• 제목/요약/키워드: H-로터

검색결과 105건 처리시간 0.025초

차량진동 및 Rotor 내구특성을 고려한 Brake System 의 최적설계 (Optimal Design of Brake System considering Vehicle Vibration and Durability of Rotor)

  • 김봉수;김희열;김강욱;손영균;이동근;박관흠
    • 대한기계학회:학술대회논문집
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    • 대한기계학회 2001년도 춘계학술대회논문집A
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    • pp.764-769
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    • 2001
  • Brake-induced vibrations of a vehicle such as brake judder are determined by the excitation of brake torque variations and by their transfer to the driver's contact points via suspension, body and steering system. The formation of brake torque variation is mainly determined by static and dynamic disk thickness variations. The vibration transfer from the excitation by brake torque variation to the perception by the driver depends on the kinematic and dynamic behaviour of the components in the transfer path. Optimization of the judder performance can be achieved either by minimizing the excitation or by reduction of the judder sensitivity of the vehicle. In this paper, the optimization process of a front rotor is suggested to reduce brake judder considering the cooling performance of the rotor, the judder sensitivity of the vehicle and durability of the rotor.

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저속 고토오크 제로터 유압모터의 최적 이 끝 틈새를 갖는 제로터 설계 연구 (A Study on Gerotor Design with Optimum Tip Clearance for Low Speed High Torque Gerotor Hydraulic Motor)

  • 서종수;정한식;정효민
    • 동력기계공학회지
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    • 제10권4호
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    • pp.119-126
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    • 2006
  • Gerotor hydraulic motor is widely used in hydraulic systems due to its low speed, high torque output and compactness in rotational direct driving of a heavy weight. Gerotor is a Planar mechanism consisted of a pair of rotor and circular teeth of stator assembly which forms a closed space, so called a chamber. The motion of rotor relative to the circular tooth is produced by the pressure difference of hydraulic operating fluid between the adjacent chamber. As all active contact points of rotor and circular teeth are subjected to very high sliding friction, a reduction in the performance of the gerotor hydraulic motor can not be avoided. Therefore, the core design parameters of gerotor profile used in hydraulic motors is to minimize a friction force by high contact stresses. The analytical design method of gerotor profile, based on envelope of a family of curves, is proposed. In this study, the influence of the tip clearances on three critical contact points between rotor and circular teeth of stator assembly has been explored by experimental data in this paper. At the same time a improvement method to reduce the friction force is proposed and the tip clearances on three critical points for getting an optimum gerotor profile are also analyzed.

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대형 증기터빈 물유입에 의한 손상메커니즘 분석과 원상복구특성 연구 (Study on Damage Mechanism Analysis and Recovery Characteristic of the Large Scale Steam Turbine Cased by Water Induction)

  • 김두영;박광하;이봉희
    • 동력기계공학회지
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    • 제15권5호
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    • pp.22-29
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    • 2011
  • In this study, the damage mechanism of large scale steam turbine due to water induction was analyzed and recovery characteristics were reviewed. A turbine consists of the rotating rotor and the stationary casing, and the clearance between them is very small for the efficiency enhancement. If water induction, while relatively cold steam or water is introduced into turbine, occurs, the considerable humping is caused at the casing near the initial water induction point and that induces the rubbing between rotor and casing. Finally, it leads to the catastrophic failure. Bowed rotor has the different characteristics in the recovery depending on damage degree. The elastic deformation due to light rubbing is recovered by turning the rotor with 3 rpm under normal operation condition, but most plastic deformation due to rubbing deforms the local microstructure and that results in permanent deformation which could not be recovered under normal operation condition. Bowed rotor has diverse characteristics depending on the recovery method, and the method is empirical and needs the cutting edge technology. Careful recovery treatment of the rotor will eliminate the risks and secure the high quality rotor similar to new rotor. If any critical error is made during the recovery, the rotor would not be recovered permanently and it should be scrapped.

제올라이트 쉬트 담지 백금촉매의 제조 및 톨루엔 연소 특성 (Preparation of Pt Catalyst Supported on Zeolite Sheet and Its Performance of Toluene Combustion)

  • 김진배;임나래;김홍수;유윤종
    • 공업화학
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    • 제22권3호
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    • pp.323-327
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    • 2011
  • 원통형으로 성형된 zeolite sheet (제올라이트를 함유하는 세라믹 종이)는 VOC 제거를 위한 효과적인 흡착로터로서 사용될 수 있다. 본 연구에서는 ZSM-5가 함유된 zeolite sheet 지지체에 Pt를 담지한 후 톨루엔 연소 촉매 성능을 ${\gamma}-Al_2O_3$ 및 cordierite honeycomb 지지체에 담지된 Pt 촉매와 비교하였다. Pt/zeolite sheet 촉매는 $Pt/{\gamma}-Al_2O_3$ 또는 Pt/cordierite honeycomb 촉매에 비하여 톨루엔 연소반응에 높은 활성을 나타냈다. 한편, Pt/zeolite sheet 촉매를 상온에서 $NH_3-H_2O$ 증기로 전처리하면 zeolite sheet에 담지된 Pt 입자의 분산도가 향상되었으며, 톨루엔 연소 촉매 활성이 크게 증가하였다.

