• 제목/요약/키워드: actuator failure

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LPG 자동차 엔진의 솔레노이드밸브, 릴레이, 공회전조절장치의 고장사례 연구 (Study for Failure Examples of Solenoid Valve, Relay and Idle Speed Control Actuator in Liquid Petroleum Gas vehicle Engines)

  • 김청균;이일권;조승현
    • 한국가스학회지
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    • 제15권3호
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    • pp.47-52
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    • 2011
  • 이 논문의 목적은 LPG 자동차의 전자제어에 대한 요소의 하나인 액추에이터에 대한 고장사례를 찾아 분석하고 연구하는 것이다. 차량의 연료를 저장하는 봄 내부의 LPG 긴급 차단 솔레노이드 밸브의 필터가 막혀 연료의 공급이 간헐적으로 차단되는 현상이 발생되어 엔진이 작동하는 동안 엔진의 초기시동불량이나 가속이 되지 않는 것을 확인하였다. 엔진 컨트럴 릴레이 부위의 접점부가 가공불량이나 조립불량에 의해 완전한 면접촉이 되지않아 접촉저항이 발생되어 초기 시동을 걸었을 때 시동이 걸렸으나 재시동을 걸 때 시동이 걸리지 않는 현상을 확인하였다. 공회전 조절장치의 내부에 카본이 퇴적되어 액추에이터가 고착되어 흡입공기의 공급이 감소되어 자동차의 시동이 걸려 공회전 상태일 때 엔진의 회전수가 규정 범위를 벗어나 상승과 하락을 반복하는 불안정 상태를 확인하였다.

항공기용 영구자석 동기전동기 고장진단의 기술 동향 및 분석 (Failure Diagnosis Technology Trends and Analysis of Permanent Magnet Synchronous Motors for Aircraft Application)

  • 김민우;고상호
    • 항공우주시스템공학회지
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    • 제16권6호
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    • pp.129-137
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    • 2022
  • 최근 항공기용 구동기는 전기식 구동기의 높은 정밀도 및 유지관리의 용이성 등으로 인해 기존 유압 중심의 기계시스템에서 전기구동 중심(More/All Electric)으로 기술이 변화하고 있다. 따라서 항공기의 전기 전동기 고장은 치명적인 결함을 넘어 인명피해로도 이어질 수 있다. 전기 전동기의 고장진단은 항공기의 안전성을 보장하는데 필수적인 요소이다. 이에 따라 효율적이고 적절한 고장진단이 요구되며 이러한 고장진단 기술 연구가 활발히 이루어지고 있다. 본 논문에서는 전기 전동기 중 영구자석 동기전동기의 고장 유형과 고장진단 기술 동향에 대해 소개하고 분석한다.

양에서 시행한 이동작동기 형태(MOVING ACTUATOR TYPE) 인공심장의 삽입실험 (Experimental Implantation of Moving Actuator Type Total Artificial Heart in Sheep)

  • 김원곤
    • Journal of Chest Surgery
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    • 제28권6호
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    • pp.533-541
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    • 1995
  • We recently developed a new model of moving actuator type totally implantable artificial heart[TIAH , based on the reverse position of the aortic and pulmonary conduits. This concept was proposed by one of surgeons in our team[Joon-Ryang Rho, M.D. to facilitate anatomical fitting of TIAHs. The moving actuator type electromechanical TIAH consisted of the left and right blood sacs, and the moving actuator including a motor. The inverted umbrella type polyurethane valves were used in the blood pumps. The aortic conduit was positioned anterior to the pulmonary conduit, which was the opposite relation to the conventional configuration of other total artificial hearts. We also adapted slip-in connectors for the aortic and pulmonary conduits. Two sheep , weighing 60-69 kg, were used for implantation. After small cervical incision and trans-sternal bilateral thoracotomy, cardiopulmonary bypass [CPB was administered using an American Optical 5-head pump and a membrane oxygenator[Univox-IC, Bentley . The anterior and posterior vena cavae were drained separately for venous return. An arterial return cannula was inserted into the right common carotid artery. During CPB, almost all of the ventricular myocardium was excised down to the atrioventricular groove and the artificial heart was implanted. We achieved 3-day survival in the first sheep and 2-day survival in the second. The day after operation the first sheep was successfully extubated and the second sheep was weaned from a respirator with good condition. After extubation, the first sheep walked around in the cage and fed herself. Serial laboratory and hemodynamic examinations were done during the experiments. In both sheep, pulmonary dysfunction was gradually developed, which was accompanied by acute renal failure. The animals were sacrificed and autopsy was done. Unexpected pregnnacy was incidentally found in both sheep. To our knowledge this is the first report of significant survival cases in the orthotopic implantation of electric TIAH using sheep.

