• 제목/요약/키워드: Electro Mechanic Actuator

검색결과 5건 처리시간 0.023초

공기압 Servo Valve 설계 및 해석 (The Analysis and Design of Electro-pneumatic Servo Valve)

  • 고진호;류동렬;이주호;김영석;김동수
    • 대한기계학회:학술대회논문집
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    • 대한기계학회 2008년도 추계학술대회A
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    • pp.1210-1214
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    • 2008
  • Electro-pneumatic servo valve is an electro-mechanical device which converts electric signal into pneumatic flow rate or pressure. In order to improve the overall performance of pneumatic servo systems, electro-pneumatic servo valves are required, which have fast dynamic characteristic, no air leakage at null, and can be fabricated at a low-cost. The first objective of this research is to design and fabricate a new electro-pneumatic servo valve which satisfies the above-mentioned requirements. In this paper, we has been modeled as a system consisting of coupled electro-mechanic and mechanical subsystems. The appropriateness of the model has been verified by simulation. The simulation model resolves the valve body motion and the solenoid current at high accuracy. Also, we are calculate the displacement of spool and computed results show winding currents, magnetic actuator force, flux density line, displacement, velocity, back EMF, eddy current etc.

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SWCNT/Nafion 복합체의 분산능 향상을 통한 IPMC의 기계적 특성 향상 (Improvement of Mechanical Properties of IPMC through Developing a Degree of Dispersion of SWCNT/Nafion Composite)

  • 권희준;김하나;강정호
    • 한국기계가공학회지
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    • 제10권5호
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    • pp.131-136
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    • 2011
  • Many researchers are recently studying about Electroactive polymer(EAP). But it has a physical limitation, because of property of material. Carbon nanotube(CNT) is known as the promising material which has excellent electro-mechanical characteristics and is mostly defect-free. It is expected that a successful synthesis of CNT and Nafion known as a primary material for IPMC would make a great improvement on its electro-mechanic feature. This study focuses on the method of synthesis of CNT with Nafion which improves electro-mechanical characteristic. To come up with mechanical dispersion with Nafion and Isopropyl Alcohol(IPA), we dispersed Single-walled carbon nanotubes(SWCNTs). For a uniformly layer of CNT, we used a spray gun on a hot plate by a simplified method. We fabricated a disperse SWCNT/Nafion composite uniformly. Through the use of the E-beam evaporator to form an uniform electrode layer, we consummated the IPMC actuator. This result shows improving 1.5 times mechanical properties about driving force in IPMC.

IPMC의 기계적 특성향상을 위한 SWCNT/Nafion 복합체 개발 (SWCNT/Nafion Composite Development for Improvement of Mechanical Properties of IPMC)

  • 권희준;이헌상;이정화;전찬봉;강정호
    • 한국기계가공학회지
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    • 제10권1호
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    • pp.47-53
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    • 2011
  • From recent research, it has revealed that Electroacitve polymer(EAP) has a physical limitation. Carbon nanotube(CNT) is known as the promising material which has excellent electro-mechanical characteristics and is mostly defect-free. It is expected that a successful synthesis of CNT and Nafion known as a primary material for IPMC would make a great improvement on its electro-mechanic feature. In this paper, we suggest the method of synthesis of CNT with Nafion which improves electro-mechanical characteristic. Using mechanical dispersion with Nafion and Isopropyl Alcohol(IPA), we disperse Single-walled carbon nanotubes(SWCNT). For a uniformly layer of CNT, we used a spray gun on a hot plate by a simplified method. In the result, we fabricated a disperse SWCNT/Nafion composite uniformly.

항공기 디지털 전자식 비행제어 시스템 기술 개발 동향 (Aircraft Digital Fly-By-Wire System Technology Development Trend)

  • 채성병
    • 한국전자통신학회논문지
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    • 제18권3호
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    • pp.509-520
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    • 2023
  • 항공기에서 소형 제트기까지 항공기에 적용되는 플라이 바이 와이어 시스템의 구성 및 특성등에 대하여 기술 하였다. 특히 비행조종컴퓨터 다중화 방안과 데이터 통신 버스, 조종면 작동기, 플라이 바이 와이어 시스템을 통하여 적용되는 제어 법칙 등에 대한 기술 개발 동향에 대해 고찰하였다. 전투기에 처음 적용되었던 플라이 바이 와이어 시스템은 여러 가지 장점으로 인해 까다로운 인증과정을 거쳐 민간 항공기에까지 적용되었고, 최근에는 소형제트기까지 적용 범위가 확장되고 있으며 미래에는 대부분 플라이 바이 와이어 항공기가 주를 이룰 것으로 전망된다.

The Simulation and Research of Information for Space Craft(Autonomous Spacecraft Health Monitoring/Data Validation Control Systems)

  • Kim, H;Jhonson, R.;Zalewski, D.;Qu, Z.;Durrance, S.T.;Ham, C.
    • 한국산학기술학회논문지
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    • 제2권2호
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    • pp.81-89
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    • 2001
  • 우주 항공위성 시스템은 변하는 불확실한 우주항공 환경에(서) 운행되고 지상기지국으로부터의 원격통신 없이 장시간 동안 동작해야 할 자율적인 능력이 요구되고, 결함 없이 임무를 수행하여야 하며, 시스템에서 계측된 데이터의 신뢰성을 유지하기 위한 고장 상태 검출과 오류 수정 시스템을 차보하는 것이 중요하다. 본 논문에서는 확장 칼만 필터 기법을 적용한 동적모델 시뮬레이션 기법(High Fidelity, Dynamic Model-based Simulation)을 제안하였으며, 제안된 시스템은 비정상적인 데이터의 효과적인 검출과 대응이 가능해짐으로써 신뢰성 있는 우주항공위성시스템을 구축하도록 자동 상태 진단/데이터 시스템에 고장검출/오류수정 시스템을 적용하는 것이다. (Autonomous Spacecraft Health Monitoring/Data Validation Control System : ASHMDVCS).

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