• Title/Summary/Keyword: 압력 간섭

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Multiplexed fabry-perot interferometric sensor system (다중화 Fabry-Perot 간섭형 광섬유 센서 시스템)

  • 나도성;예윤해;이동영;박광순
    • Korean Journal of Optics and Photonics
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    • v.10 no.4
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    • pp.273-278
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    • 1999
  • A TDM-multiplexed fiber optic pressure/temperature sensor system utilizing fiber optic Fabry-Perot interferometers as sensing devices was developed and applied to measure water level variations and temperature variations. The maximum measurement speed of the system without saving measurement data is 4500 times per second and the response time of the sensors is thought to be ~ms. The difference between the theoretical value and the measured value for the scale factor of water level sensor and temperature sensor was +13.7%, -18% respectively. The nonlinearity of the sensors after calibration was less than 1%. The sensor system was applied to verify the capability of measuring the temperature variations and water level variations at a high speed.

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A Measurement Method of Internal Defects of Pressure Vessles by Using Real-Time Holographic Interferometry (실시간 홀로그래픽 간섭법을 이용한 압력용기의 내부결함 측정법)

  • Moon, Sang-Joon;Kang, Young-June;Baik, Sung-Hoon;Kim, Cheol-Jung
    • Transactions of the Korean Society of Mechanical Engineers A
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    • v.20 no.4
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    • pp.1233-1240
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    • 1996
  • Conventional measurement methods using ultrasonic wave or x-ray, eddy current for non-destructive testing(NDT) in nuclear power plants and other industrial plants have been utilized as the method of contact with objects to be inspected. For this reason these methods require relatively much time and inspection area is limited by the location of probe or film. But holograpic interferometry which is a non-contact optical measurement method using a coherent light source has an advantage that quantative measurement can be performed at a time. In this paper a new method using realtime holographic interfreometry and image processing for detecting internal flaws of pressure vessels is presented.

Experimental Study on the Blade Excitation Frequency for the Natural Frequence of Centrifugal Pump Piping Systems (원심펌프 배관계 진동에 영향을 주는 블레이드 가진주파수의 실험적 고찰)

  • 김윤제;신호길
    • Journal of Energy Engineering
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    • v.10 no.4
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    • pp.335-341
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    • 2001
  • Pressure pulsations generated by the blade-tongue interaction induce vibration of the piping systems and the structure connected to pumps, resulting in the severe noise and fatigue fracture. Experiments were made on the natural frequencies of liquid columns in piping systems with a single suction, single stage, centrifugal volute pump. Experimental results show that the natural frequencies of the liquid columns in the pump piping systems depend on the dimensions of the pipes and the impeller shapes, and are not affected substantially by the rate of discharge and the rotating speed of the pump.

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Control of High-Pressure Exhaust Gas Flows Using Shock-Wave Confinement (충격파 감금법을 이용한 고압배기가스 유동의 제어)

  • ;;K.Matsuo
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 1998.04a
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    • pp.19-19
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    • 1998
  • 최근 화학, 연소, 동력, 제철 등의 각종 플랜트에서 조업압력이 고압화되어 가고 있으며, 이에 수반하여 배관계를 통하는 고압가스 유동에 관한 연구가 활발하게 진행되고 있다. 배관계를 통하는 고압가스의 유동에 있어서 유량의 적절한 제어, 유동에 의하여 야기되는 배관계의 소음·진동, 그리고 배기가스의 적절한 처리법 등은 공학적으로 매우 중요한 문제로 알려져 왔다. 일반적으로 정상운전을 하는 플랜트에서 고압 배기가스의 문제는 배기가스 Expander에 의하여 에너지를 회수하는 방법이 생각될 수 있으나, 실제 공업현장에서는 배기가스를 안전하고, 또 소음·진동을 발생시키지 않도록 적절하게 처리하는 것이 매우 중요한 기술적 과제로 남아 있다. 일반적으로 배기가스의 압력이 임계압력(critical pressure) 이상으로 되는 경우(실제 대부분의 플랜트에서 배기가스의 압력은 임계압력보다 매우 높다), 배관계 내부에서 충격파(shock-wave)가 발생하여 난류와동 혹은 난류경계층과 간섭하게 됨으로써 강력한 공기역학적 소음이나 진동을 발생시키게 된다. 이와 같은 소음·진동에 대한 대책으로는 현재 가스배출부에 감압밸브를 직렬로 설치하거나, 유로에 다공판(porous plates)들을 삽입하여 감압과정을 공간적으로 분산시킴으로써, 충격파가 발생하지 않도록 하는 방법을 주로 채택하고 있다. 그러나 이러한 방법을 적용하는 경우 배기가스 유동에 대한 유량의 제어기능이 저하되는 문제가 발생한다.

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Study on Unsteady Flow Field around Rectangular Cylinders using Proper Orthogonal Decomposition (POD) (POD를 이용한 구조기본단면 주변 비정상흐름장 특성에 관한 연구)

  • Lee, Jae-Hyung;Matsumato, Masaru
    • Journal of Korean Society of Steel Construction
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    • v.20 no.6
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    • pp.751-759
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    • 2008
  • In this study, the effect of an unsteady flow field around a body of aerostatic/aerodynamic forces were investigated using rectangular cylinders (B/D = 2, 3, 4, 5). Proper orthogonal decomposition (POD) was introduced to the analysis of the fluctuating pressure field that was measured on the stationary/oscillatory B/D=4 rectangular cylinder, and the characteristics of the proper functions with flow patterns were identified. In addition, the physical decoupling and interactions in the different co-existing flow patterns were investigated through POD. The comparison with the identified proper function associated with a particular flow pattern revealed that the Karman vortex is almost not affected by the separation bubble, but that the Karman vortex considerably interferes in the development of the separation bubble around the trailing edge. It can be considered that the Karman vortex induces the increment of the curvature of the substantial separated flow.

