• 제목/요약/키워드: Engine test cell

검색결과 48건 처리시간 0.023초

친환경 자동차의 전자파 방사 노이즈 특성 분석 (Analysis of Electro-magnetic Interference Noise for Eco-friendly Vehicle)

  • 김해성;용부중
    • 한국자동차공학회논문집
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    • 제19권6호
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    • pp.76-81
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    • 2011
  • Fossil fuel, the energy source of internal combustion engine automobiles, is limited in resource and has caused environmental issues for decades. Accordingly, automobile manufacturers from many countries around the world are developing or producing eco-friendly vehicles that utilize alternative sources of energy. These vehicles are equipped with many electronic and electrical components which operate on high voltage and/or large current that were not used in conventional combustion engine automobiles. In this paper, in order to analyze the electro-magnetic interference noise, electric vehicles and fuel cell electric vehicles are tested under the guidelines of KMVSS (Korean Motor Vehicle Safety Standards) as well as under test modes that are not stipulated under the guidelines.

직렬형 하이브리드 굴절차량용 대용량 LPB 팩의 적용 및 성능 평가 (Performance Evaluation for Application of Large Capacity LPB Pack Equipped to Series Hybrid Articulated Vehicle)

  • 이강원;목재균
    • 한국전기전자재료학회논문지
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    • 제25권11호
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    • pp.930-937
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    • 2012
  • Newly developed Series hybrid low-floor articulated vehicle which can meet both road and railway running conditions. It has the rated driving speed of 80 km/h and three driving modes with hybrid(engine+battery) driving mode, engine driving mode, battery driving mode. The battery driving mode requires the several 10 km running without additional charging operation. The vehicle has been equipped with LPB (lithium polymer battery) pack for the series hybrid propulsion system. LPB pack consists of 168 cells (3.7 V in a cell, 80 Ah) in series, DC Circuit breaker, mechanical rack, BMS (battery management system). This paper has shown the design process of LPB pack and application to the vehicle. Driving results in the road was successful to be satisfied with the requirement of the series hybrid vehicle.

Ni-MH 전지전원의 모델링과 충.방전 장치 개발 (Modeling of The Ni-MH Battery Source and Development of The Charger.Discharger System)

  • 김광헌;허민호;박영수;안재영;양승학;이일기
    • 전력전자학회:학술대회논문집
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    • 전력전자학회 1998년도 전력전자학술대회 논문집
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    • pp.433-437
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    • 1998
  • Equalize SOC of the cell which effect on the charge.discharge ability and the efficiency of the battery, through the charge.discharge characteristic test of the battery source, and develope the high efficiency charge.discharge system in the series HEV have a constant engine-generator output. For this, in this paper, establish the electrical model and the condition of high efficiency charge.discharge, and proposed the improvement method of charge.discharge characteristic in the battery source that consist of twenty Ni-MH cells connected serial/parallel

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선박엔진의 실린더 라이너의 손상 진단을 위한 진동 분석법 (Vibration Analysis for Failure Diagnosis of Cylinder Liner of Large Ship Engine)

  • 구현호;조연상;박준홍;박흥식
    • Tribology and Lubricants
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    • 제30권1호
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    • pp.21-28
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    • 2014
  • Damage to the cylinder liner of large ship engines, such as scuffing on the surface, can occur very easily because it is operated in a corrosive environment. This scuffing may be due to oil film destruction and corrosive wear caused by water and sulfur included in the fuel, abrasive impurities, and poor lubricants. Thus, a method for monitoring the condition and diagnosing the failure of the cylinder liner and piston ring is needed. In this study, a reciprocating friction and wear test was carried out with a cast iron specimen, which simulated an engine cylinder in a corrosive atmosphere. The lubricants used were base oil, stirred oil with distilled water, a NaCl solution, and dilute sulfuric acid. The friction coefficient and frequency spectrum were measured using a load cell and acceleration sense in each experimental condition. We then used these results to diagnose the failure of the cylinder liner.

회전익항공기용 연료셀 피탄 수치모사 연구 (Numerical Simulation of Bullet Impact for Fuel Cell of Rotorcraft)

  • 김현기;김성찬
    • 한국전산구조공학회논문집
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    • 제25권5호
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    • pp.405-411
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    • 2012
  • 회전익항공기의 연료셀 내부는 연료보관 및 연료를 엔진으로 공급하기 위한 배관과 구성품들이 배치되어 있다. 특히, 기동헬기는 전장에서 사용되는 헬기로써, 수 km 고도에서 비행하는 고정익기보다 비행고도가 낮기 때문에 피탄될 가능성이 높다. 따라서, 항공기의 생존성을 극대화하기 위해서는 피탄시 유체내부 상승압력에 의한 내부 구성품들이 받는 영향성을 검토하여 설계되어야 함은 주지의 사실이다. 그러나 내탄시험은 연료셀 자체의 제작비용 및 준비기간이 상당히 소요되고, 실탄 사용에 따른 시험수행의 제약 때문에 수치모사를 통한 관련 데이터의 확보가 필요하다. 이를 위해 본 연구에서는 유체-구조 수치모사 프로그램인 Autodyn을 이용하여 회전익항공기 연료셀의 내탄 수치모사를 수행하여, 피탄 후 연료셀 내부에서의 탄 거동을 분석하고 유체내부의 압력과 연료 셀 자체의 등가응력을 평가하였다.

