• Title/Summary/Keyword: Engine test

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교육용 마이크로 가스터빈 엔진 성능 시험장치 개발 (Development of the Educational Micro Gas Turbine Engine Performance Test System)

  • 고성희;기자영;박미영;공창덕;이경재
    • 한국추진공학회:학술대회논문집
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    • 한국추진공학회 2008년도 제31회 추계학술대회논문집
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    • pp.31-35
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    • 2008
  • 본 시험장치는 가스터빈 관련 교육기관, 연구소 등에 가스터빈 엔진의 작동 원리와 구조에 대한 기초지식을 제공하고 가스터빈 엔진의 이론적 열역학 계산을 실제 성능시험을 통하여 비교해 볼 수 있도록 개발되었다. 추력 30lbf급 마이크로 터보제트 엔진을 대상으로 하여 NI DAQ(데이터 수집)장치와 LabVIEW 프로그램으로 각 구성품의 온도, 압력과 추력, 연료유량, 공기유량 등의 실시간 데이터를 모니터링 및 획득할 수 있도록 시험장치를 구성하였다.

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KSR-III 엔진 축소형 모델 연소 특성(I) (The Combustion Characteristics of a Subscale Engine of KSRIII(I))

  • 김영한;김용욱;고영성;이수용;류철성;설우석
    • 대한기계학회:학술대회논문집
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    • 대한기계학회 2001년도 춘계학술대회논문집D
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    • pp.846-851
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    • 2001
  • For the successful development of the main engine of KSR(Korea Sounding Rocket)-III, Korea Aerospace Research Institute(KARI) carried out the experimental study on the subscale model engines. Several types of engines were tested on the Small Liquid Rocket Engine Test Facility. One of the typical test results of a Sub. engine(Sub. Mod.3) is presented here. It uses the Jet A-1 as fuel, liquid oxygen as oxidizer, and Tri-Ethyl Aluminium(TEA1) as ignition agent. The gas pressure feed system is adopted as a feeding mechanism and the design chamber pressure is 200psia. The physical phenomena are described in three regimes(ignition, transient, and steady state) with the pressure, thrust, flowrate and image data. And the pressure oscillation is analyzed in Fourier domain (<500Hz). Then we conclude that in this experiment, the engine shows the characteristic low frequency of 80Hz and it is stable for that frequency of pressure oscillation.

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소형 트럭용 CNG/가솔린 겸용 엔진 개발과 성능 분석 (Development of CNG/Gasoline Bi-fuel engine for a small truck and the evaluation of engine performance)

  • 권오운;김재수;박용국;김성준
    • 산업기술연구
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    • 제26권B호
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    • pp.21-28
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    • 2006
  • A diesel truck of 1 ton is re-powered by a gasoline engine and the fuelling system of gasoline engine modified to gasoline/CNG bi fuel system. The engine characteristics such as fuel economy and power are evaluated by driving rest, sloping test and dynamometer. The driving test prove the driving cost is saved by 55% and the maximum speed is raised by 13%, which is mainly due to the higher calorific value of CNG. The sloping test is done on the road of which slope is 15%. The truck shows the mean velocity of 88km/h, which means that a re-powered truck is working fine. The BHP are measured by dynamometer. The power and torque produced by a re-powered truck are reduced by 13% and 14% respectively from the power of gasoline engine. The BHP reduction is one of main problems which one has to solve in near future.

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마이크로컴퓨터를 이용한 엔진성능시험(性能試驗)의 자동화(自動化)에 관한 연구(硏究)(I) -엔진성능시험(性能試驗)과 데이터수집(蒐集)의 자동화(自動化)- (A Microcomputer-Based Data Acquisition/Control System for Engine Performance Test(I) -Automation of Engine Performance Test and Data Acquisition-)

  • 류관희;정창주;박보순
    • Journal of Biosystems Engineering
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    • 제12권3호
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    • pp.7-16
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    • 1987
  • This study was carried out to develop a microcomputer-based data acquisition and control system which was able to collect the data of engine performance test automatically and control the speed and load of the engine. The results of the study are summarized as follows: 1. The signal processing devices, which were able to measure cylinder pressure, coolant temperature, compositions of exhaust gas, fuel consumption, engine rpm and torque etc., were developed. The results of calibration showed that all of devices had high accuracy ranging from 0.3% to 0.69% respectively. 2. The PIA (peripheral interface adapter) for interfacing digital signal and PTM (programmable timer module) for displaying real time every 0.0408 sec were designed and developed. 3. An engine-speed control system using a stepping motor and driver was developed. The control system had the stability, and faster settling time than the manual control system. 4. The automatic control system of electrical dynamometer, which was able to control the speed and load of dynamometer, was developed with a SSD (shackleton system driver) and D/A converter. 5. The computer programs, which were able to collect and process the data of engine tests, were developed using both the machine language and BASIC.

