• 제목/요약/키워드: Main Rotor System

검색결과 157건 처리시간 0.024초

브러시리스 직류 전동기용 새로운 센서리스 드라이브 개발에 관한 연구 (A study on the development of a new sensorlss drive system for the brushless DC motors)

  • 장항제
    • 전력전자학회:학술대회논문집
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    • 전력전자학회 2000년도 전력전자학술대회 논문집
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    • pp.591-595
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    • 2000
  • In this paper we proposed a new sensorless drive system for the trapezoidal type brushless DC motor which does not use any mechanical position or speed sensor and applicable to the systems requiring a constant speed and torque such as Fan. For this a novel indirect rotor position sensing technique based on a detailed analysis of the terminal voltage characteristics is proposed in this paper. And a sensorless drive system for the brushless DC motor is implemented using a 87c196mc fo the main microprocessor and a power FET for the inverter. The experimental results will show the validity of the proposed indirect sensing method and the practical use of the sensorless drive

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트랙션용 전동기의 코깅토크 감쇄 구조에 관한 연구 (A study on Cogging Torque attenuation structure of traction motor)

  • 고형근;김병국;이상규;조재희;박태홍
    • 한국철도학회:학술대회논문집
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    • 한국철도학회 2011년도 정기총회 및 추계학술대회 논문집
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    • pp.2365-2372
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    • 2011
  • BLDC 모터와 같은 동기전동기에서 소음과 진동의 원인이 되는 코깅토크는 전동기내의 비 균일 토크로서 전동기 시스템의 자기 에너지가 최소인 위치로 이동하려는 접선방향의 힘으로 부하전류와 상관없이 회전자 영구자석과 고정자 슬롯의 상호작용에 의해 발생한다. 이러한 코깅토크는 전동기의 소음과 진동의 주요 원인이 되므로 전동기 설계 시 반드시 고려해야 한다. 코깅토크는 영구자석이 부착된 회전자에 의하여 공극 중에 비교적 저차의 고조파 자속밀도와 고정자 철심 슬롯의 상호작용으로 발생한다는 점을 중시하여 본 논문에서는 실험계획법의 일종인 반응표면 법을 사용하여 코깅토크를 저감하는 방법에 대해 제시하였다.

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자동화 비행시험기법에 의한 소형 무인헬리콥터의 파라메터 추정 (Parameter Estimation of a Small-Scale Unmanned Helicopter by Automated Flight Test Method)

  • 방극희;김낙완;홍창호;석진영
    • 제어로봇시스템학회논문지
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    • 제14권9호
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    • pp.916-924
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    • 2008
  • In this paper dynamic modeling parameters were estimated using a frequency domain estimation method. A systematic flight test method was employed using preprogrammed multistep excitation of the swashplate control input. In addition when one axis is excited, the autopilot is engaged in the other axis, thereby obtaining high-quality flight data. A dynamic model was derived for a small scale unmanned helicopter (CNUHELI-020, developed by Chungnam National University) equipped with a Bell-Hiller stabilizer bar. Six degree of freedom equations of motion were derived using the total forces and moments acting on the small scale helicopter. The dynamics of the main rotor is simplified by the first order tip-path plane, and the aerodynamic effects of fuselage, tail rotor, engine, and horizontal/vertical stabilizer were considered. Trim analysis and linearized model were used as a basic model for the parameter estimation. Doublet and multistep inputs are used to excite dynamic motions of the helicopter. The system and input matrices were estimated in the frequency domain using the equation error method in order to match the data of flight test with those of the dynamic modeling. The dynamic modeling and the flight test show similar time responses, which validates the consequence of analytic modeling and the procedures of parameter estimation.

가변속 구동을 위한 단상 유도전동기의 벡터제어 (Vector Control of Single Phase Induction Motor for Variable Speed Drive)

  • 이득기;이경주;정종진;김흥근
    • 대한전기학회:학술대회논문집
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    • 대한전기학회 2000년도 하계학술대회 논문집 B
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    • pp.1260-1263
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    • 2000
  • Vector control of a single phase induction machine(SPIM) is usually employed by mechanical methods than electrical ones. The disadvantage of a SPIM has large noise at the starting. Using auxiliary winding which is only utilized for starting, the SPIM can be controlled with the vector control method. Regarding a auxiliary winding one phase, the SPIM is analyzed by the unsymmetrical two phase motor and phase transformation is unnecessary such as three phase IM. Including a auxiliary winding, SPIM is modeled by mathematical getting by component of turns ratio with main to auxiliary winding. It will be take with complicated resultant formula, by comparison to symmetrical three phase TM. For using the vector control theory, it must be decoupled of rotor flux and torque component. stator current is controlled and decoupled. This paper presents a variable-speed control system of SPIM, which to decoupled with flux and torque component and to use machine equivalent circuit referred to rotor, conventionally three phase IM by similar method.

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원, 타원 및 인벌루트 조합된 치형형상을 갖는 로터 개발 (Development of an Automated Design System for Oil Pumps with Multiple Profiles(Circle, Ellipse and Involute))

  • 정성윤;김문생;조해용;김철
    • 한국정밀공학회지
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    • 제26권3호
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    • pp.103-112
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    • 2009
  • A internal lobe pump is suitable for oil hydraulics of machine tools, automotive engines, compressors, constructions and other various applications. In particular, the pump is an essential machine element of an automotive engine to feed lubricant oil. The subject of this paper is the theoretical analysis of internal lobe pump whose the main components are the rotors: usually the outer one is characterized by lobe with elliptical and involute shapes, while the inner rotor profile is determined as conjugate to the other. And the integrated system which is composed of three main modules has been developed through AutoLISP under AutoCAD circumstance. It generates new lobe profile and calculates automatically the flow rate and flow rate irregularity according to the lobe profile generated. Results obtained from the analysis enable the designer and manufacturer of oil pump to be more efficient in this field.