Development of the Dynamometer Control System for Medium Speed Diesel Engines

  • Choi, Sang-Gu;Ryu, Sang-Hun;Kim, Jeom-Goo;Park, Ho-Chol
    • 제어로봇시스템학회:학술대회논문집
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    • 제어로봇시스템학회 2004년도 ICCAS
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    • pp.243-247
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    • 2004
  • The dynamometers which had made in a long time ago could not control the input/output quantity of water minutely and was sensitive to a noise since it was controlled by an analog control method. Therefore, a fully digital controlled system was urgently required to be robust against various noises. In this paper, the new system which can control the amount of circulated water in dynamometer was developed. This system is consisted of an industrial digital type controller and a servo motor. The industrial PLC was used as a main controller for the developed system, and the actuator and servo motor were used to control the inlet and outlet valve independently. The torque signal of load cell was fed back to the main controller to regulate the diesel engines load. Generally, an input/output valve position of the old dynamometer was fixed with a proper situation for an engine output test and the torque was changed according to the time interval. However, the torque value for the dynamometer could not be constantly kept because of the variation of the input water flow and fluid characteristic. Therefore, the automatic control of an inlet and outlet valve should be performed to keep the constant torque. So, the PID control method was applied to solve this problem. Also, the development of a web-based remote control system was described in this paper. This software will give us the convenience of operation, the more efficient operations, and the reduced operator workload for operation of the dynamometer. The application results of the system have been verified at actual diesel engine field.

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유류분해 미생물의 특성 및 제제화 가능성 평가

  • 윤정기;김태승;노회정;김혁;박종겸;고성환
    • 한국지하수토양환경학회:학술대회논문집
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    • 한국지하수토양환경학회 2004년도 총회 및 춘계학술발표회
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    • pp.297-300
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    • 2004
  • The various microbial tests were performed to determine bioremediation agent capacity for eight strains isolated from the oil contaminated regions. Two tests for isolated strains were conducted such as cell hydrophobicity and emulsifying activity. The biodegradation of SHM (saturated hydrocarbon mixture) and AHM (aromatic hydrocarbon mixture) with the strains also was carried out. The strains having higher cell hydrophobicity and emulsifying activity degraded petroleum oil effectively. The degradation capacity for SHM was represented more than 90% in YS-7 and WLH-1 of isolated strains, and KH3-2 were capable of degrading AHM. Especially, WLH-1 as yeast was shown more than two or three times in the degradation capacity of automobile engine lubricants and the biomonitoring results of contaminated soil for residual oil degrading test showed that the hydrocarbon biodegradation was increased in the second treatment by this strain.

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Thrust - Performance Test of Ethylene-Oxygen Single-Tube Pulse Detonation Rocket

  • Hirano, Masao;Kasahara, Jiro;Matsuo, Akiko;Endo, Takuma;Murakami, Masahide
    • 한국추진공학회:학술대회논문집
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    • 한국추진공학회 2004년도 제22회 춘계학술대회논문집
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    • pp.205-210
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    • 2004
  • The pulse detonation engine (PDE) has recently expected as a new aerospace propulsion system. The PDE system has high thermal efficiency because of its constant-volume combustion and its simple tube structure. We measured thrust of single-tube pulse detonation rocket (PDR) by two methods using the PDR-Engineering Model (full scale model) for ground testing. The first involved measuring the displacement of the PDR-EM by laser displacement meter, and the second involved measuring the time-averaged thrust by combining a load cell and a spring-damper system. From these two measurements, we obtained 130.1 N of time-averaged thrust, which corresponds to 321.2 sec of effective specific impulse (ISP). As well, we measured the heat flux in the wall of PDE tubes. The heat flux was approximately 400 ㎾/$m^2$. We constructed the PDR-Flight Mode] (PDR-FM). In the vertical flight test in a laboratory, the PDR-FM was flying and keeping its altitude almost constant during 0.3 sec.

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소형 액체 추진기관 연소 시험을 위한 추력 측정 장치의 성능 특성 연구 (Performance Characteristics of Thrust Measurement System for Hot-Firing Test of Small Liquid Propulsion Engines)

  • 김인태;허환일;김정수;장기원;이재원
    • 한국항공우주학회지
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    • 제32권9호
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    • pp.122-129
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    • 2004
  • 소형 액체 엔진의 개발을 위한 과정에는 정확한 추력 측정이 성공적인 시험 및 평가를 위해 필수적이다. 본 논문에서는 추력 측정 장치의 개발을 위해 고려해야 할 설계 요소 및 제작 과정 동을 살펴본다. 측정 장치의 특정들이 기술되고 진공 환경을 모사한 연소 시험을 통해서 그 성능을 평가하였다. 측정 장치의 성능 시험을 위해 추진제 주입 압력의 변화에 따라 정상모드와 펄스모드에서 연소 시험을 수행하였으며 고유 진동수 및 구조물 의 선형성 시험과 같은 특성 시험을 통해 소형 액체 엔진의 정확한 추력 측정을 위한 적합성을 확인하였다.