• Title/Summary/Keyword: simulator(모사장치)

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Ignition properties in simulator of 120mm tank charges (120mm 전차탄용 모사 장치에서의 점화 특성)

  • 이정환;권순길;황준식;김동섭;김태인;김진호
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2003.10a
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    • pp.43-46
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    • 2003
  • This study was conducted via diagnostics in a transparent 120mm tank gun chamber simulator. Pressure rises at the breech and forward ends of the simulator chamber were measured by using PCB pressure gages. This technique has been used to develope of various advanced HEAT and KE rounds of 120mm tank gun. In the studies, many ignition phenomena occurring during the early phase of the ballistic cycle was observed and analyzed. It can provide insights into the functioning of the igniter, flame spreading, and formation of pressure waves in the gun chamber.

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Development of Test Simulator for Developing Fuel Quantity Measurement System for Supersonic Jet Trainer Conformal Fuel Tank (초음속항공기 보조연료탱크 연료량측정시스템 개발용 모사시험장치 개발)

  • Kim, Bong-Gyun;Park, Dae-Jin;Jeon, Hyeon-Wu;Lee, Sangchul
    • Journal of the Korean Society for Aviation and Aeronautics
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    • v.26 no.2
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    • pp.76-82
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    • 2018
  • A test simulator is needed to develop a fuel quantity measurement system that takes into account the roll and pitch motion of the aircraft. In this paper, we develop a test simulator that consists of attitude simulation equipment, fueling equipment, and data storage equipment. The attitude simulation equipment simulates the aircraft attitude. It is manufactured to operate pitch angle and roll angle movement. The fueling equipment supplies fuel to the supplementary fuel tank. The data storage equipment collects and stores the measured data. We also develop an automation software that operates the test simulator and collects data automatically. The test simulator has been automated to prevent testers from being exposed to toxic fuel. Through automation software, the collection period is reduced by one quarter compared to manual collection. The developed fuel quantity measurement system is verified through the test simulator.

AC-PDP에서 VDS를 이용한 구동파형 최적화 연구

  • 고재준;김영권;이춘우;조광섭;최은하
    • Proceedings of the Korean Vacuum Society Conference
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    • 2000.02a
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    • pp.196-196
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    • 2000
  • 본 연구에서는 다용도 구동 모사 장치인 VDS(versatile driving simulator)를 이용하여 기존에 상용되고 있는 AC-PDP의 파형 분석 및 구동 파형 최적화를 위한 기초 연구 결과들을 소개한다. 일반적으로 PDP, FED, LCD 등의 평판 표시장치들은 패널 자체의 특성 뿐만 아니라 패널에 인가되는 전압 파형과 구동 방법에 따라 효율 및 화질을 포함한 전체 성능이 크게 좌우된다. 따라서 각 표시장치에 가장 적합한 파형과 구동법을 연구하는 것은 매우 중요한 과제이다. 특히 PDP의 경우 구동 파형이 효율과 화질에 미치는 영향은 절대적이라 해도 과언이 아니다. 그러나 이들 평판 표시장치를 구동하는 상용회로들은 스위칭 회로를 이용한 것이 대부분으로 한 개의 파형 당 한 부분의 회로가 담당하는 형태로 되어 있다. 즉 자유도가 매우 제한되어 있다. 따라서 파형 변화에 따른, 그리고 구동법의 변화에 따른 연구를 하기 위해서는 많은 인력과 시간이 소요된다는 어려움이 있다. 이러한 문제점을 해소하기 위하여 새로운 개념의 구동모사 장치 VDS(versatile driving simulator)를 개발하였다. VDS 시스템은 디지털 기술과 아날로그 기술을 통합하여 제작된 구동 모사장치로써 평판 표시 장치에 인가되는 실제 파형 및 구동법을 손쉽게 변화시킬 수 있으며 이의 결과를 빠르게 확인할 수 있도록 설계되었다.

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The study of mechanical human respiratory simulator via characteristic test of motor and proportional valve (모터와 비례제어 밸브의 특성실험을 통한 기계적 호흡 모사장치연구)

  • Lee, M.K.;Lee, T.S.;Chi, S.H.;Oh, S.K.
    • 한국전산유체공학회:학술대회논문집
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    • 2008.03b
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    • pp.492-495
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    • 2008
  • As the obesity patients increase recently, breath disease such an OSA(obstructive sleep apnea) is also increasing. When the breath disease occurs, the risk comes to be high. Dependence degree the PAP(positive airway pressure) is also coming to be high. The mechanical simulator is composed cylinder, valve, ball screw and the motor that they correspond to the lung and airway, the diaphragm of the human. In order to confirm the characteristic of the motor and the valve, it accomplished an test. The simulator traces breath pattern against the normal breath and the OSA.

