• Title/Summary/Keyword: 축소형 시험설비

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Test Facility Improvement for Hot Firing Test of a 7-tonf Combustor in Sub-scale model (7톤급 연소기 축소형 모델 시험을 위한 설비 개량)

  • Kang, Dong-Hyuk;Lim, Byoung-Jik;Kim, Hyeon-Jun;Choi, Hwan-Seok
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2012.05a
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    • pp.498-501
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    • 2012
  • The Model Rocket Engine Test Facility has been improved to develop the Korea Space Launch Vehicle II(KSLV-II). The modified Model Rocket Engine Test Facility will be used to develop 7-tonf class liquid rocket engine combustor. The test result and test technique acquired from this facility will be used to develop the high performance liquid rocket engine combustor. This paper describes the modified Model Rocket Engine Test Facility for a Sub-scale model test of the 7-tonf class combustor.

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LOx/kerosene Sub-scale LRE Firing Test Facility (액체산소/케로신 소형로켓엔진 연소시험설비)

  • Kim Seung-Han;Lim Byoung-Jik;Han Yeoung-Min;Seol Woo-Seok;Lee Soo-Yong;Moon Il-Yoon
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2004.10a
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    • pp.166-169
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    • 2004
  • This paper describes the design, installation and certification activity of a combustion test facility of subscale thrust chambers propelled by pressure-fed liquid oxygen and kerosene, and suggests major key issues considered at each development stage of the facility

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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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A Study on the Nozzle Flow in the Sub-scale High-Altitude Test (축소형 고공환경모사 시험에서의 노즐 유동에 관한 연구)

  • Choi, Jiseon;Lee, Seongmin;Lee, Heejune;Ko, Youngsung;Kim, Seonjin;Lee, Jungmin
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2017.05a
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    • pp.1011-1015
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    • 2017
  • In this study, numerical and experimental studies on the nozzle flow in a sub-scale cold flow test were conducted to simulate high altitude condition. In the theoretical calculation, the temperature of the nozzle outlet is calculated to be lower than the liquefaction point, and the fluid exists at the phase change point. Also, numerical analysis result is higher than theory calculation but lower than liquefaction temperature. As a result of cold flow test, it was confirmed that the temperature was much higher than theory and analysis. This is because it assumed that it is adiabatic in the theoretical calculation, but the experiment in the actual environment is not the adiabatic but the heat exchange with the outside exists.

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Analyses of Hazard Voltages According to the Buried Depth of Small-sized Model Grounding Electrode (축소형 모델 접지전극의 매설깊이에 따른 위험전압의 분석)

  • Paek, Young-Hwan;Lee, Bok-Hee
    • Journal of the Korean Institute of Illuminating and Electrical Installation Engineers
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    • v.23 no.4
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    • pp.56-61
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    • 2009
  • This paper presents the ground surface potential profiles and hazard voltages around the metallic structure connected to a small-sized model ground electrode. Because it is very difficult to draw valid conclusions concerning a general grounding problem from actual field data, scale model tests can be used to determine the touch and stop voltages and surface potential profiles around ground electrode. In this work, a hemispherical vessel with a diameter of 1,100[mm] was employed to simulate uniform soil. As a result, the ground surface potential around the ground electrode was significantly raised In particular the ground surface potential at the just upper point of ground rod was higher than other points. When the buried depth of ground rod is increased, the ground surface potential and step voltage were lowered but the touch voltage was elevated.

A Miniature Inertia Simulator using Vector Controlled Induction Motor (벡터제어 유도전동기를 이용한 축소형 관성 시뮬레이터)

  • 김길동;박현준;한영재;한경희;조정민
    • The Transactions of the Korean Institute of Power Electronics
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    • v.7 no.1
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    • pp.74-80
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    • 2002
  • A propulsion system apparatus for railroad vehicle is estimated it's performance because of safety and confidence. In general, flywheel type testing method is widely used in the equipment. However, mechanical inertia generated by the flywheel can not be varied (or controlled) and can not be represent actual running resistance. In this study, we have focused on the development of variable vehicle load generation. Therefore, we have proposed the method which uses variable vehicle load controlled by vector motor to get the characteristics of the real vehicle load and confirmed the results with those of computer simulations.

