leakage vortex is moved upstream when flow rate is decreased, thus disturbing the formation of wake flow near the rotor tip. The tip leakage vortex interfaces with blade pressure surface, and results in high velocity fluctuation near the pressure surface. From the relative velocity distributions near the rotor tip, large axial velocity decay is observed at near stall condition, which results in large blockage compared to that at the design condition. Througout the flow measurements using a quasi-orthogonal measuring points to the tip leakage vortex, it is noted that the radial position of the tip leakage vortex is distributed between 94 and 96 percent span for all flow conditions. High spectrum density due to the large fluctuation of the tip leakage vortex is observed near the blade suction surface below the frequency of 1000 Hz at near stall condition.

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유럽에서 유통되는 일회용침 끝의 미세 형태에 대한 관찰 (Investigation of Micromorphological Characteristics of Acupuncture Needle Tip Sold in Europe)

  • 장인수;이태호;이창현;박종배
    • Korean Journal of Acupuncture
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    • 제21권4호
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    • pp.43-51
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    • 2004
  • Objectives : In order to ensure safe acupuncture treatment, the quality of the needle tip is essential. But, there have not been so many studies about the quality of the acupuncture needle tip. For this reason we have been already reported about the quality of acupuncture needle tip in Korea using scanning electron microscope(SEM) in 2002, 2003. In order to compare than other society, we investigated the current condition of the tips of the acupuncture needles sold in Europe. Methods : We obtained the needles made by 7 companies, which are sold currently in Europe, and selected 50 pieces out of 100 pieces from each company by randomized methods. And then we observed the tip of each needle using a scanning electron microscope at ${\times}800$ magnification. Results and Discussion : We found that needles had several defects such as scratch marks on the surface, metallic scuff, lumps and irregularities of the needle tips, stubbed or malformed tips, tips of point off-center, peeled off coated tips, same as Korean needles. There was much difference on the quality of needles among the manufacturers, and some needles seem to need thorough quality control. Allowing for the high price, the quality of some needle in Europe generally are better than that of Korean needles. But some Korean needles hold a top position than European ones in quality. We want a good industrial standard to be made in acupuncture manufacturing fields in the near future, because the safety is not less valuable than the efficacy in medicine.

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입사각 변화에 따른 터빈 블레이드에서의 열전달 특성 변화 (II) - 블레이드 표면 - (Effect of Incidence Angle on Turbine Blade Heat Transfer Characteristics (II) - Blade Surface -)

  • 이동호;조형희
    • 대한기계학회논문집B
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    • 제31권4호
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    • pp.357-366
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    • 2007
  • The present study investigated local heat/mass transfer characteristics on the surface of the rotating turbine blade with various incidence angles. The experiments are conducted in a low speed annular cascade with a single stage turbine. The blade has a flat tip with the mean tip clearance of 2.5% of the blade chord. A naphthalene sublimation method is used to measure detailed mass transfer coefficient on the blade. At design condition, the inlet Reynolds number is $Re_c=1.5{\times}10^5$ which results in the blade rotation speed of 255.8 rpm. Also, the effect of off-design condition is examined with various incidence angles between $-15^{\circ}$ and $+7{\circ}$. The results indicated that the incidence angle has significant effects on the blade surface heat transfer. In mid-span region, the laminar separation region on the pressure side is reduced and the laminar flow region on the suction side shrinks with increasing incidence angle. Near the tip, the effect of tip leakage flow increases in span wise and axial directions as the incidence angle decreases because the tip leakage flow is formed near the suction side surface. However, the effect of tip leakage flow is reduced with positive incidence angle.

자동 분주기 Fixed Tip의 Carryover 방지를 위한 개선 방안 (The Prevention of Carryover in the Automated System With Fixed Tips)

  • 황보라;어두희;배진수;박종오;김지영;석재동
    • 핵의학기술
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    • 제13권3호
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    • pp.181-184
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    • 2009
  • 목적 : 자동 분주기 (TECAN)의 fixed tip 사용 시 충분한 세척에도 불구하고 고농도 검체 뒤에 연이은 검체가 영향을 받는 carryover 현상이 발생되는 경우가 있다. 이는 검사결과가 위 양성으로 나타날 수 있는 위험성이 있으므로 이상유무 판단을 위해 잦은 재검을 실시해야 하는 번거로움이 있다. 따라서 본 연구는 경제성이 높은 fixed tip을 사용하면서 carryover를 방지할 수 있는 방법을 개선하고자 한다. 실험재료 및 방법 : 자동분주기(Tecan)를 이용하여 HBs Ag, HBs Ab, HBc Ab(IgG) 검사를 대상으로 실행하였으며, fixed tip 방식의 분주시스템으로 일반 환자의 검체 분주 후에 생리식염수를 분주 할 수 있도록 배치하였다. 세척 단계는 0.25mol/L NaOH용액을 이용하였으며, 생리식염수의 검사결과 cpm을 측정하여 carryover의 발생 유무를 확인하였다. 또한 3가지 검사를 0.25 mol/L NaOH 용액이 검사에 미치는 영향을 분석하였다. 결과 : 생리식염수 결과는 100% 음성결과를 보였으며, 0.25 mol/L NaOH를 세척액으로 사용한 fixed tip에서 검체분주 시 환자 혈청은 HBc Ab (IgG)검사에서 cut-off zone (cut-off${\pm}$10%)을 제외한 모든 결과에서 기존 외래보고 결과와 동일한 값을 얻었다. 결론 : 생리식염수 검사결과 100% 음성을 보인 것은 실험에서 사용한 세척액으로 fixed tip을 세척하는 방법이 carryover를 방지할 수 있고, 이로 인해 발생하는 위양성을 방지할 수 있었다. 또한, 환자 검체의 결과 값이 기존 보고 결과와 일치함으로 0.25 mol/L NaOH 용액이 간염 검사결과에 영향을 끼치지 않음을 확인하였다. 따라서 본 실험에서 실시한 방법이 disposable tip보다 상대적으로 경제적인 fixed tip을 사용하면서도 carryover가 없는 정확한 결과를 얻을 수 있는 효과적인 방안임을 알 수 있다.

