• Title/Summary/Keyword: 시간측정 위치

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Ignition Transition by Ignition Position and time of Gaseous Oxygen/Kerosene Combustor (기체산소/케로신 연소기에서 점화 위치 및 시간에 따른 점화 과정 연구)

  • Song, Wooseok;Son, Min;Shin, Dongsoo;Koo, Jaye
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2017.05a
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    • pp.814-819
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    • 2017
  • The objective of this paper is to observe effects of an ignition position and time on the ignition transition. A gaseous oxygen and liquid kerosene are used for propellants with the shear-coaxial injector. In order to study the ignition delay time and combustion instability intensity, the pressure transducer was used. The ignition position was changed with the injector spacer. Sequences except the igniter operation time were fixed to compare the ignition time only. Initial pressure peak and ignition delay time increased as the ignition time was delayed. Also, the unstable flame development zone was detected as the igniter was away from the injector.

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Partial Discharge Sensor Characteristics for Distriminating Location in Power Cable (전력 케이블의 부분방전 위치 추정용 센서 특성 연구)

  • Nam, S.H.;Shin, D.S.;Kwon, Y.H.;Lee, S.J.;Kim, D.W.
    • Proceedings of the KIEE Conference
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    • 2002.11b
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    • pp.326-328
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    • 2002
  • 본 논문에서는 케이블 내전압 시험 및 부분 방전 측정 시험에 사용될 수 있는 전구 차단 장치의 차단 기준에 큰 영향을 미치는 케이블 부분방전 센서의 특성에 관한 연구를 수행하였다. 특히, 부분방전 발생시 부분방전 발생 위치를 보다 정확하게 판별할 수 있는 센서의 종류 및 구조를 주파수 특성과 시간 특성을 함께 측정한 결과를 보고한다.

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Structural Damage Assessment Using Transient Dynamic Response (동적과도응답을 사용한 구조물의 손상진단)

  • 신수봉;오성호;곽임종;고현무
    • Journal of the Computational Structural Engineering Institute of Korea
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    • v.13 no.4
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    • pp.395-404
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    • 2000
  • A damage detection and assessment algorithm is developed by measuring accelerations at limited locations of a structure under forced vibrations. The developed algorithm applies a time-domain system identification (SI) method that identifies a structure by solving a linearly constrained nonlinear optimization problem for optimal structural parameters. An equation error of the dynamic equilibrium of motion is minimized to estimate optimal parameters. An adaptive parameter grouping scheme is applied to localize damaged members with sparse measured accelerations. Damage is assessed in a statistical manner by applying a time-windowing technique to the measured time history of acceleration. Displacements and velocities at the measured degrees of freedom (DOF) are computed by integrating the measured accelerations. The displacements at the unmeasured DOF are estimated as additional unknowns to the unknown structural parameters, and the corresponding velocities and accelerations we computed by a numerical differentiation. A numerical simulation study with a truss structure is carried out to examine the efficiency of the algorithm. A data perturbation scheme is applied to determine the thresholds lot damage indices and to compute the damage possibility of each member.

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첨단장비시대 - 인공위성자동위치측정시스템(GPS)

  • Jeong, Man-Yeong
    • The Science & Technology
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    • v.30 no.11 s.342
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    • pp.82-83
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    • 1997
  • GPS는 2개 이상의 인공위성에서 발사된 극초단파를 수신하여 이동물체의 위도, 경도, 높이, 표준시간 등을 정확히 파악할 수 있는 최첨단 장비이다. 뛰어난 효능으로 걸프전 때도 각광을 받았던 이 항법시스템은 안개나 사막의 먼지 속에서도 물체의 정확한 위치를 안내해 준다.

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Development of Ceramic Pepper Dryer (세라믹 고추 건조기 개발)

  • Cho, Hyun-Seob
    • Proceedings of the KAIS Fall Conference
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    • 2008.11a
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    • pp.178-180
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    • 2008
  • 세라믹 건조기를 개발하기 위하여 탄화규소가 주원료로한 세라믹 발열판을 제작하여 건조기 내부에 설치하여 실험하였다. 발열판 장착위치에 따른 실험결과 위치는 큰 변수가 되지 않았고, 발열판 자체 온도 분포를 측정한 결과 시간이 흐름에 따라 온도 분포는 약간의 차이가 있기는 하지만 대체적으로 균일한 분포를 나타내었다.