A Running Stability Test of 1/5 Scaled Bogie using Small-Scaled Derailment Simulator (소형탈선시뮬레이터를 이용한 1/5 축소대차의 주행안정성 시험)

  • Eom, Beom-Gyu;Kang, Bu-Byoung;Lee, Hi-Sung
    • Journal of the Korean Society for Railway
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    • v.15 no.1
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    • pp.9-16
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    • 2012
  • The dynamic stability of railway vehicle has been one of the important issues in railway safety. The dynamic simulator has been used in the study about the dynamic stability of railway vehicle and wheel/rail interface optimization. Especially, a small scale simulator has been widely used in the fundamental study in the laboratory instead of full scale roller rig which is not cost effective and inconvenient to achieve diverse design parameters. But the technique for the design of the small scale simulator about the dynamic characteristics of the wheel-rail system and the bogie system has not been well developed in Korea. Therefore, the research using the small-scaled derailment simulator and the 1/5 scaled bogie has been conducted. In this paper, we did running stability test of 1/5 scaled bogie using small-scaled derailment simulator. Also, for the operation of the small scaled simulator, it is required to investigate the performance and characteristics of the simulator system. This could be achieved by a comparative study between an analysis and an experiment. This paper presented the analytical model which could be used for verifying the test results and understanding of the physical behavior of the dynamic system comprising the small- scaled derailment simulator and the 1/5 scaled bogie.

Seismic Analysis of the Reflective Metal Insulation for Thermal Shielding of Main Equipments of Nuclear Power Plants (원전 설비 열차폐를 위한 반사형 금속단열재의 내진 해석)

  • Kim, Seung-Hyeon;Rhee, Huinam
    • Journal of the Korea Academia-Industrial cooperation Society
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    • v.17 no.6
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    • pp.166-172
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    • 2016
  • This paper deals with the seismic qualification of the reflective metal insulation for thermal shielding that is installed on the outer surfaces of the main equipment of the primary coolant system of a nuclear power plant. A small-scale model of the reactor pressure vessel, which has equivalent dynamic characteristics, was designed to be tested in domestic seismic testing facilities in the future. In this study, seismic analysis of the small-scale model installed with metal insulation was performed using equivalent static analysis and response spectrum analysis. The required Response Spectrum for main equipment of the primary coolant system of APR-1400 plant were considered to establish the enveloping response spectrum, which was applied to the seismic analysis model. The results from two seismic analysis methods were compared to show the structural adequacy of the metal insulator design against a safe shutdown earthquake. This study will form the basis for the seismic testing to support the seismic qualification of the reflective metal insulator.

An Experimental Study of a Diffuser Starting Characteristics for Simulating High-Altitude Environment by using a Liquid Rocket (액체로켓엔진 연소기를 이용한 고고도 환경 모사용 디퓨저 시동특성 연구)

  • Lee, Yang-Suk;Jeon, Jun-Su;Ko, Young-Sung;Kim, Yoo;Kim, Sun-Jin
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.38 no.12
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    • pp.1195-1201
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    • 2010
  • Performance tests of a supersonic exhaust diffuser were conducted by using a liquid rocket engine for simulating high-altitude environment. The experimental setup consisted of a combustion chamber, a vacuum chamber and a diffuser. The combustion tests for simulating high-altitude environment were carried out at three cases by chamber pressure variation(26, 29, 32barg). The test results showed that the diffuser was started at all case and vacuum chamber pressures were approximately 140torr. The starting pressure using combustion gas was similar with that of cold gas, but the vacuum chamber pressure was relatively high because of high temperature in the vacuum chamber. The results of this test can be used as an essential database for the design of real-scale high-altitude simulation test facility in the future.

Implementation of IoT-based carbon-neutral modular smart greenhouse (IoT 기반 탄소중립 모듈형 스마트 온실 구현)

  • Seok-Keun Park;Kil-Su Han;Min-Soon Lee;Changsun Shin
    • Smart Media Journal
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    • v.12 no.5
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    • pp.36-45
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    • 2023
  • Recently, in digital agriculture, the types and utilization of greenhouses based on IoT are spreading, and greenhouses are being modernized, enlarged, and even factoryized using smart technology. However, a specific standardization plan has not been proposed according to the equipment for data collection in the smart greenhouse and the size or shape of the greenhouse. In other words, there is a lack of standard data for facility equipment, such as the type and number of sensors and equipment according to the size of the greenhouse, the type of greenhouse construction film and materials suitable for crops and carbon neutrality. Therefore, in this study, the suitability of the implementation, installation and quantity of IoT equipment for data collection was tested, and some standard technologies were presented through the implementation of data collection and communication methods. In addition, impact strength, tensile, tear, elongation, light transmittance, and lifespan issues for PE, PVC, and EVA, which account for about 90% of existing greenhouses, were presented, and the shape, size, and environmental problems of greenhouses made of films were presented. presented in the text. In this research paper, a standardized carbon-neutral modular smart greenhouse using nano-material film was implemented as a solution to environmental problems such as greenhouse size, farm crop type, greenhouse lifespan, and film, and its performance with existing greenhouses was analyzed and presented. Through this, we propose a modularized greenhouse that can be expanded or reduced freely without distinction in the size of the greenhouse or the shape of farmhouse crops, and the lifespan is extended and standardized. Finally, the average characteristics of greenhouses using existing PE, PVC, and EVA films and the characteristics of greenhouses using new carbon-neutral nanomaterials are compared and reviewed, and a plan to implement an expandable IoT greenhouse that supports carbon neutrality is proposed.