• 제목/요약/키워드: Engine Fault

검색결과 142건 처리시간 0.024초

공작기계용 원격 고장진단 및 보수 시스템 (Remote Fault Diagnosis and Maintenance System for NC Machine Tools)

  • 신동수;현웅근;정성종
    • 한국정밀공학회지
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    • 제15권1호
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    • pp.19-25
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    • 1998
  • Remote fault diagnosis and maintenance system using general telecommunication network is necessary for an effective fault diagnosis and higher productivity of NC machine tools. In order to monitor machine tool condition and diagnose alarm states due to electrical and mechanical faults, a remote data communication system for monitoring of NC machine fault diagnosis and status is developed. The developed system consists of (1) remote communication module among NC's and host PC using PSTN. (2) 8 channels analog data sensing module, (3) digital I/O module for control or NC machine, (4) communication module between NC machine and remote data communication system via RS-232C, and (5) software man-machine interface. Diagnostic monitoring results generated through a successive type inference engine are displayed in user-friendly graphics. The validity and reliability of the developed system is verified to be a powerful commercial version on a vertical machining center through a series of experiments.

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BLDCM 구동 인버터의 실시간 데이터를 이용한 고장진단 (Fault Diagnosis based on Real-Time Data of the inverter system for BLDCM drive)

  • 김광헌;배동관
    • 조명전기설비학회논문지
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    • 제12권2호
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    • pp.29-37
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    • 1998
  • 이 논문은 브리시리스 직류전동기의 구동 인버터의 실시간 데이터를 이용한 고장진단에 관한 것이다. 구동 인버터의 고장유형을 파악하여 주요 고장증세별로 분류하고, 고장결과를 예측하여 ASCL로 시뮬레이션함으로써 지식 베이스로 구성하였다. 구동 인버터에 대해 실시간으로 감시된 데이터는 전문가 시스템의 추론기관에서 시뮬레이션된 지식베이스와 비교하게 된다. 고장이 발생하면, 운전을 중지시킨 후, 전문가 추론을 함으로써 고장원인을 진단한다. 이로써 구동 인버터에 대해 전문적인 지식을 갖고 있지 않는 사용자에게, 고장원인 제거 및 수리대책에 관한 전문가의 지식을 신속히 제공하는 것이다.

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Design of Fault Diagnosis Expert System Using Improved Fuzzy Cognitive Maps and Rough Set Based Rule Minimization

  • 이종필;변증남
    • 한국지능시스템학회:학술대회논문집
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    • 한국퍼지및지능시스템학회 1997년도 추계학술대회 학술발표 논문집
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    • pp.315-320
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    • 1997
  • Rule minimization technique adapted from rough set theory was applied to remove redundant knowledge which is not necessary to make a knowledge base. New algorithm to diagnose fault using Improved Fuzzy Cognitive Maps(I-FCMs), and Fuzzy Associative Memory(FAM) is proposed. I-FCM[22] is superior to gathering knowledge from many experts and descries dynamic behaviors of systems very well. I-FCM is not only a knowledge base, but also a inference engine. FAM has learning capability like neural network[12]. Rule minimization and composition of I-FCM and FAM make it possible to construct compact knowledge base and breaks the border between inference engine and knowledge base.

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Demagnetization Diagnosis of Permanent Magnet Synchronous Motor Using Frequency Analysis at Standstill Condition

  • Yoo, Jin-Hyung;Jung, Tae-Uk
    • Journal of Magnetics
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    • 제21권2호
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    • pp.249-254
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    • 2016
  • Recently, electric vehicles have got significant attention because it is more eco-friendly and efficient than internal combustion engine vehicles. Instead of an internal combustion engine, the electric vehicle has a motor for propulsion. The permanent magnet synchronous motor which has permanent magnet instead of field winding in the rotor has especially higher efficiency and power density than other types of motor. When the irreversible demagnetization is occurred, drivers are exposed to high risk of accident by the fault operation of motor. Therefore, the irreversible demagnetization of permanent magnet should be detected to reduce the risk of accident. In this study, the demagnetization diagnosis method based on the result of locked rotor test is proposed. Based on short measurement time, the proposed diagnosis method aims to detect the demagnetization fault when an electric vehicle is at a complete standstill. The proposed method is verified through the finite element analysis.

브레이크 스위치 결함에 의한 간헐적인 가속불량 현상의 고장진단 사례연구 (Case Study of Intermittent Poor Acceleration Fault Diagnosis by Brake Switch Fault)

  • 김성모;조행득
    • 한국생산제조학회지
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    • 제24권2호
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    • pp.203-210
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    • 2015
  • This paper investigates the failure of a car with a 2.5-liter CRDi engine of the Hyundai Company. The failure is caused by intermittent poor acceleration while driving. To analyze the cause, we investigated the air intake volume, the fuel injection, and the air-fuel ratio, which were determined to be normal. The brake switch signal error was discovered while analyzing the function that limits the output of the engine. While investigating the cause, we discovered the corrosion of the pins on the connector of the brake switch. We determined that it was generated by soapy water flowing in the solar film. Therefore, the cause of the failure was the brake switch signal errors. Additionally, we determined that ECM was the normal fail-safe mode that implemented the override device for safety during normal acceleration. Based on these results, further solar film experiments must be conducted to fully elucidate the causes.