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A Practical Method of Acoustic Emission Source Location in Anisotropic Composite Laminates (이방성 적층복합재 구조에서 AE 발생원 위치표정을 위한 실용적인 방법)

  • Kim, Jeong-Kon;Kang, Yong-Kyu;Kwon, Oh-Yang
    • Journal of the Korean Society for Nondestructive Testing
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    • v.23 no.3
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    • pp.237-245
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    • 2003
  • Since the velocity is dependent on the fiber orientation in anisotropic composites, the application of traditional acoustic emission (AE) source location techniques based on the constant velocity to composite structures has been practically impossible. The anisotropy makes the source location procedure complicated and deteriorates the accuracy of the location. In this study, we have divided the region of interest(ROI) into a set of finite elements, taken each element as a virtual source, and calculated the arrival time differences between sensors by using the velocities at every degree from 0 to 90. The calculated and the experimentally measured values of the arrival time difference aye then compared to minimize the location error. The results from two different materials, namely AA6061-T6 and CFRP(uni-directional; UD, $[0]_{32}4$) laminate confirmed the practical usefulness of the proposed method.

Analysis on Activation Characteristic of Heat Detectors in a Compartment Fire (실내화재에서의 열감지기 동작특성 분석)

  • Ryu, Hocheol
    • Journal of the Society of Disaster Information
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    • v.10 no.4
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    • pp.598-608
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    • 2014
  • The first operation of alarm system starts at a detector. And the largest effect is produced on the operation of detector by the fire source position and installation position. Nevertheless, the Korean standard for the installation of detector only specifies matters of fire detector installation according to area and height, without consideration of installation position and fire source position. Therefore, this study carried out a fire test in consideration of detector installation position and fire source position (5 places) in order to minimize casualties owing to the fast operation of fire detector when a fire occurred. Considering that it took the longest time for a detector close to a wall to work in the results of this test, it was possible to find that a minimum clearance to the wall was required.

Vibration Sensing and Impact Location Measurement Using Intensity-Based Optical Fiber Vibration Sensor (광강도형 광섬유 진동센서를 이용한 진동감지 및 충격위치 측정)

  • 양유창;황운봉;박현철;한경섭
    • Composites Research
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    • v.13 no.5
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    • pp.1-9
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    • 2000
  • An intensity-based optical fiber vibration sensor is applied to monitor the structural vibration and detect impact locations on a plate. Optical fiber vibration sensor is constructed by placing two cleaved fiber end, one of which is cantilevered in a hollow glass tube. The movement of the cantilevered section lags behind the rest of the sensor in response to an applied vibration and the amount of light coupled between the two fibers is thereby modulated. For vibration sensing, optical fiber vibration sensor is mounted on the carbon fiber composite beam and its response is investigated to free and forced vibration. In impact location detection, four optical fiber vibration sensors whose location is predetermined are placed at chosen positions and the different arrival times of impact-generated vibration signal are recorded by an FFT analyzer. Impact location can be calculated from these time delays. Experimental results show that optical fiber vibration sensor signals coincide with gap sensor in vibration sensing. The precise location of impact can be detected on an acrylate plate.

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A Spatiotemporal Location Prediction Method of Moving Objects Based on Path Data (이동 경로 데이터에 기반한 이동 객체의 시공간 위치 예측 기법)

  • Yoon, Tae-Bok;Park, Kyo-Hyun;Lee, Jee-Hyong
    • Journal of the Korean Institute of Intelligent Systems
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    • v.16 no.5
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    • pp.568-574
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    • 2006
  • User adaptive services have been important features in many applications. To provide such services, various techniques with various kinds of data are being used. In this paper, we propose a method to analyze user's past moving paths and predict the goal position and the path to the goal by observing the user's current moving path. We develop a spatiotemporal similarity measure between paths. We choose a past path which is the most similar to the current path using the similarity. Based on the chosen path, user's spatiotemporal position is estimated. Through experiments we confirm this method is useful and effective.

Residual Propellant Gauging Methods for Geostationary Satellites and Recent Technology Status (정지궤도위성의 잔여추진제량 측정방법 및 기술동향)

  • Park, Eungsik;Huh, Hwanil
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.42 no.10
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    • pp.870-877
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    • 2014
  • Geostationary satellites undergo various orbital perturbations and this results in location change. Therefore, all the geostationary satellites use the thruster in order to control the location change. For this purpose, the suitable amount of liquid propellant is mounted and the amount of propellant is reduced as time goes by. This means that the lifetime of the satellite depends on the residual propellant amount. Therefore precise residual propellant gauging is very important for the mitigation of economic losses arised from premature removal of satellite from its orbit, satellites replacement planning, slot management and so on. In this paper, we introduce the propellant gauging methods used in the geostationary satellites and the propellant gauging method studied in the laboratory level.