• 제목/요약/키워드: MACH

검색결과 1,265건 처리시간 0.021초

Mach-Zehnder 변조기를 이용한 Loop-back System (Loop-back System Using Mach-Zehnder Modulator)

  • 김희주;강동성;전금수;반재경
    • 대한전자공학회논문지SD
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    • 제38권7호
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    • pp.479-485
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    • 2001
  • 본 논문에서는 광원이 불필요하며 단일 광섬유를 통하여 양방향 전송이 가능한 BS(base station)용 광송 수신기 모듈을 제안한다. 본 논문에서 제안하는 방식에서는 BS의 송신단에서 Ring type으로 구성된 Mach-Zehnder 변조기의 양방향 변조를 이용하여 CO(central office)에서 제공된 광원을 변조하여 다시 CO로 전송한다. Ring 타입으로 구성된 변조기의 등가모델을 도출하였으며, 등가모델과 측정결과가 매우 잘 일치함을 확인할 수 있었다. 또한 Ring type에서 Mach-Zehnder 변조기의 광학적인 대칭이 RF 신호 전송 특성에 중요한 영향을 미침을 확인할 수 있었다.

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광섬유 Mach-Zehnder 간섭계를 이용한 부분방전 초음파 검출특성 (Detecting Characteristics of Ultrasonics Generated by Partial Discharge in Insulating Oil Using the Optical Fiber Mach-Zehnder Interferometer)

  • 이상훈;심승환;이광식;김달우
    • 조명전기설비학회논문지
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    • 제17권4호
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    • pp.50-56
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    • 2003
  • 본 논문에서는 유입변압기 진단을 목적으로 부분방전시 발생하는 여러 가지 물리적 화학적 현상중 초음파를 검출하기 위하여 광섬유 Mach-Zehnder 간섭계를 구성하였다. 구성된 광섬유 센서의 초음파 검출 평가 실험을 실시하고, 절연유 중에 배치한 침-평판전극에 교류 고전압을 인가하여 방전시 발생하는 초음파를 측정하고 퓨리에 변환 및 wavelet 변환을 이용한 데이터 분석 결과를 나타냈다.

초음속 노즐을 통하는 부족팽창 제트에 관한 수치계산적 연구 (2) (Numerical Study on Under-Expanded Jets through a Supersonic Nozzle(II))

  • 김희동;신형승
    • 대한기계학회논문집B
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    • 제20권6호
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    • pp.1994-2004
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    • 1996
  • Numerical calculation was applied to supersonic under-expanded jets, and compared with the results of a linear theory and other experiments. TVD difference scheme was employed to solve 2-dimensional and axisymmetric inviscid Euler equation. This paper aims to explore the effects of angle of divergence and design Mach number of nozzle on the structure of under-expanded jets. The angle of divergence was varied from 0 to 20 deg. The results show that the length of the first cell of the under-expanded jets decreases and Mach disk generates at lower nozzle pressure ratio, if the angle of divergence or design Mach number of nozzle increases. The distance from the nozzle exit to Mach disk in 2-dimensional jets becomes much larger than that of axisymmetric jets, and the widths of the jet boundary and the barrel shock wave are also larger than that of axisymmetric jets. Calculation results indicate that the configuration of the under-expanded jets is strongly dependent on the nozzle pressure ratio.

원거리의 물과 오일을 구별할 수 있는 UV형광측정시스템 개발과 분석에 대한 연구 (Long Distance Identification of Water and Oil using an Ultraviolet Fluorescence Measurement System)

  • 백경훈;이준석;전수정;박보람;박성욱
    • 센서학회지
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    • 제31권4호
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    • pp.266-270
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    • 2022
  • Owing to the rising volume of seaborne trade, oil spills damage the marine environment for over 250 yearly. Thus, various analysis methods such as the Fourier-transform infrared (FTIR), Raman spectroscope, and gas chromatography are used to monitor oil spills at sea, but these methods are expensive. Recently, to reduce operational costs, an underwater fluorometer was adopted. However, this approach is not ideal for the remote sensing of oil spills because the device gets submerged in the sea. In this study, we have designed and developed a monitoring system that uses ultraviolet fluorescence to detect spilled oil or water from a distance, as well as proposed an analyzing method defining based on water Raman signal and QF535. Each fluorescence spectrum of water, oil (crude oil), and Bunker A was obtained using the system, and was calculated and analyzed from the spectrum individually. Based on the results of the analysis, we could successfully identity water and oil at a long distance.

Analytical and computational analysis of pressure at the nose of a 2D wedge in high speed flow

  • Shaikh, Javed S.;Kumar, Krishna;Pathan, Khizar A.;Khan, Sher A.
    • Advances in aircraft and spacecraft science
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    • 제9권2호
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    • pp.119-130
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    • 2022
  • Supersonic projectiles like rockets, missiles, or aircraft find various applications in the field of defense. The shape of the wings is mainly designed as wedge shape or delta wings for supersonic vehicles. The study of supersonic flows over the wedges and flat plate delta wings around the large scale of incidence angle is considered in the supersonic projectile. In the present paper, the prime attention is to study the pressure at the nose of the plane wedge over the various Mach number and the various angles of incidence. Ghosh piston theory is used to obtain the pressure distribution analytically, and the results are compared with CFD analysis results. The wedge angle and Mach number are the parameters considered for the research work. The range of wedge angle is 50 to 250, and Mach number is 1.5 to 4.0 are considered for the current research work. The analytical results show excellent agreement with the CFD results. The results show that both the parameters wedge angle and Mach number are influential parameters to vary the static pressure. The static pressure increases with an increase in Mach number and wedge angle.