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DLC-coated Si-tip FEA 제조에 있어서 Al 희생층을 이용한 게이트 누설 전류의 감소 (Decrease of Gate Leakage Current by Employing AI Sacrificial Layer in the DLC-coated Si-tip FEA Fabrication)

  • 주병권;이상조;김훈;이윤희;오명환
    • 대한전기학회논문지:전기물성ㆍ응용부문C
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    • 제48권8호
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    • pp.577-579
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    • 1999
  • DLC film remaining on device surface could be removed by eliminating AI sacrificial layer as a final step of lift-off process in the fabrication of DLC-coated Si-tip FEA. The field emission properties(I-V curves, hysteresis, and current fluctuation etc.) of the processed device were analyzed and the process was employed to 1.76 inch-sized FEA panel fabrication in order to evaluate its FED applicability.

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High vacuum packaging and vacuum evaluation for field emission display

  • Jung, S.J.;Woo, K.J.;Lee, N.Y.;Ahn, S.;Moon, G.J.;Kim, K.S.;Kim, M.S.
    • Journal of Korean Vacuum Science & Technology
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    • 제3권1호
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    • pp.95-97
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    • 1999
  • A 3.12" FED panel was packaged successfully using the anode plate on which phosphors and black matrix were coated and cathode plate containing emitter arrays. The vacuum level of the panel was investigated during panel evacuation, tip-off and getter activation process. The packaged panel exhibited vacuum level below 2${\times}$10-6 Torr. Similar experiments were carried out for 10" panel made of bare plates. In addition, the vacuum level of two panels was compared continuously after tip off process; one with the getter and the other without it.

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Structure of Tip Leakage Flow in a Forward-Swept Axial-Flow Fan Operating at Different Loading Conditions

  • Baek, Je-Hyun;Lee, Gong-Hee;Myung, Hwan-Joo
    • International Journal of Air-Conditioning and Refrigeration
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    • 제12권1호
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    • pp.50-60
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    • 2004
  • An experimental analysis using three-dimensional Laser Doppler Velocimetry(LDV) measurement and computational analysis using the Reynolds stress model in FLUENT are conducted to give a clear understanding of the effect of blade loading on the structure of tip leakage flow in a forward-swept axial-flow fan operating at the maximum efficiency condition ($\Phi$=0.25) and two off-design conditions ($\Phi$=0.21 and 0.30). As the blade loading increases, the onset position of the rolling-up of tip leakage flow moves upstream and the trajectory of tip leakage vortex center is more inclined toward the circumferential direction. Because the casing boundary layer becomes thicker and the mixing between the through-flow and the leakage jet with the different flow direction is enforced, the streamwise vorticity decays more fast with the blade loading increasing. A distinct tip leakage vortex is observed downstream of the blade trailing edge at $\Phi$=0.30, but it is not observed at $\Phi$=0.21 and 0.25.

입사각이 터빈 동익 팁누설유동 영역에서의 압력손실에 미치는 영향 (Effects of Incidence on Aerodynamic Losses in the Tip-Leakage Flow Region of a High-Turning Turbine Rotor Blade)

  • 채병주;이상우
    • 한국유체기계학회 논문집
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    • 제13권2호
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    • pp.41-47
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    • 2010
  • The effect of incidence angle on the three-dimensional flow and aerodynamic loss in the tip leakage flow region downstream of a turbine rotor cascade has been investigated for two tip gap-to-chord ratios of h/c=0.0% (no tip gap) and 2.0%. The incidence angle is changed to be $i=-10^{\circ}$, $0^{\circ}$, and $5^{\circ}$. The results show that for $i=5^{\circ}$, secondary flows including the passage vortex are intensified noticeably, and there is a strong interaction between the passage and tip leakage vortices. For $i=-10^{\circ}$, however, the passage vortex is weakened significantly, so that there exists only a strong leakage-jet-like secondary flows near the casing wall. For h/c=0.0% and 2.0%, aerodynamic loss tends to increase with increasing i from $-10^{\circ}$ to $5^{\circ}$. A small increment of i in its positive incidence range results in a remarkable aerodynamic loss increase, while increasing i in the negative incidence range leads to a small change in the aerodynamic loss generation.