• 제목/요약/키워드: Test Facility

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75톤급 액체로켓엔진용 가스발생기 후연소 시험설비 인증시험 결과 (Certification Test Result of After-burner Test Facility for Gas-generator of 75 tonf Class Liquid Rocket Engine)

  • 김채형;이광진;한영민;정용갑
    • 한국추진공학회지
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    • 제19권5호
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    • pp.91-97
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    • 2015
  • 75톤급 액체로켓엔진용 가스발생기 후연소 시스템 설비를 제작하였으며, 연소기 연소시험설비 시험장에서의 설비인증 시험을 통해 그 성능을 확인하였다. 후연소 설비인증 시험은 메탄과 산소의 공급성능, 가스발생기와 후연소 설비에 설치된 가스토치의 안정적인 연소 능력을 검증하는데 있다. 단독성능 시험에서 공급시스템은 감압 없이 일정한 압력으로 메탄과 산소를 공급했으며, 가스 토치 압력은 설계조건을 만족하였다. 가스발생기 점화용 가스토치와의 연계시험에서 가스발생기 점화 성능과 연료과농 배기가스의 후연소 성능에 관한 인증 시험을 성공적으로 수행하였다.

소형 축류터빈의 상온 성능시험기 개발 (Development of a Test Facility for Cold-air Performance of Small Axial Turbine)

  • 손창민;차봉준;이대성
    • 대한기계학회논문집
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    • 제19권7호
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    • pp.1780-1786
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    • 1995
  • The main goal of the present study is to establish the techniques and methodolgies of turbine performance test through evaluating the objective turbine test piece, and checking the reliability of the self-developed test facility by performing a series of turbine tests under ambient temperature condition. A high speed coupling, a lubrication system and a test bed of the test facility were modified through a series of preliminary test in order to reduce the vibration and oil leakage. The flowrate control of the test facility and data acquisition were accomplished by using a software called "Labview" The measurement of shaft horse power and control of rotational speed according to the conditions of turbine rotation were performed by a separate system. The preliminary evaluation of the measured data suggests that the developed test facility and the test technique can be used reliably for the performance test of turbines with the minor improvement.provement.

핵연료집합체 기계적특성 시험시설 구축과 기능시험 (Construction and Functional Tests of Fuel Assembly Mechanical Characterization Test Facility)

  • 이강희;강흥석;윤경호;양재호
    • 한국압력기기공학회 논문집
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    • 제12권1호
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    • pp.11-16
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    • 2016
  • Fuel assembly's mechanical characterization test facility (FAMeCT) in KAERI was constructed with upgraded functional features such as increased loading capacity, underwater vibration testing and severe earthquake simulation for extended fuel design guideline. This facility is designed and developed to provide out-pile fuel data for accident analysis model and fuel licensing. Functional tests of FAMeCT were performed to confirm functionality, structural integrity, and validity of newly-built fuel assembly mechanical test facility. Test program includes signal check of data acquisition system, load delivering capacity using real-sized fuel assemblies and a standard loading cylindrical rigid specimen. Fuel assembly's lateral bending test was carried out up to 30 mm of pull-out displacement. Limit case axial compression loading test up to 33 kN was performed to check structural integrity of UCPS (Upper Core Plate Simulator) support frame. Test results show that all test equipment and measurement system have acceptable range of alignment, signal to noise ratio, load carrying capacity limit without loss of integrity. This paper introduces newly constructed fuel assembly's mechanical test facility and summarizes results of functional test for the mechanical test equipment and data acquisition system.

액체로켓엔진 연소시험설비 예비설계 (Preliminary Design of Liquid Rocket Engine Test Facility)

  • 김승한;한영민
    • 한국추진공학회:학술대회논문집
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    • 한국추진공학회 2011년도 제37회 추계학술대회논문집
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    • pp.885-891
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    • 2011
  • 본 논문은 액체산소와 케로신을 추진제로 하는 액체로켓엔진의 성능평가를 위한 엔진 지상 연소시험설비 예비설계 결과를 기술하였다. 엔진 지상 연소시험설비의 설계 요구조건에 기반한 설계 규격 및 설비 구성을 제시하였다. 엔진 지상 연소시험설비 예비설계 결과는 향후 한국형발사체 75톤급 엔진 지상 연소시험설비의 상세설계 및 구축을 위한 기본 자료로 활용될 예정이다.