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A Preliminary Study for the Development of Diagnostic X-ray Simulator using Visible Light Source (일반광원을 이용한 진단용 X선 모사 실험장치 개발을 위한 예비 연구)

  • 정광호;서태석;이형구;최보영;윤세철
    • Progress in Medical Physics
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    • v.13 no.3
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    • pp.169-175
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    • 2002
  • The purpose of this study is to verify the usefulness of X-ray simulator which uses a visible light source for further study. We developed a small experimental equipment which is composed of three main components - source, localizer and detector. Cartesian coordinate was set in 3D space, and the position of target was assumed the origin of the coordinate. The light from the source passes directly through the target, and projection image is formed on the screen, which can be taken with the digital camera. Since projection images were acquired behind the screen, they were flipped over right and left. By examining the characters of visual light source and equipments, it could be concluded that developed system was useful for experimental purpose.

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A study on the Development of a Driving Simulator for Reappearance of Vehicle Motion (I) (차량 주행 감각 재현을 위한 운전 시뮬레이터 개발에 관한 연구 (I))

  • Park, Min-Kyu;Lee, Min-Cheol;Son, Kwon;Yoo, Wan-Suk;Han, Myung-Chul;Lee, Jang-Myung
    • Journal of the Korean Society for Precision Engineering
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    • v.16 no.6
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    • pp.90-99
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    • 1999
  • A vehicle driving simulator is a virtual reality device which a human being feels as if the one drives a vehicle actually. The driving simulator is used effectively for studying interaction of a driver-vehicle and developing vehicle system of a new concept. The driving simulator consists of a vehicle motion bed system, motion controller, visual and audio system, vehicle dynamic analysis system, cockpit system, and etc. In it is paper, the main procedures to develop the driving simulator are classified by five parts. First, a motion bed system and a motion controller, which can track a reference trajectory, are developed. Secondly, a performance evaluation of the motion bed system for the driving simulator is carried out using LVDTs and accelerometers. Thirdly, a washout algorithm to realize a motion of an actual vehicle in the driving simulator is developed. The algorithm changes the motion space of a vehicle into the workspace of the driving simulator. Fourthly, a visual and audio system for feeling higher realization is developed. Finally, an integration system to communicate and monitor between sub systems is developed.

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Design of Small-Scale Simulator for Verification of Wind Turbine Conrol (풍력터빈 제어 검증용 축소형 시뮬레이터 설계)

  • Hwang, Jin-Su;Lee, Ho-Chul;Won, Seoung-Young;Chun, Sung-Gu;Lee, Byung-Chul;Ryu, Ji-Yune
    • 한국신재생에너지학회:학술대회논문집
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    • 2011.05a
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    • pp.55.1-55.1
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    • 2011
  • 풍력터빈에 적용되는 제어로직에 대한 검증을 실험실 기반에서 검증하기 위해서는 바람 및 터빈에 대한 적절한 모델링이 선행되어야 한다. 특히 피치 및 토크제어에 대한 특성을 검증하기 위해서는 블레이드 공력특성 및 터빈의 동특성에 대한 반영이 필연적이다. 본 논문에서는 풍력터빈 적용 제어로직 검증을 위하여 대상터빈에 대한 스케일링 결과, 바람을 모사하기 위한 구동장치 동작 및 터빈 모사장치에 대한 설계 결과에 대하여 소개하도록 한다.

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Development of Fuel Quantity Measurement System for Aircraft Supplementary Fuel Tank (항공기 보조연료탱크 연료량측정시스템 개발)

  • Yang, Junmo;Kim, Bonggyun;Hahn, Sunghyun;Lee, Sangchul
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.48 no.11
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    • pp.927-933
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    • 2020
  • This paper presents a fuel quantity measurement system (FQMS) for an aircraft supplementary fuel tank considering the change of aircraft attitude. The developed FQMS consists of fuel sensors, a signal process unit, an indicator and a software to estimate the fuel quantity from the sensor data. To replicate the change of the roll and pitch attitude on the ground, the test simulator is developed in this work. Using the test simulator, the sensor data at various fuel quantities, roll and pitch angles are automatically measured to build a training data set. The data-driven software to estimate the fuel quantity is then developed using a trilinear interpolation method with the training data set. The developed FQMS is verified by investigating the fuel estimation error of the test data set that we know the true values. Through the test, it is confirmed that the error of the developed FQMS system satisfies the criteria of TSO-C55 document.