신경망을 이용한 터보제트 엔진의 고장 진단 (Sensor Fault Detection and Isolation of a Turbojet Engine Using Neural Network)

  • 김종선;이강웅;김진곤;부준홍;유상신;민성기
    • 한국항행학회논문지
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    • 제3권1호
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    • pp.32-43
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    • 1999
  • 본 논문에서는 터보제트 엔진 제어기의 신뢰성을 향상시키기 위한 지능형 고장진단 알고리즘을 제안하였다. 제안된 기법은 다층 신경망을 이용한 고장진단 기법으로 서로 다른 종류의 센서를 사이의 기능적 종속관계를 추정하여 고장 부위를 규명하고 처치한다. 고장센서 신호는 역전파 알고리즘을 이용한 훈련된 신경망을 통하여 추정한다. 실험데이터에 기초한 터보제트 엔진의 선형공간 모델에 적용한 시뮬레이션을 통하여 제안된 알고리즘의 구현 가능성을 검증한다.

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항공기용 가스터빈 엔진의 건전성 관리를 위한 소프트웨어 발전 동향 (A Survey on the Software Technology of Health Management System for Aircraft Gas Turbine Engine)

  • 박익수;기태석;김중회;민성기
    • 한국추진공학회지
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    • 제22권5호
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    • pp.13-21
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    • 2018
  • 항공기용 엔진의 건전성 관리를 위한 탑재장비 및 지상 장비 소프트웨어의 발전 동향을 살펴보았다. 과거에는 지상 장비 중심의 결함 검출 및 식별기법에서 탑재 소프트웨어를 이용한 모델 기반의 건전성 식별 기법으로 변화해 왔고, 현재는 지상과 탑재장비 소프트웨어의 통합된 구조로 발전해 가고 있다. 이러한 진보된 기법이 선진국을 중심으로 기술발전을 이루어 가고 있음에 비해 국내의 연구는 초보적인 수준에 머물러 있다. 본 논문에서는 국내외 기술개발 현황을 고려하여 최적의 발전 방향을 제시하였다.

An Improved Hybrid Kalman Filter Design for Aircraft Engine based on a Velocity-Based LPV Framework

  • Liu, Xiaofeng
    • International Journal of Aeronautical and Space Sciences
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    • 제18권3호
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    • pp.535-544
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    • 2017
  • In-flight aircraft engine performance estimation is one of the key techniques for advanced intelligent engine control and in-flight fault detection, isolation and accommodation. This paper detailed the current performance degradation estimation methods, and an improved hybrid Kalman filter via velocity-based LPV (VLPV) framework for these needs is proposed in this paper. Composed of a nonlinear on-board model (NOBM) and VLPV, the filter shows a hybrid architecture. The outputs of NOBM are used for the baseline of the VLPV Kalman filter, while the system performance degradation factors on-line estimated by the measured real system output deviations are fed back to the NOBM for its updating. In addition, the setting of the process and measurement noise covariance matrices' values are also discussed. By applying it to a commercial turbofan engine, simulation results show the efficiency.

Sensor Fault Detection of Small Turboshaft Engine for Helicopter

  • Seong, Sang-Man;Rhee, Ihn-Seok;Ryu, Hyeok
    • 한국추진공학회:학술대회논문집
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    • 한국추진공학회 2008년 영문 학술대회
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    • pp.97-104
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    • 2008
  • Most of engine control systems for helicopter turboshaft engines are equipped with dual sensors. For the system with dual redundancy, analytic methods are used to detect faults based on the system dynamical model. Helicopter engine dynamics are affected by aerodynamic torque induced from the dynamics of the main rotor. In this paper an engine model including the rotor dynamics is constructed for the T700-GE-700 turboshaft engine powering UH-60 helicopter. The singular value decomposition(SVD) method is applied to the developed model in order to detect sensor faults. The SVD method which do not need an additional computation to generate residual uses the characteristics that the system outputs in direction of the left singular vector if an input is applied in direction of the right singular vector. Simulations show that the SVD method works well in detecting and isolating the sensor faults.

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GHP 운전시 COV에 의한 정상상태 판별 및 이상검출 방법 연구 (A Study on Steady-State Criterion based on COV and a Fault Detection Method during GHP Operation)

  • 신영기;오세재;정진희
    • 설비공학논문집
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    • 제23권11호
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    • pp.705-710
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    • 2011
  • Fault detection has to be proceeded by steady state filtering to get rid of transient effect associated with thermal capacity. Coefficient of variance (COV), ratio of standard deviation devided by moving average, was employed as steady-state filter. Engine speed and refrigerant pressures were selected as parameters representing system dynamics. The filtered values were registered as members of steady-state DB. They were found to show good functional relationship with ambient temperature. The relationship was fitted with a second order polynomial and the distribution bounds of the data around the fitted curve were expressed by visual inspection because of varying average and random data interval. Fault data were compared with the steady-state data obtained during normal operation. The fault data were easily isolated from the fault-free one. To make such isolation reliable, tests to construct good DB should be designed in a systematic way.