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Fine Seek Control of Extended Applicable Range for Optical Disk Drives

  • Ryoo, Jung-Rae;Jin, Kyoung-Bog;Doh, Tae-Young;Chung, Myung-Jin
    • Transactions on Control, Automation and Systems Engineering
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    • 제3권3호
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    • pp.146-151
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    • 2001
  • Optical disk drive has excellent advantage of random accessibility of which performance is measured by access time. However, due to the increased rotational velocity of the disk and constraints of mechanical structure, two-stage seek algorithm which executes coarse and fine seeks sequentially has been adopted in most commercial optical disk drives. Although the laser spot is moved to a target track by a single seek operation, the limited operation range of the fine actuator restricts the application of the fine seek algorithm below a few hundreds of tracks. Especially, excessive movement of the objective lens causes a failure in generation of track-cross pulse and results in an unstable seek operation. In this paper, a new control algorithm for extending the fine seek range is proposed with an appropriate control structure. The coarse actuator is utilized to reduce the misalignment between the objective lens and the laser beam axis, and the fine actuator is controlled to follow the reference velocity trajectory. The proposed algorithm is applied to a CD-ROM drive to show its feasibility and some experimental results are presented.

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PDMS를 이용한 마이크로 구동기의 제작 및 평가 (Detection of Tool Failure by Wavelet Transform)

  • 이동원;박종성
    • 한국기계가공학회지
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    • 제7권2호
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    • pp.72-77
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    • 2008
  • In this study, we propose and develop PDMS-based modular actuators. The microactuator which looks like a small insect uses thermal expansion power of the PDMS (polydimethylsiloxane; $sylgar^{(R)}$ 184 silicone elastomer). The PDMS-based microactuator provides a large displacement due to a high thermal expansion coefficient (approximately 310ppm). The microacruator with 1mm length $350{\mu}m$ width is optimized by using a numerical analysis. The shape of the PDMS actuatoris variously designed. They are placed at several positions to find the optimal position that provides a high transformation ratio. The PDMS-based microactuators are fabricated using a conventional micromaching technique. The fabricated microactuator is heated using a hot-plate. The actuator displacement is measured as a function of temperature from $27^{\circ}C$ to $300^{\circ}C$. The experimental results are compared to the simulation result. When heating temperature up to $300^{\circ}C$ is applied to the PDMS actuator, each V-groove-shaped joint is actuated $30{\mu}$ mat $300^{\circ}C$. Anotherdesign of the microactuator has a maximum displacement of about 656mm.

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굽힘 압전 복합재료 작동기의 전기적 피로 거동 (Electric Fatigue Behavior of a Bending Piezoelectric Composite Actuator)

  • 우성충;구남서
    • 대한기계학회:학술대회논문집
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    • 대한기계학회 2008년도 추계학술대회A
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    • pp.362-367
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    • 2008
  • In the present work, we address electric fatigue behavior in bending piezoelectric actuators using an acoustic emission technique. Electric cyclic fatigue tests have been performed up to ten million cycles on the fabricated specimens. To confirm the fatigue damage onset and its pathway, the source location and distributions of the AE behavior in terms of count rate are analyzed over the fatigue range. It is concluded that electric cyclic loading leads to fatigue damages such as transgranular damages and intergranular cracking in the surface of the PZT ceramic layer, and intergranular cracking even develops into the PZT inner layer, thereby degrading the displacement performance. The electric-induced fatigue behavior seems to show not a continuous process but a step-by-step process because of the brittleness of PZT ceramic. Nevertheless, this fatigue damage and cracking do not cause the final failure of the bending piezoelectric actuator loaded up to 107 cycles. Investigations of the AE behavior and the linear AE source location reveal that the onset time of the fatigue damage varies considerably depending on the existence of a glass-epoxy protecting layer.