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트랙터의 기관속도(機關速度) 및 변속비(變速比)의 자동제어(自動制御)에 관(關)한 연구(硏究)(I) -기관속도(機關速度) 및 변속비(變速比) 제어(制御) 시스템- (Automatic Control of Engine Speed and Transmission Ratio for Efficient Tractor Operations(I) -Control Systems for Engine Speed and Transmission Ratio-)

  • 강성봉;류관희;오길근
    • Journal of Biosystems Engineering
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    • 제18권4호
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    • pp.305-316
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    • 1993
  • Fuel efficiency in tractor operations dep6nds on the selection of transmission gears and upon the engine being operated at or near maximum torque much of time. The objective of this study was to develop automatic control systems for tractor transmission ratio and governor setting so that the engine is operated at or near maximum torque as much of time as possible. An indoor test unit, which can be used to simulate tractor operation, was built in order to investigate the system design parameters and test the performance of the control system designed. The test-unit consists of engine, gear-type transmission, dynamometer, and control systems for transmission ratio and engine speed. Governor setting lever was controlled by a step motor, and the clutch and transmission levers were controlled by hydraulic cylinders and solenoid valves. The control systems showed good time responses which are assumed to be suitable for optimal tractor operation. The time required for shifting gears from clutch disengagement to engagement was about 1 second, which is almost the same as that for manual shift. And the settling time for engine speed control system was about 5 to 6 seconds.

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다단연소사이클 엔진의 터보펌프 및 유공압 라인 특성 (Characteristics of Turbopump and Hydraulic lines of Staged Combustion Cycle Engine)

  • 이정호;전준수;황창환;우성필;이광진;유병일;한영민
    • 한국추진공학회:학술대회논문집
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    • 한국추진공학회 2017년도 제48회 춘계학술대회논문집
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    • pp.94-98
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    • 2017
  • 고성능 상단엔진 개발을 위한 9톤급 다단연소사이클 엔진의 선행연구가 진행 중에 있다. 다단연소사이클 엔진 기술검증시제(TDM0)를 제작을 완료하여, 나로우주센터 엔진 연소시험설비에서 예연소기와 터보펌프로 구성된 파워팩 연소시험과 주 연소기까지 장착된 엔진 연소시험을 차례로 수행하였다. 다단연소사이클 엔진 유공압 라인의 진공화 과정과 연소시험에서 나타난 터보펌프의 및 유공압 라인의 특성을 간략히 기술한다.

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저급 혼합연료유 연소시험 결과 (The Test Result of the Blended Oil Combustion in the Engine having used Marine Gas Oil)

  • 이기동;강대선
    • 선박안전
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    • 통권23호
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    • pp.37-50
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    • 2007
  • The test result is a part of a study on the reduction of fuel expense. the test was conducted in the ship of east sea fisheries supervision office which is modified from 139 ton trawler to 183 ton petrol ship. The result of NOx emission and Smoke Value for main engine and generator engine are measure and included in this paper. The information on pre-treatment systems and measuring equipment also includes.

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Development of Operating Program for EECU Test Bench

  • Kang, Myoungcheol;Kho, Seonghee;Ki, Jayoung
    • International Journal of Aerospace System Engineering
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    • 제1권1호
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    • pp.10-15
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    • 2014
  • This study presents technical description of the operating program development that operates the test bench for functional test of EECU. The test bench is capable of testing, simulation and adjustment of the EECU software using the operating program. The test bench is for the Development Project of the EECU platform for FADEC system. The operating program is consists of 3 modules which are the test bench operating module, cockpit simulator module and SILS module. The operating module mainly carries out the EECU test with manual operation and operating scenarios. Also that record and process the test data. The cockpit simulator module is capable of implementation of virtual cockpit control input and engine status display. The SILS module can simulate engine and EECU operation in software environment.

15만 파운드급 테스트 셀을 이용한 엔진성능 시험기술 (Aircraft Engine Performance Test Technologies by 150K lbf Thrust Test Cell)

  • 김우철;김철;김상백
    • 한국추진공학회:학술대회논문집
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    • 한국추진공학회 2017년도 제48회 춘계학술대회논문집
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    • pp.180-187
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    • 2017
  • 항공기 엔진 지상 성능시험을 위한 15만 파운드 급 Test 설비를 구축하기 위해 Test Cell Type, Cell Flow, Cell Bypass Ratio, Approach Velocity, Cell Depression, Front Cell Distortion, Noise 및 Vibration 등의 주요 설계 목표를 설정 하였고, 설비 완공 후 최종 성능검사를 통해 목표 값을 충족하는 성능 데이터를 획득할 수 있었다.

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스크램제트 엔진 흡입구 시험을 위한 자유제트형 지상추진시험설비의 마하 5 성능 검증 (Mach 5 Performance Verification of Free-jet Type Ground Propulsion Test Facility for Scramjet Engine Intake Test)

  • 이양지;양인영;이경재;오중환;최진
    • 한국추진공학회지
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    • 제26권1호
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    • pp.77-87
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    • 2022
  • 한국항공우주연구원 스크램제트 엔진 시험설비를 활용한 스크램제트 엔진 흡입구 지상 시험을 수행하기 위하여 일반적으로 진행하는 시험 가능 여부 확인 절차를 소개하였다. 스크램제트 흡입구 시험을 수행하기 위하여 새롭게 제작된 마하 5 노즐의 설계 과정을 정리하였으며, 노즐의 코어 유동 분포를 확인하기 위한 장치를 설명하고 코어 유동 시험 분석 결과를 기록하였다. 일련의 시험 결과를 통하여 흡입구가 신규 마하 5 노즐 코어에 위치하는 것을 확인하였다.