• Title/Summary/Keyword: He-Ne laser

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Study of Flame Structure by Chemiluminescence and Laser Diagnostics in Model Gas Turbine Combustor (자발광 및 레이저 계측기법을 이용한 모형 가스터빈 연소기에서 화염구조 분석)

  • Yoon, Ji-Su;Kim, Min-Ki;Lee, Min-Chul;Yoon, Young-Bin
    • Journal of the Korean Society of Propulsion Engineers
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    • v.16 no.5
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    • pp.10-19
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    • 2012
  • To eliminate the onset of combustion instabilities and develop effective approaches for control, flame structure is very important. In this study, we conducted experiments under various operating conditions with a model gas turbine combustor to examine the relation of combustion instability and flame structure by OH chemiluminescence and laser diagnostics of He-Ne laser absorbtion system. The swirling LNG($CH_4$)/air flame was investigated with overall equivalence ratio of 1.2 and dump plane fuel-air mixture velocity 25 ~ 70 m/s. We founded that the combustion instability phenomenon occurs at lower mixing velocity and higher mixing velocity conditions. We also concluded that fluid dynamical vortex frequency has major effects on the combustion instability characteristics at lower mixing velocity condition.

A study of room temperature PR(photoreflectance) charicteristics for AlGaAs/GaAs multiple-quantum well (AlGaAs/GaAs multiple-quantum well에 대한 상온에서의 photoreflectance 특성연구)

  • 김동렬;최현태;배인호;김말문;한병국;우덕하;김선호;최상삼
    • Journal of the Korean Vacuum Society
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    • v.6 no.2
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    • pp.109-113
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    • 1997
  • PR spectra of MBE grown AlGaAs/GaAs MQW have been measured at room temperature using the He-Ne laser and the Ar laser as the pump source. We have observed various subband transition peaks and PR spectra were fitted to standard analytic line shape. Above that results, obtained us transition energy from n=1 conduction band to heavy hole(C1-H1) and to light hole(C1-L1) subband. Photoluminescence(PL) at room temperature showed main peak with a shoulder. Good agreement between PL and PR measured n=1 intersubband transition energies was confirmed that PL main peak with a shoulder is associated with the C1-H1, C1-L1 transition. Additionally, we have calculated the C1-H1 and C1-L1 intersubband energy within envelope function approximation(EFA).

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Study of Flame Structure by Chemiluminescence and Laser Diagnostics in Model Gas Turbine Combustor (자발광 및 레이저 계측기법을 이용한 모형 가스터빈 연소기에서 화염구조 분석)

  • Yoon, Ji-Su;Kim, Min-Ki;Lee, Min-Chul;Yoon, Young-Bin
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2012.05a
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    • pp.367-376
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    • 2012
  • To eliminate the onset of combustion instabilities and develop effective approaches for control, flame structure is very important. In this study, we conducted experiments under various operating conditions with a model gas turbine combustor to examine the relation of combustion instability and flame structure by OH chemiluminescence and laser diagnostics of He-Ne laser absorbtion system. The swirling LNG(CH4)/air flame was investigated with overall equivalence ratio of 1.2 and dump plane fuel-air mixture velocity 25 ~ 70 m/s. We founded that the combustion instability phenomenon occurs at lower mixing velocity and higher mixing velocity conditions. We also concluded that fluid dynamical vortex frequency has major effects on the combustion instability characteristics at lower mixing velocity condition.

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A study on the Real time Observation of Microscopic Change with Focused Laser Beam (집속된 레이저빔을 이용한 미소변화의 실시간 관찰에 관한 연구)

  • Jang, Heui-Sung;Lee, Hyuk
    • Proceedings of the KIEE Conference
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    • 1993.11a
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    • pp.356-358
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    • 1993
  • With a focused laser beam, we make a microscopic change on a thin film, and organize the overall system that can observe the change with a microscope. This system utilizes the energy of a laser beam which is focused by a simple lense system. That is a laser beam which has its waist at working distance of a lense. The microscopic change induced by the energy of laser beam focused through a lense can be observed in real time. The experiment with this system shows that the 10mW He-Ne 632.8nm laser can change the black vinyl instantaneously.

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Fabrication of Fresnel zone plate with femtosecond laser lithography technology (펨토초 레이저 리소그라피 기술을 이용한 Fresnel zone plate 제작 연구)

  • Sohn, I.B.;Noh, Y.C.;Ko, M.J.
    • Laser Solutions
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    • v.14 no.2
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    • pp.13-16
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    • 2011
  • We fabricated the Fresnel zone plate using femtosecond laser lithography-assisted micro-machining, which is a combined process of nonlinear lithography and wet etching. We investigated the focusing properties by launching a 632.8nm wavelength He-Ne laser beam into the zone plate. The spot size of the primary focal point was $27{\mu}m$ and the intensity of focal point was 0.565W/$cm^2$.

