• 한국추진공학회:학술대회논문집
• /
• 한국추진공학회 2004년도 제22회 춘계학술대회논문집
• /
• pp.521-523
• /
• 2004

The Japan Aerospace Exploration Agency (JAXA) has proposed new vertical take-off and landing (VTOL) aircraft known as the Jet-VTOL aircraft shown in Fig.1. The Jet-VTOL aircraft is based on a canard wing configuration. The aircraft has the clustered lift-fans mounted near the center of gravity for vertical flight, and has the clustered fans mounted beside the vertical tail for cruise flight. Both fans are driven by the core engine mounted inside the aft end of fuselage. The propulsion system is innovative and attractive not to be seen even in the world.

• 전력전자학회:학술대회논문집
• /
• 전력전자학회 2001년도 전력전자학술대회 논문집
• /
• pp.22-24
• /
• 2001

This paper presents the characteristics of current harmonics and torque ripple of Brushless DC motor, which is developed the fan blower of vehicles, according to input voltage waveform. To investigate the torque ripple and the phase current harmonics, these characteristics is analysed and compared the experimental results. In the process of analysis, FEM is introduced and computed a transient state torque of BLDC with a sinusoidal and a PWM wave voltage.

• 전력전자학회:학술대회논문집
• /
• 전력전자학회 2015년도 전력전자학술대회 논문집
• /
• pp.207-208
• /
• 2015

팬(fan), 펌프(pump), 블로어(blower), 전기 자동차(electric/hybrid vehicle), 전동차와 같은 다양한 분야에서 3상 전동기의 고속 운전에 대한 요구가 증대되고 있다. 일반적으로 3상 전동기가 정격 속도 이상의 고속에서 운전하기 위해서는 회전자 자속(rotor flux)의 크기를 운전 상황에 따라 감소시키는 약자속(flux weakening) 제어가 필수적이다. 유도 전동기의 회전자 자속 기준 벡터 제어 시의 약자속 운전은 자속 성분 전류의 크기를 제어하여 유도 전동기의 고속 운전을 가능하게 하는데, 이러한 전류 제어 기반의 약자속 제어는 그 구조가 복잡하고, 제어기 이득 선정에 따른 동특성(dynamic)이 영향울 받는 문제점을 가지고 있다. 본 논문에서는 이러한 단점을 개선하기 위한 순시적 약자속 제어 방법을 제안하고 3.7kW 유도 전동기를 이용한 실험을 통하여 제안된 방식의 성능을 검증한다.

• 한국소음진동공학회논문집
• /
• 제15권10호
• /
• pp.1177-1185
• /
• 2005

This paper investigates the noise radiated by a cascade of flat-plate airfoils interacting with homogeneous, isotropic turbulence. At frequencies above the critical frequency, all wavenumber components of turbulence excite propagating cascade modes, and cascade effects are shown to be relatively weak. In this frequency range, acoustic power was shown to be approximately proportional to the number of blades. Based on this finding at high frequencies, an approximate expression is derived for the power spectrum that is valid above the critical frequency and which is in excellent agreement with the exact expression for the broadband power spectrum. The approximate expression shows explicitly that the acoustic Power above the critical frequency is proportional to the blade number, independent of the solidity, and varies with frequency as ${\phi}_{ww}(\omega/W$), where ${\phi}_{ww}$ is the wavenumber spectrum of the turbulence velocity and W is mean-flow speed. The formulation is used to perform a parametric study on the effects on the power spectrum of the blade number stagger angle, gap-chord ratio and Mach number. The theory is also shown to provide a close fit to the measured spectrum of rotor-stator interaction when the mean square turbulence velocity and length-scale are chosen appropriately.

• 한국전자통신학회논문지
• /
• 제13권4호
• /
• pp.757-764
• /
• 2018

본 논문은 공조시스템에 사용되는 1마력급 2상 BLDC 팬모터의 설계 및 구현에 관하여 기술한다. 본 연구에서 구현한 BLDC 모터는 수명 및 내구성이 우수한 무정류자 모터방식이며 2상 전원에 의해 구동된다. 공조시스템에 사용되는 모터의 가장 중요한 목표사양은 정격운전점에서 높은 효율을 갖는 것이다. 이를 위해 BLDC 모터의 고정자 형상과 회전자 자석의 설계를 수행하고 구동을 위한 제어회로를 설계하였다. BLDC 모터는 모터부와 제어부 그리고 전원부가 일체화된 구조를 갖는다. BLDC 모터의 특성계산을 위해 유한요소해석을 사용하였으며 시제품의 제작 및 성능시험을 실시하여 설계결과의 적합성을 확인하였다.

• 한국소음진동공학회논문집
• /
• 제19권8호
• /
• pp.809-815
• /
• 2009

The previous work(Cheong et al., 2006) where the characteristics of acoustic emissions of wind turbines has been investigated according to the methods of power regulation, has showed that the acoustic power of wind turbine using the stall control for power regulation is more correlated with the wind speed than that using the pitch control. In this paper, basically extending this work, the noise generation characteristics of large modern upwind wind turbines are experimentally indentified according to the power regulation methods. To investigate the noise generation mechanisms, the distribution of noise sources in the rotor plane is measured by using the beam-forming measurement system(B&K 7768, 7752, WA0890) consisting of 48 microphones. The array results for the 660 kW wind turbine show that all noise is produced during the downward movement of the blades. This result show good agreement with the theoretical result using the empirical formula with the parameters: the convective amplification; trailing edge noise directivity; flow-speed dependence. This agreement implies that the trailing edge noise is dominant over the whole frequency range of the noise from the 660 kW wind turbine using the pitch control for power regulation.