광통신용 $Ti:LiNbO_3$외부 광변조기/스위치 설계

  • 김창민;정석원
    • 전기의세계
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    • 제44권9호
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    • pp.28-37
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    • 1995
  • 외부 광스위치/변조기로는 차단형(cut-off type)[1], 균일 방향성 결합기(uniform directional coupler)[2-4], Mach-Zehnder 간섭계(Mach-Zehnder interferometer)[5-7], 교번 .DELTA..betha. 방향성 결합기(alternation directional coupler)[8-9], 교차 결합기(crossed coupler[10-11], Y-분기 방향성 결합기(Y-branch directional coupler)[12-14] 등의 여러가지가 연구되어졌다. 본 논문에서는 위에서 열거한 여러 가지 광변조기를 해석, 설계하는데 기본이 되는 광결합 이론으로 normal mode 이론과 coupled mode 이론을 소개한다. 아울러 이러한 이론들을 이용하여 전술한 변조기 중 균일 방향성 결합기, Y-분기 방향성 결합기, Mach-Zehnder 간섭계의 광스위칭/변조 원리를 살펴본다.

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복굴절, 입력 편광상태 및 광손실이 광섬유간섭계의 visibility에 미치는 영향 (The visibility variation of the mach-zehnder optical fiber interferometerdue to birefringences, input states of polarization and optical losses)

  • 강현서;이영택;이경식
    • 전자공학회논문지A
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    • 제33A권2호
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    • pp.140-147
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    • 1996
  • The output of the mach-zehnder optical fiber interferometer varies with birefringences existing in the figer arms. New equations experessing for the visibility of the mach-zehnder interferometer were derived in terms of a number of parameters related to the birefringences, the input SOP and the optical losses. Based on the equations the visibility of the interferometer was simulated in different cases. Some maximum visibility conditons were also presented.

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미소 저주파 자기장 측정을 위한 Mach-Zehnder 형 광섬유 간섭계 쎈서의 특성조사 (Sensitive Fiber-Optic Mach-Zehnder Interfermeter for the Detection of Low Frequency Magnetic Field)

  • 안준태
    • 한국광학회:학술대회논문집
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    • 한국광학회 1991년도 제6회 파동 및 레이저 학술발표회 Prodeedings of 6th Conference on Waves and Lasers
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    • pp.109-109
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    • 1991
  • 자기변형 효과가 큰 Metallic glass 2605SC에 20cm의 광섬유를 붙여서 교류 자기장 측정을 위한 Mach-Zehnder형 광섬유 간섭계를 구성하였다. 능동 위상 추적 방법을 사용하여 간섭계의 위상차를 최대 측정감도를 갖는 $\pi$/2로 고정시킴으로써 온도 및 진동등의 영향에 의한 신호소멸 현상을 해결하였다. 0.2~2.0 KHz에서 주파수특성, dc bias의 영향 그리고 교류 자기장과 간섭계 출력 사이의 선형성을 조사하였다.

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극초음속 쐐기 유동의 Viscous Interaction (Hypersonic Viscous Interaction of Wedge Flows)

  • 김규홍;노오현
    • 한국전산유체공학회:학술대회논문집
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    • 한국전산유체공학회 1996년도 춘계 학술대회논문집
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    • pp.40-45
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    • 1996
  • This paper discribes the viscous interaction of Hypersonic Wedge Flows using Roe FDS and AUSM+. For this purpose we developed the frozen and the equilibrium code and numerically simulated the viscous interaction by changing the surface temperature and the mach number. We used curve fitting data in NASA Reference Publication 1181, 1260 to calculate equilibrium properties. We compare the equilibrium flow with the frozen flow. We conclude that the mach number and the surface temperature are significant parameters, as the surface temperature and the mach number increase the viscous interaction becomes stronger, and we must consider high-temperature effects in hypersonic flow

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초고속 광통신용 5Gbps 급 Ti:LiNbO$_3$ Mach-Zehnder interferometric 광변조기 개발 (Development of 5Gbps Ti:LiNbO$_3$ Mach-Zehnder Interferometric Optical Modulator for High-speed Optical Communications)

  • 김성구;윤형도;윤대원;유용택
    • 한국전기전자재료학회:학술대회논문집
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    • 한국전기전자재료학회 1997년도 추계학술대회 논문집
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    • pp.477-479
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    • 1997
  • The preparation of mach-zehnder inteferometric optical modulator and the properties of electrode and modulation bandwidth for high speed optical communications were described. The results of fabricated optical modulator was that optical 3-dB bandwidth 4.7GHz, driving voltage 6V and fiber-waveguide-fiber insertion loss 4.5dB for TM mode respectively.

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