• 제목/요약/키워드: Rotor performance

검색결과 1,504건 처리시간 0.022초

소형 로터 블레이드의 제자리 비행 성능 시험장치 개발 및 검증 (Development and Verification of Small-Scale Rotor Hover Performance Test-stand)

  • 이병언;서진우;변영섭;김정;이관중;강범수
    • 한국항공우주학회지
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    • 제37권10호
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    • pp.975-983
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    • 2009
  • 본 논문은 동축반전 로터 블레이드의 성능 특성 파악을 위한 선행연구로서, 단일 로터 블레이드에 대한 공력 데이터 획득 및 성능 특성을 확인하기 위한 연구에 중점을 두었다. 이를 위해 제자리 비행 상태에서 추력과 토크의 측정이 가능한 소형 로터 블레이드용 회전 시험장치를 구성하고 제작하였다. 로터 회전 시험장치는 회전장치부, 센서부, 그리고 데이터 획득 시스템으로 구성되었으며, 고정된 회전속도에서 콜렉티브 피치각을 변화시키면서 추력과 토크를 측정할 수 있도록 하였다. 이를 통하여 저 레이놀즈 수 ($Re{\approx}3{\times}10^5$) 영역에서 운용되는 단일 로터의 제자리 비행 성능 시험을 수행하였고 소형 로터 블레이드의 제자리 비행 성능을 획득하여 로터 회전 시험장치의 성능을 검증하였다.

Performance Comparison of Three Different Types of Attitude Control Systems of the Quad-Rotor UAV to Perform Flip Maneuver

  • Lee, Byung-Yoon;Yoo, Dong-Wan;Tahk, Min-Jea
    • International Journal of Aeronautical and Space Sciences
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    • 제14권1호
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    • pp.58-66
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    • 2013
  • This paper addresses the performance of three different types of attitude control systems for the Quad-rotor UAV to perform the flip maneuver. For this purpose, Quad-rotor UAV's 6-DOF dynamic model is derived, and it was used for designing an attitude controller of the Quad-rotor UAV. Attitude controllers are designed by three different methods. One is the open-loop control system design, another is the PD control system design, and the last method is the sliding mode control system design. Performances of all controllers are tested by 6-DOF simulation. In case of the open-loop control system, control inputs are calculated by the quad-rotor dynamic model and thrust system model that are identified by the thrust test. The 6-DOF realtime simulation environment was constructed in order to verify the performances of attitude controllers.

순항중인 틸트로터의 회전하는 블레이드에 대한 공력성능 수치해석 (Numerical Analysis of Aerodynamic Performance for Rotating Blades of Tilt Rotor Aircraft in Cruise Mode)

  • 안성원;고성호;김병수;최성욱
    • 한국전산유체공학회:학술대회논문집
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    • 한국전산유체공학회 2005년도 춘계 학술대회논문집
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    • pp.21-24
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    • 2005
  • Numerical analysis were made for the unsteady flow fields of the rotor system of a Tilt-Rotor aircraft in cruise mode. The Reynolds-averaged thin-layer Wavier-Stokes equations were discretized by Roe's upwind differencing scheme and integrated in time by the LU-SGS algorithm. The computational domain of the rotor system was constructed by seven multi-block Chimera grids. Comparison of pressure coefficient on the surface of the main wing and blades were made for 3cases of advance ratio(0.325, 0.350, 0.375) and thrust and power coefficients for the rotor were compared with experimental data.

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회전자 시정수를 보상한 유도전동기 센서리스 벡터제어 (Sensorless Vector Control of Induction Motor with Rotor Time Constant Compensation)

  • 박철우;이무영;윤경섭;구본호;권우현
    • 대한전기학회:학술대회논문집
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    • 대한전기학회 1998년도 하계학술대회 논문집 B
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    • pp.493-496
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    • 1998
  • Several sensorless vector control methods of induction motor have been proposed, but these methods don't have the satisfying performance to the change of the rotor time constant. Therefore, this paper proposes the sensorless vector control method which estimates the rotor speed using MRAS and compensates the rotor time constant using current error feedback at the same time. This method can guarantees the accurate performance of sensorless vector control while the rotor speed and the rotor time constant are changing. This method is verified by computer simulation using SIMULINK in MATLAB.

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새로운 유도전동기의 회전자저항 추정 알고리즘 (A New Rotor Resistance Identification Algorithm for Induction Motors)

  • 김규식
    • 대한전기학회:학술대회논문집
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    • 대한전기학회 1994년도 하계학술대회 논문집 A
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    • pp.303-306
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    • 1994
  • This paper presents a new rotor resistance identification algorithm for induction motors. The algorithm is derived form the fact that the slip frequency given in the d-q rotating frame is equal to that measured in the x-y fixed frame. Rotor resistance varies greatly with the machine temperature. In certain cases, the rotor resistance can increase 100 % over its ambient or nominal value. This deteriorates the dynamic performance of vector control systems for induction motors. However, the control scheme proposed in this paper is robust with respect to variations in rotor resistance because an efficient identification algorithm for rotor resistance is employed. To illuminate the performance of the proposed controller further, the simulation results are presented.