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한국형발사체 엔진 지상 연소시험설비 개발 (Development of Liquid Rocket Engine Test Facility)

  • 김승한;정용갑;한영민
    • 한국추진공학회:학술대회논문집
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    • 한국추진공학회 2012년도 제38회 춘계학술대회논문집
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    • pp.479-483
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    • 2012
  • 본 논문은 액체산소와 케로신을 추진제로 하는 한국형발사체 1단 엔진의 성능평가를 위한 엔진 지상연소시험설비 개발 현황을 기술하였다. 한국형발사체 75톤급 엔진 지상 연소시험설비의 설계 요구조건에 기반한 설계 규격 및 설비 구성을 제시하였다. 엔진 지상 연소시험설비 기본설계 결과는 향후 한국형발사체 75톤급 엔진 지상 연소시험설비의 상세설계 및 구축을 위한 기본 자료로 활용될 예정이다.

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터보펌프 Cavitation 성능시험기 개발 및 성능시험에 관한 연구 (Development of Turbopump Cavitation Performance Test Facility and the Test of Inducer Performance)

  • 손동기;김춘택;윤민수;차봉준;김진한;양수석
    • 대한기계학회:학술대회논문집
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    • 대한기계학회 2001년도 춘계학술대회논문집E
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    • pp.619-624
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    • 2001
  • A performance test facility for turbopump inducer cavitation was developed and the inducer cavitation performance tests were performed. Major components of the performance test facility are driving unit, test section, piping, water tank, and data acquisition and control system. The maximum of testing capability of this facility are as follows: flow rate - 30kg/s; pressure - 13 bar; rotational speed 10,000rpm. This cavitation test facility is characterized by the booster pump installed at the outlet of the pump that extends the flow rate range, and by the pressure control system that makes the line pressure down to vapor pressure. The vacuum pump is used for removing the dissolved air in the water as well as the line pressure. Performance tests were carried out and preliminary data of test model inducer were obtained. The cavitation performance test and cavitation bubble flow visualization were also made. This facility is originally designed for turbopump inducer performance test and cavitation test. However it can be applied to the pump impeller performance test in the future with little modification.

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직경 2m급 축소로터 시험장치 개조 및 보완 (Modification of Dia. 2m-Small-scaled Rotor Test Facility)

  • 송근웅;이재하;김승호
    • 한국소음진동공학회:학술대회논문집
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    • 한국소음진동공학회 2012년도 추계학술대회 논문집
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    • pp.190-195
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    • 2012
  • Small-scaled Rotor Test facility(GSRTS, General Small-scaled Rotor Test Facility) in KARI could not use the test because facility aging and parts discontinued. Also in order to perform a joint international research, GSRTS modifications should be needed. So requirements of GSRTS modifications were established and according to the requirements, GSRTS modifications were conducted. Facility operation test, 6-component fixed balance calibration, Small-scaled OLS rotor performance test were performed to verify the results of GSRTS modifications. Reasonable results were obtained in comparison to calculation results. Then GSRTS ready was completed to conduct international collaborative research and wind tunnel test.

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액체로켓엔진 성능 및 냉각특성 연구를 위한 연소시험장치 개발 (Development of Combustion Test Facility for Liquid Rocket Engine)

  • 김동환;이성웅;유병일
    • 한국항공우주학회지
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    • 제34권2호
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    • pp.106-111
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    • 2006
  • 액체로켓엔진의 성능 및 냉각특성 연구를 위한 연소시험장치를 개발하였다. 본 시험장치는 액체산소와 kerosene을 추진제로 사용하는 추력 1.0 KN 이하의 액체로켓엔진의 성능 및 냉각 특성연구가 가능하며, 실제 연소시험을 통해 정상적인 작동을 확인하였다. 향후 액화천연가스와 천연가스를 사용하는 로켓엔진의 시험 및 재생냉각시험이 가능토록 설비 개량을 실시할 예정이다

수위계 표준시험장치 개발 및 최고측정능력에 관한 연구 (Best Measurement Capability and Standard Test Facility for the Water-level Gauges)

  • 신강욱;홍성택
    • 제어로봇시스템학회논문지
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    • 제13권10호
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    • pp.1012-1017
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    • 2007
  • Rain data and water-level data are importantly used for dam operation at flood period. Because dams are directly controlled by the water-level data, the characteristic of the water-level gauges is necessary to be managed. Thus, we developed the standard test facility and method for testing the water-level gauges which are a float type, a supersonic type and a radar type. And we calculated the uncertainty of the standard test facility to maintain the accuracy of water-level gauges. Through development of this facility, we could obtain the characteristics and the calibration factor of the water-level gauges. And, this study showed that the standard test facility can be widely used for dam operation and basin management.