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Study on Clinical Effect of Low Level Laser Therapy by Live Blood Analysis (생혈액분석을 통한 저용량 He-Ne 레이저 유침치료에 관한 임상적 연구)

  • Kim, sung-chul
    • Journal of Acupuncture Research
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    • v.18 no.3
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    • pp.23-34
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    • 2001
  • Objective : The purpose of this study was to investigate the effect of Intravascular Laser Irradiation of Blood(ILIB) by the live blood analysis. Methods : We had analysed the changing forms of the live blood samples with Ultra Darkfield Microscope before and after Intravascular Laser Irradiation of Blood. Results and Conclusion : 1. Nomal Erythrocytes were increased significantly after ILIB by the live blood analysis. 2. Poikilocytes were decreased significantly after ILIB by the live blood analysis. 3. Target Cells were decreased significantly after ILIB by the live blood analysis. 4. Somatid was improved significantly after ILIB by the live blood analysis. 5. Erythrocyte Aggregtion was improved significantly after ILIB by the live blood analysis.

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The Design of Path Length Controller in Ring Laser Gyroscope for Attitude Control in the space launch vehicle (우주발사체 자세제어용 링 레이저 자이로 피에조 구동기 설계)

  • Kim, Eui-Chan;Yang, Koon-Ho
    • Aerospace Engineering and Technology
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    • v.9 no.2
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    • pp.31-35
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    • 2010
  • The Ring Laser Gyroscope makes use of the Sagnac effect within a resonant ring cavity of a He-Ne laser and has more accuracy than the other gyros. The space launch vehicle use require the high accuracy Gyro to control and determine the altitude to deliver the satellite in the space. In this paper, The theory of the Path Length Control is explained. The electrical design of Path Length Controller is described. The Design for Path Length Controller is composed of the demodulator, integrator, phase shifter, high voltage amplifier. We apply the circuit to 28cm square ring laser gyro and get the test results.

The Design of Path Length Controller in Ring Laser Gyroscope for Attitude Control in the LEO satellite (위성 자세제어 자이로 센서 피에조 구동기 설계)

  • Kim, Eui-Chan
    • Proceedings of the IEEK Conference
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    • 2009.05a
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    • pp.341-343
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    • 2009
  • The Ring Laser Gyroscope makes use of the Sagnac effect within a resonant ring cavity of a He-Ne laser and has more accuracy than the other gyros. The Low Earth Orbit satellite for observatory use require the high accuracy Gyro to control and determine the altitude because of the need of payload pointing accuracy. In this paper, The theory of the Path Length Control is explained. The electrical design of Path Length Controller Is described. The Design for Path Length Controller is composed of the demodulator, integrator, phase shifter, high voltage amplifier. We apply the circuit to 28cm square ring laser gyro and get the test results.

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The Design of Path Length Controller in Ring Laser Gyroscope for Attitude Control in the LEO satellite (저궤도 위성 자세제어를 위한 자이로의 광경로 제어기 설계)

  • Kim, Eui-Chan;Lee, Heung-Ho
    • The Transactions of The Korean Institute of Electrical Engineers
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    • v.57 no.2
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    • pp.256-260
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    • 2008
  • The Ring Laser Gyro makes use of the Sagnac effect within a resonant ring cavity of A He-Ne laser and has more accuracy than the other Gyros. The Low Earth Orbit satellite for observatory use require the high accuracy Gyro to control and determine the altitude because of the need of payload pointing accuracy. In this paper, The theory of the Path Length Control is explained. The electrical design of Path Length Controller is described. The Design for Path Length Controller is composed of the demodulator, Integrator, Phase shifter, High Voltage Amplifier. We apply the circuit to 28cm square ring laser gyro and get the test results.

The Design of Path Length Controller in Ring Laser Gyroscope for Attitude Control in the LEO satellite (저궤도 위성 자세제어 센서 RLG 피에조 구동기 설계)

  • Kim, Eui-Chan;Lee, Heung-Ho
    • The Transactions of The Korean Institute of Electrical Engineers
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    • v.57 no.9
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    • pp.1584-1588
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    • 2008
  • The Ring Laser Gyroscope makes use of the Sagnac effect within a resonant ring cavity of a He-Ne laser and has more accuracy than the other gyros. The Low Earth Orbit satellite for observatory use require the high accuracy Gyro to control and determine the altitude because of the need of payload pointing accuracy. In this paper, The theory of the Path Length Control is explained. The electrical design of Path Length Controller is described. The Design for Path Length Controller is composed of the demodulator, integrator, phase shifter, high voltage amplifier. We apply the circuit to 28cm square ring laser gyro and get the test results.