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PM Assisted, Brushless Wound Rotor Synchronous Machine

  • Ali, Qasim;Atiq, Shahid;Lipo, Thomas A.;Kwon, Byung-il
    • Journal of Magnetics
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    • 제21권3호
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    • pp.399-404
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    • 2016
  • This paper presents a new permanent magnet (PM) assisted topology for a recently introduced brushless wound rotor synchronous machine (BL-WRSM) [1]. The BL-WRSM had a dual-inverter configuration for generating a composite magneto motive force (MMF) with a fundamental component and a subharmonic component. The subharmonic component of the MMF is used for brushless excitation of the rotor. In this paper, additional PMs were introduced on the rotor of the BL-WRSM, making it a hybrid BL-WRSM. We also discussed the flux weakening operation for the hybrid BL-WRSM. The hybrid BL-WRSM offered advantages for starting the machine and provided better performance under full-load conditions. The finite element method (FEM) was used to analyze the performance of the hybrid BL-WRSM, and we compared its performance with BL-WRSM. Finally, prototypes were built with and without the PM-assistance, and experiments were conducted to demonstrate their performance.

로터 팁 간극이 초음속 터빈 성능에 미치는 영향에 대한 전산해석 연구 (Numerical Study of the Supersonic Turbine Rotor Tip Variation Effect on the Turbine Performance)

  • 박편구;정은환;김진한;이수용
    • 한국추진공학회:학술대회논문집
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    • 한국추진공학회 2006년도 제27회 추계학술대회논문집
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    • pp.382-386
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    • 2006
  • 초음속 충동형 터빈에 대하여 로터 팁 간극이 터빈 성능에 미치는 영향을 고찰하기 위하여 팁 간극이 변화된 터빈에 대하여 3차원 유동해석을 수행하였다. 계산 결과 팁 간극이 증가함에 따라 터빈의 효율이 감소하고 팁으로 유출되는 유량이 증가함을 확인하였으며 팁 간극에 의한 유동교란보다는 누설손실 의한 영향이 터빈성능감소에 더 큰 영향을 주는 것을 확인하였다.

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MPM을 이용한 고압전동기 운전중 상태 평가 (On-Line Assessment of High Voltage Motor Condition using the Motor Performance Monitor)

  • 김희동;공태식
    • 전기학회논문지
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    • 제57권9호
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    • pp.1589-1593
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    • 2008
  • The condition of a high voltage motor was monitored with the motor performance monitor (MPM) at the motor control center. The MPM detected defects in the rotor bar and end ring and input power according to motor and load conditions. The assessment of the condition of a coal pulverizer motor indicated it was clearly in good condition in terms of the rotor bars, over voltage, and motor performance. However, the side bands at frequency, 56.48 Hz indicated existence of rotor end-ring fault. The large torque ripple indicated abnormal operating conditions. After visual inspection, it has been observed that an impeller blade of the circulating water pump was broken off causing the irregular torque pattern.

10kW급 상반전 조류터빈의 설계와 성능에 관한 연구 (Design and Performance Evaluation of a 10kW Scale Counter-Rotating Tidal Turbine)

  • 황안둥;양창조
    • 한국유체기계학회 논문집
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    • 제17권1호
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    • pp.47-53
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    • 2014
  • This paper aims to present the design and performance evaluation of a counter-rotating tidal turbine using CFD and to compare its performance with single rotor. The device scale is 10kW and the rotating part consists of two rotors which rotate in opposite direction. Compared with conventional single rotor, the counter-rotating system shows higher power efficiency at high stream velocity but lower efficiency at low stream velocity. The added counter-rotated rotor together helps improve the energy absorption capacity but has influence on the upstream rotor that reduces its performance. In terms of power capture, the designed counter-rotating tidal turbine is more advantageous in high speed tidal condition.

고성능 복합재료 가요성 커플링에 관한 연구 (A Study of High Performance Composite Flexible Couplings)

  • 김필종;박일경;김근택;우경식
    • 한국복합재료학회:학술대회논문집
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    • 한국복합재료학회 2004년도 춘계학술발표대회 논문집
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    • pp.79-82
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    • 2004
  • The rotor drive system in rotor-craft carries out power transmission from powerplant to rotors and the drive shafts are fallen into misaligned condition by the vibration of engine and shafts and the deformation of supporting structures. The high performance flexible coupling accommodates these misalignments of drive shafts. In this study, we compare the performance of the metalic flexible coupling with the composite flexible coupling through analytic method to develop the high performance flexible coupling used in the rotor drive system of UAV tilt-rotor.

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