• 전기학회논문지
• /
• 제56권6호
• /
• pp.1039-1046
• /
• 2007

This paper presents the analysis for power consumption, mechanical vibration and acoustic noise characteristics of the Coreless and Slotless Brushless DC motor in Digital Lightening Processor(DLP) Motor with the Air-Dynamic Bearing. The Coreless BLDC motor has not the stator yoke as well as the stator slot to remove the unbalance force by the interaction between the stator yoke and Air-Dynamic Bearing clearance. The assembling tolerance and the processing error make the air-gap difference between the magnet and the stator yoke .which occurs the unbalanced electro-magnetic force in the Slotless BLDC motor. It imposes the air-dynamic bearing on the disturbance force and makes the Air-Dynamic Bearing vibrated and noised. Also, The attractive force between the magnet and the silicon steel stator yoke increases the power consumption. In this paper, the power consumption, mechanical vibration and acoustic noise of the Coreless BLDC motor and the Slotless BLDC motor with the silicon steel stator yoke are simulated, analyzed, and tested using the manufactured proto-type motors with Air-Dynamic bearing. The simulated and tested results present that the Coreless BLDC motor without the silicon steel stator yoke has the lower mechanical vibration and noise ,and lower power consumption than the Slotless BLDC motor with the silicon steel stator yoke in Digital Lightening Processor Motor with Air-Dynamic Bearing.

• Journal of Electrical Engineering and Technology
• /
• 제4권2호
• /
• pp.255-265
• /
• 2009

This paper presents the acoustic noise and mechanical vibration reduction of a coreless brushless DC motor with an air dynamic bearing used in a digital lightening processor. The coreless brushless DC motor does not have a stator yoke or stator slot to remove the unbalanced force caused by the interaction between the stator yoke and the rotor magnet. An unbalanced force makes slotless brushless DC motors vibrate and mechanically noisy, and the attractive force between the magnet and the stator yoke increases power consumption. Also, when a coreless brushless DC motor is driven by a $120^{\circ}$ conduction type inverter, high frequency acoustic noise occurs because of the peak components of the phase currents caused by small phase inductance and large phase resistance. In this paper, a core-less brushless DC motor with an air dynamic bearing to remove mechanical vibration and to reduce power consumption is applied to a digital lightening processor. A $180^{\circ}$ conduction type inverter drives it to reduce high frequency acoustic noise. The applied methods are simulated and tested using a manufactured prototype motor with an air dynamic bearing. The experimental results show that a coreless brushless DC motor has characteristics of low power consumption, low mechanical vibration, and low high frequency acoustic noise.

• 대한전기학회:학술대회논문집
• /
• 대한전기학회 2005년도 제36회 하계학술대회 논문집 B
• /
• pp.1444-1446
• /
• 2005

Recently most machineries have been small size and mobile type. And human body insertion type endoscope and micro robot technology has been developed. Then the motors used in this field are developed in micro size such as about 2mm in diameter. The structure of this motor is similar to a general brushless DC(BLDC) motor but because of small size there is no position sensor such as hall sensor. In this paper, a design and fabrication result of an ultra-small brushless DC motor is presented. This motor is designed to 3-phase coreless winding and operated with sensor-less type driver. Test results confirmed the feasibility of the proposed motor drive system design.

• 항공우주시스템공학회지
• /
• 제12권2호
• /
• pp.1-6
• /
• 2018

위성의 자세제어 구동기에 사용되는 직접구동 모터(BLDC Motor)의 영구자석 자속밀도 분포 불균일은 위성 토크 리플을 발생시켜 자세에 지대한 영향을 미친다. 본 논문은 이러한 토크 리플을 줄이기 위해 영구자석의 형상, 배치, 공극에 따른 자속밀도를 이론과 유한요소법 시뮬레이션을 통하여 분석하고 가장 적합한 자석 형상조합을 찾고자 한다. 사각형과 아치형, 단일 자석 배치와 듀얼자석 배치형상의 자속밀도 성능비교를 통해 최적의 자석 배치형상을 구하였으며, 이의 검증을 위해 시제품 모터(Protype Motor) 제작을 통하여 성능을 검증하였다.

• 항공우주시스템공학회지
• /
• 제13권3호
• /
• pp.1-8
• /
• 2019

전자기적 힘에 의해 김블 모터에 토크가 발생하며 코일 전류 변화는 토크 리플을 야기한다. 이는 김블속도에 영향을 주는 동시에 위성의 자세를 불안정하게 한다. 따라서 위성의 자세 제어 정확도 향상을 위해서는 김블 모터의 토크 리플 저감이 필수적이다. 본 논문에서는 일반적인 집중형 권선과 분포형 권선에 대해 모터의 모델링으로부터 발생 토크를 이론적으로 시뮬레이션 분석하였다. 토크 리플을 저감하는 권선을 선정하여 시제품을 설계 및 제작하여 자기장 및 역기전력의 이론적 해석 결과와 측정 결과를 비교하여 설계와 제작의 합치성을 확인하였다. 저속 시험을 통해 전절권 분포형 권선의 속도 안정도가 향상되어 토크 리플이 저감됨을 입증하였다.