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전기적 피로하중을 받는 압전 작동기의 손상 메커니즘 (Damage Mechanisms of a Piezoelectric Actuator under Electric Fatigue Loading)

  • 우성충;구남서
    • 대한기계학회논문집A
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    • 제32권10호
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    • pp.856-865
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    • 2008
  • Damage mechanisms in bending piezoelectric actuators under electric fatigue loading are addressed in this work with the aid of an acoustic emission (AE) technique. Electric cyclic fatigue tests have been performed up to $10^7$ cycles on the fabricated bending piezoelectric actuators. An applied electric loading range is from -6 kV/cm to +6 kV/cm, which is below the coercive field strength of the PZT ceramic. To confirm the fatigue damage onset and its pathway, the source location and distributions of the AE behavior in terms of count rate and amplitude are analyzed over the fatigue range. It is concluded that electric cyclic loading leads to fatigue damages such as transgranular damages and intergranular cracking in the surface of the PZT ceramic layer, and intergranular cracking even develops into the PZ inner layer, thereby degrading the displacement performance. However, this fatigue damage and cracking do not cause the final failure of the bending piezoelectric actuator loaded up to $10^7$ cycles. Investigations of the AE behavior and the linear AE source location reveal that the onset time of the fatigue damage varies considerably depending on the existence of a glass-epoxy protecting layer.

배선 단선과 에어 누설에 관련된 자동차 ECS 시스템의 고장사례 고찰 (Study of Failure Examples of Automotive Electronic Control Suspension System Including Cases with Wiring Disconnection and Air Leakage)

  • 이일권;박종건;신명신;장주섭
    • Tribology and Lubricants
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    • 제29권3호
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    • pp.180-185
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    • 2013
  • The purpose of this study was to analyze the tribological characteristics of the Electronic control suspension System in a car. In the first example, the cilp used to attach the front electronic control suspension(ECS) system's control actuator was fastened very tightly. Thus, the wire was cut because of continual rotation of the shock-up shover piston rod used to adjust the height of the car. This verified the disconnection phenomenon where wire damaged makes it impossible for the ECS system to send signal to the actuator. The second example, involved a minute hole that allowed gas to leak from the ECS system. As a result, the height of the car verified the down phenomenon. In the third example, the resistance of a wire measured at $0.21{\Omega}$, when the G sensor was disconnected from the system. This verified the system shutdown and lighting of the ECS warning lamp because of body interference caused by a slight pressure on the battery cover. Therefore, quality control is always necessary to ensure safety and durability of a car.

Prediction of Gear Bending Fatigue Life of Electro-mechanical Actuator for Aircraft Through Finite Element Analysis

  • Kim, Taehyung;Seok, Taehyeon;Kwon, Soon-hyeong;Lee, Byung-ho;Kwon, Byung-gi;Kwon, Jun-yong;Cheong, Seong-kyun
    • 항공우주시스템공학회지
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    • 제14권6호
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    • pp.58-67
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    • 2020
  • In this study, finite element fatigue analysis combined with a fatigue correlation factor is proposed to predict the bending fatigue life of a gear in an electro-mechanical aircraft actuator. First, stress-life curves are obtained for the gear material via a round bar fatigue test. Subsequently, stochastic stress-life (P-S-N) curves are derived for 50% and 1% failure probabilities, separately. The curves are applied to the fatigue analysis model of a single gear tooth, and the effect of the fatigue correction factor is analyzed. The analytical P-S-N curves reflecting the fatigue correction factor matched the experimental data. This shows that the analytical fatigue life is reliable and that the analysis technique is effective.

온라인 학습 신경망 조직을 이용한 내고장성 제어계의 설계 (A Design of a Fault Tolerant Control System Using On-Line Learning Neural Networks)

  • Younghwan An
    • 소음진동
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    • 제8권6호
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    • pp.1181-1192
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    • 1998
  • 본 연구에서는 신경조직망을 이용한 항공제어계의 내고장성 성능에 대해 관점을 두었다. 이 내고장성 제어계는 감지기와 작동기의 고장 발견. 확인 그리고 보완으로 이루어진다 SFDIA는 주 신경조직망과 n개의 국소 신경조직망으로 이루어지는데, 여분의 감지기 없이 n개의 감지기로 내고장성 능력을 성취함을 목적으로 한다. 또한, AFDIA는 같은 주 신경조직망과 세개의 신경조직망 제어기들로 구성되며. 이 제어기들은 평형을 유지하는 역할을 하며 고장으로 인한 pitching. rolling. 그리고 yawing moment를 상쇄하는 기능을 한다. 본 연구에서는 특히 잘못된 경보와 고장 확인의 성능이 떨어짐이 없이 SFDIA와 AFDIA의 효과적인 통합 기능을 수행하는데 중점을 두었으며 여러 가지 작동기와 감지기의 고장에 대한 연구 결과가 제시되었다.

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