타원의 치형 형상을 갖는 로터 설계 자동화 시스템 개발 (Development of an Automated Design System for Oil Pumps with Ellipse Lobe Profile)

  • 정성윤;한승무;김철
    • 한국정밀공학회지
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    • 제26권1호
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    • pp.120-129
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    • 2009
  • An internal lobe pump is suitable for oil hydraulics of machine tools, automotive engines, compressors, constructions and other various applications. In particular, the pump is an essential machine element of an automotive engine to feed lubricant oil. The subject of this paper is the theoretical analysis of internal lobe pump whose the main components are the rotors: usually the outer one is characterized by lobes with elliptical shape, while the inner rotor profile is determined as conjugate to the other. And the integrated system which is composed of three main modules has been developed through AutoLISP under AutoCAD circumstance. It generates new lobe profile and calculates automatically the flow rate and flow rate irregularity according to the lobe profile generated. Results obtained from the analysis enable the designer and manufacturer of oil pump to be more efficient in this field.

고압전동기용 진동 감시 시스템을 위한 특징 파라미터 추출기법 개발 (Development of the Extracting Technique of the Character Parameter for the Vibration Monitoring System in High Voltage Motor)

  • 이달호;박정철
    • 한국정보전자통신기술학회논문지
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    • 제12권4호
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    • pp.349-358
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    • 2019
  • 본 논문에서는 회전체의 특징 파라미터들을 추출하기 위한 센서의 신호들을 수집하는 방법을 연구하고자 한다. 이를 위해, 모형 시험을 수행하기 위한 진동 테스트 리그를 개발하여 정상적으로 운전하에서의 신호특성을 분석하였다. 다른 진동 요소들로부터 주기적인 충격에 의해 발생되는 진동 성분을 추출하기 위하여 포락 신호처리(Envelope FFT Analysis) 기법을 사용하였다. 회전속도에 따른 신호분석과 더불어 회전체의 저주파수 특성을 잘 나타내는 속도센서 및 진동 테스트 리그의 부하변화에 따른 신호를 분석하였다. 그 결과, 베어링 하우징에서 측정되는 가속도 신호는 진폭이 작으며 조화 성분과 모터의 회전주파수 성분만이 발생함을 확인하였다. 즉, 회전수가 높아짐에 따라 가속도의 진폭이 높아짐을 확인할 수 있었다. 회전속도가 증가하면 원 데이터의 형상의 차이가 있는 것을 확인할 수 있었고, 가속도 FFT 그래프와 비교하였을 경우 저 주파수에서 노이즈에 강하며 해당 회전 주파수 성분을 뚜렷하게 나타내었다. 또한 부하를 변화시켜도 주요 회전 주파수 성분이 증가하지 않음을 알 수 있었다.

소형 원판형 하이브리드 자기 부상 모터 (A Small Disk-type Hybrid Self-healing Motor)

  • 김승종
    • 한국소음진동공학회논문집
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    • 제11권8호
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    • pp.338-348
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    • 2001
  • A hybrid self-hearing motor, which Is a functional combination of general permanent magnet (PM) motor and hybrid active magnetic bearing(AMB), was proposed a few years ago. In this paper the hybrid self-bearing motor is modified to a disk type, in which one of two magnetic hearings was substituted for a thin yoke to make the system more compact. An outer rotors in this self-hearing motor is actively controlled only in two radial directions while the ocher motions are passively salable owing to the disk-type structure. Main advantages of the proposed self-hearing motor are simple control mechanism, low power consumption and smart structure. Mathematical model for the magnetic force Is built wish consideration of the radial displacement of the rotor. The model helps us not only to design a levitation controller but also to expect the system performance. Some experimental results show good capability and feasibility of the Proposed self-bearing motor.

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비행 모드에 따른 CRW UAV 추진시스템의 정상상태 운전특성 해석 (Steady State Operational Characteristic Analysis of the Propulsion System for the Canard Rotor Wing UAV in three different Flight Modes)

  • 공창덕;강명철;기자영;박종하;양수석;전용민
    • 한국추진공학회:학술대회논문집
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    • 한국추진공학회 2003년도 제21회 추계학술대회 논문집
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    • pp.215-218
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    • 2003
  • 본 연구에서는 회전익 상태에서 이/착륙, 저속 전진비행을 하고, 고정익 상태에서 고속 전진비행을 하는 스마트 무인기 추진시스템을 모델링하고 회전익 모드, 고정익 상태의 고속 비행모드, 팁 제트 노즐과 주 엔진 노즐을 모두 이용하는 혼합모드에 대해 정상상태 성능해석을 수행하였다.

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저속영역에서의 브러시리스 직류전동기의 센서리스 운전 성능 향상에 대한 연구 (A Study on Performance Improvement of Sensorless Operation of the Brushless DC Moter in Low Speed Region)

  • 서문석;배종표;최재혁;김종선;유지윤;여형기
    • 전력전자학회:학술대회논문집
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    • 전력전자학회 2002년도 전력전자학술대회 논문집
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    • pp.124-128
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    • 2002
  • This Paper propose a novel sensorless drive system for the trapezoidal brushless DC motor in Bow speed region. The inverter DC input voltage is controlled by step-down converter for low speed operation. A indirect rotor position sensing technique based on a detailed analysis of the terminal voltage characterisrics is proposed in this paper. A sensorless drive system is implemented using a TMS320F240 for the main process and IPM(Intelligent Power Module) for the inverter.

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