• Journal of Power Electronics
• /
• 제15권5호
• /
• pp.1264-1273
• /
• 2015

An inverter output power control based power factor correction (PFC) strategy is being extensively used for permanent magnet synchronous motor (PMSM) drives in appliances because such a strategy can considerably reduce the cost and size of the inverter. In this strategy, PFC circuits are removed and large electrolytic DC-link capacitors are replaced with small film capacitors. In this application, the PMSM d-q axes currents are controlled to produce ripples, the frequency of which is twice that of the AC main voltage, to obtain a high power factor at the AC mains. This process indicates that the PMSM operates under periodic magnetic saturation conditions. This paper proposes a back electromotive-force (back-EMF) estimator for the high-speed sensorless control of PMSM operating under periodic magnetic saturation conditions. The transfer function of the back-EMF estimator is analyzed to examine the effect of the periodic magnetic saturation on the accuracy of the estimated rotor position. A simple compensation method for the estimated position errors caused by the periodic magnetic saturation is also proposed in this paper. The effectiveness of the proposed method is experimentally verified with the use of a PMSM drive for a vacuum cleaner centrifugal fan, wherein the maximum operating speed reaches 30,000 rpm.

• 한국소음진동공학회:학술대회논문집
• /
• 한국소음진동공학회 2009년도 춘계학술대회 논문집
• /
• pp.63-67
• /
• 2009

The previous work (Cheong et al., 2006) where the characteristics of acoustic emissions of wind turbines has been investigated according to the methods of power regulation, has showed that the acoustic power of wind turbine using the stall control for power regulation is more correlated with the wind speed than that using the pitch control. In this paper, basically extending this work, the noise generation characteristics of large modern upwind wind turbines are experimentally indentified according to the power regulation methods. To investigate the noise generation mechanisms, the distribution of noise sources in the rotor plane is measured by using the Beam-forming measurement system (B&K 7768, 7752, WA0890) consisting of 48 microphones. The array results for the 660 kW wind turbine show that all noise is produced during the downward movement of the blades. This result show good agreement with the theoretical result using the empirical formula with the parameters: the convective amplification; trailing edge noise directivity; flow-speed dependence. This agreement implies that the trailing edge noise is dominant over the whole frequency range of the noise from the 660 kW wind turbine using the pitch control for power regulation.

• 한국입자에어로졸학회지
• /
• 제15권4호
• /
• pp.139-148
• /
• 2019

This study was performed for the application of a high-speed centrifugal cyclone to shale gas mining process. This device uses the centrifugal force to control particles similar to typical cyclones, and the disk located inside the cyclone is forced to rotate using a motor. The pressure difference occurred during the rotating of disk. Hence, inflow rate was generated without a blower fan. In addition, flow rate increased with elevating rpm of motor. The installing the disk in multiple stages on the inner rotor increased the instantaneous disk outlet flow. Hence, the control efficiency of oil particle increased from 1.05% to 31.2%. By modifying the structure of the disk so that the air flow to the opposite direction of the cyclone, the control efficiency of oil particles increased to 81.5%. By increasing the capacity of the motor and the size of the disk, the flow rate was increased to 2.5 ㎥/min because the rpm of motor and pressure difference increased. As rpm of motor increased, the cut-off diameter (d_pc) became smaller. Unlike the Lapple's equation, d_pc was inversely proportional to the effective number of rotations (N_e). The control efficiency was maintained even if the concentration of oil particles increased, for this reason, the higher the oil concentration, the more particles were accumulated and controlled.

• 항공우주시스템공학회지
• /
• 제14권1호
• /
• pp.68-73
• /
• 2020

본 논문은 산악 지형, 도심, 함정, 교량 등에서 수직 이·착륙 비행, 제자리 비행, 고정익기처럼 저속 및 고속비행을 할 수 있는 덕티드 추진체를 사용한 수직 이·착륙 초소형 무인 항공기 개발 동향을 기술한다. 이 항공기는 여러 측면에서 헬리콥터와 고정익기와는 비행 특성이 다르다. 미육군 미래 전투 체계와 DARPA의 OAV 프로그램의 목적은 운용자에 안전하고 낮은 음향 특성을 갖는 수직 이·착륙 덕티드 팬 초소형 무인 항공기 개발이다. 현재의 초소형 무인 항공기에 영상/적외선 카메라를 탑재하고 숲이나 언덕 뒤에 숨어 있는 적을 정지비행과 응시로 약 1 시간 동안 감시 및 정찰을 한다. OAV의 Class-I은 개인 병사가 배낭에 담아 운반할 수 있는 크기와 무게의 수직 이·착륙 덕티드 MAV 개발이다. Class-II는 Class-I보다 두 배의 운용 시간과 더 넓은 범위의 비행이 가능한 유기체의 수직 이·착륙 덕티드 팬 초소형 무인 항공기 개발이다. 초소형 무인기는 장시간 운용을 위해 현재의 '호버 및 응시'에서 '퍼치-앤-응시'으로 기술을 발전시켜야 한다. 근 미래의 OAV 개념은 유·무인 지상 차량이 주행하는 동안에 차량의 상부에 자동 이착륙하고, 탑재된 상태로 이동하고, 재급유, 재충전, 재이륙하는 합동 운용으로 임무 능력과 효율성을 확장하는 것이다. 덕티드 MAV는 지상 차량의 착륙 패드에서 자동으로 이착륙하기 위해 저렴한 초소형 GPS를 활용한 고정밀 상대 위치 기술 개발이 필요하다. 또한, VTOL 덕티드 MAV와 유·무인 지상 차량 간에 유기체의 협업 동작이 가능케하는 공통 명령과 제어 아키텍처를 개발할 필요가 있다.