Numerical Analysis of the Turbine Rotor Flow with the Unsteady Passing Wake from a Stator (정익에서 발생한 비정상 후류를 지나는 터빈 동익 유동장 수치해석)

  • Lee, Eun-Seok
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.35 no.4
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    • pp.275-280
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    • 2007
  • A turbine stage consists of stators and rotors. The stator provides the required inlet flow conditions so that the rotor can produce the necessary power. Passing wakes generated from the trailing edge of the stator make an interaction with the rotor. In the present study, this flow mechanism is investigated using the numerical analysis. In case of a large gap distance between the stator and rotor, the flow can be solved independently. First, only the stator flow field is solved. Second, the rotor flow field is solved including the passing wake characteristics obtained from the stator analysis. The passing wake experiences the shearing as it approaches to the rotor blade leading edge. And it is chopped when it strikes the rotor blade. After that, the chopped wakes becomes the prolongation as it travels downstream. The flow according to the variation of the gap distance is also studied. Pressure jumps due to the passing wakes result in the pressure and lift loss and it gets stronger with the closer gap distance.

TPMS Interference Suppression Based on Beamforming (Beamforming을 이용한 TPMS 간섭제거)

  • Hwang, Suk-Seung;Kim, Seong-Min;Park, Cheol
    • The Journal of the Korea institute of electronic communication sciences
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    • v.6 no.2
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    • pp.180-185
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    • 2011
  • The TPMS(Tire Pressure Monitoring System) is an electronic system designed to display the air pressure inside the pneumatic tires and report real-time tire-pressure information to the driver of the vehicle, either via a gange, a pictogram display, or a simple low-pressure warning light. Although the data measured by TPMS sensor is transmitted to internal signal processer in a vehicle through wireless communication, the receiver may suffers from various interferences such as amateur radio station, RFID(Radio-Frequency IDentification) for controlling container, RKE(Remote Keyless Entry) signal, and so on. In this paper, we consider beamforming technology to suppress various high-power interference signals for the TPMS wireless communications. Also, we propose the proper data structure and antenna arrangement for the beamformer inside the vehicle. The performance for the interference suppression is illustrated by computer simulation example.

Aerodynamic Characteristics of Supersonic Jets Impinging on $60^{\cire}$ Wedge (꼭지각이 $60^{\cire}$인 쐐기에 충돌하는 초음속 제트의 공기역학적 특성)

  • 박종호;이택상;김윤곤
    • Journal of the Korean Society of Propulsion Engineers
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    • v.8 no.1
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    • pp.8-15
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    • 2004
  • Supersonic jets impinging on $60^{\cire}$ wedge were investigated to obtain fundamental design data for jet deflector It was of interest to study flow phenomena such as shock interaction and separation induced by shear layer. Experiments using supersonic cold flow system were conducted for Schlieren flow visualization and measurement of surface pressure. Numerical results were compared with the experimental results. The major parameters are underexpansion ratio, distance from nozzle to apex and design Mach number. Flow conditions were obtained for the wedge shock to attach on or detach from the wedge. The dominant feature of flow-field is shock pattern induced by the Interaction between the wedge shock and the barrel shock.

The analysis of interferometry fringe pattern under shearing quantity and inside pressure change for inspect inside defects using by digital shearography (Digital shearography를 이용한 내부결함 검출에 있어서 전단량과 내부압력 변화에 따른 간섭줄무늬 패턴 분석)

  • 김형택;김경석;홍진후;강기수
    • Proceedings of the Korean Society of Precision Engineering Conference
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    • 2001.04a
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    • pp.140-143
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    • 2001
  • Digital shearography, a speckle pattern method is based on the superposition of two laterally sheared images. Therefore, object points which are positioned in some distance from each other are superposed in the image plane. This shearography, one of NDT methods without contact, is able to inspect defects in pipelines and pressure vessels that are used in nuclear power plants. This is can inspect whole fields and has a low sensitivity to environmental noise. Because optical setting is very simple, it has a little exhaustion of time, cost and man power. And also it can find a defect position through real time monitoring of a part. This paper, finds out the relationship among shearing quantity image quality and defect size with this method.

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A study of Main Rotor Blade Tip shape and analysis of flow around Main Rotor Blade Tip (Main Rotor Blade Tip 형상 변화에 따른 유동분석)

  • Kim, Se-Il
    • Proceeding of EDISON Challenge
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    • 2013.04a
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    • pp.382-386
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    • 2013
  • 본 연구에서는 Main Rotor Blade Tip 형상 변화에 따른 후류해석을 통해 와류 생성 및 주변 유동을 분석하여 블레이드 팁 형상의 변화가 와류 간섭을 감소시키는지의 여부를 확인하였다. EDISON CFD를 이용하여 블레이드 Blade Tip 형상에 따라 유동이 어떻게 나타나며, Blade 후류의 압력과 점성의 변화를 분석하여 와류의 양상을 해석하였다. 비교 Blade 형상은 2세대 긴 직사각형 모형, KUH 수리온의 Blade, 유로콥터사의 'Blue Edge'로 비교적 최근에 개발된 대표적인 Blade Tip 형상 3개로 정하였다. 결과를 토대로 블레이드 뒷전의 와류흐름 양상을 확인하여 블레이드 와류 간섭현상의 감소를 확인하였다.

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