RANS 방정식을 이용한 HAWT 로터 블레이드의 회전 유동장 해석 (ROTATING FLOW ANALYSIS AROUND A HAWT ROTOR BLADE USING RANS EQUATIONS)

  • 김태승;이철;손창호;조창열
    • 한국전산유체공학회지
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    • 제13권2호
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    • pp.55-61
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    • 2008
  • The Reynolds-Averaged Navier-Stokes(RANS) analysis of the 3-D steady flow around the NREL Phase VI horizontal axis wind turbine(HAWT) rotor was performed. The CFD analysis results were compared with experimental data at several different wind speeds. The present CFD model shows good agreements with the experiments both at low wind speed which formed well-attache flow mostly on the upper surface of the blade, and at high wind speed which blade surface flow completely separated. However, some discrepancy occurs at the relatively high wind speeds where mixed attached and separated flow formed on the suction surface of the blade. It seems that the discrepancy is related to the onset of stall phenomena and consequently separation prediction capability of the current turbulence model. It is also found that strong span-wise flow occurs in stalled area due to the centrifugal force generated by rotation of the turbine rotor and it prevents abrupt reduction of normal force for higher wind speed than the designed value.

유전 알고리즘과 인공 신경망 기법을 이용한 무인항공기 로터 블레이드 공력 최적설계 (AERODYNAMIC DESIGN OPTIMIZATION OF UAV ROTOR BLADES USING A GENETIC ALGORITHM AND ARTIFICIAL NEURAL NETWORKS)

  • 이학민;유재관;안상준;권오준
    • 한국전산유체공학회지
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    • 제19권3호
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    • pp.29-36
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    • 2014
  • In the present study, an aerodynamic design optimization of UAV rotor blades was conducted using a genetic algorithm(GA) coupled with computational fluid dynamics(CFD). To reduce computational cost in making databases, a function approximation was applied using artificial neural networks(ANN) based on a radial basis function network. Three dimensional Reynolds-Averaged Navier-Stokes(RANS) solver was used to solve the flow around UAV rotor blades. Design directions were specified to maximize thrust coefficient maintaining torque coefficient and minimize torque coefficient maintaining thrust coefficient. Design variables such as twist angle, thickness and chord length were adopted to perform a planform optimization. As a result of an optimization regarding to maximizing thrust coefficient, thrust coefficient was increased about 4.5% than base configuration. In case of an optimization minimizing torque coefficient, torque coefficient was decreased about 7.4% comparing with base configuration.

화상 처리를 이용한 섬유 배향각 분포 측정에서 농도법과 카운트법의 정확도 비교 (Accuracy Comparison between Intensity Method and Count Method in Measurement of Planar Orientation of Fibers Using Image Processing)

  • 이상동;김혁;이동기;한길영;김이곤
    • 비파괴검사학회지
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    • 제18권5호
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    • pp.357-364
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    • 1998
  • 농도법과 카운트법에 의한 섬유 배향각 분포 측정의 정확도에 대해서 비교 검토하기 위하여, 섬유 종횡비와 면적비 및 섬유 배향 상태를 변화시켜 플로터로 섬유 배향 시뮬레이션 그림을 작도하여 섬유 배향 함수값을 구하였다. 이 섬유 배향 함수값을 시뮬레이션 그림에 대해 농도법과 카운트법으로 측정한 섬유 배향 함수값과 비교 검토하였다. 결국, 섬유 배향각 분포 측정의 정확도는 카운트법이 농도법보다 약 4% 정도 높게 나타남을 알 수 있었다.

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3MW급 IEC Wind Class IIa 풍력발전시스템 개발 (Development of 3MW Wind Turbine for IEC Wind Class IIa)

  • 이기학;이상일;우상우;오인규;박종포
    • 한국전산유체공학회:학술대회논문집
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    • 한국전산유체공학회 2011년 춘계학술대회논문집
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    • pp.236-239
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    • 2011
  • This paper introduces the design concepts and characteristics of WinDS3000$^{TM}$(TC IIa) which is a trade name of Doosan's 3MW offshore/onshore wind turbine. WinDS3000$^{TM}$(TC IIa) has been designed in consideration of high Reliability, Availability, Maintainability and Serviceability (RAMS) and low cost of electricity (CDE) for the TC IIa condition based on GL guideline. An integrated drive-train design with an innovative three-stage gearbox has been introduced to minimize nacelle weight of the wind turbine and to enhance a high reliability for transmission. A permanent magnet generator with full converter system has been introduced to get higher efficiency in partial load operation and grid-friendly system for both 50 Hz and 60 Hz. A pitch-regulated variable speed control system has been introduced to control wind turbine power while generator reaction torque can be adjusted almost instantaneously by the associated power electronics. The wind turbine has been also equipped with condition monitoring and diagnostic systems in order to meet maintainability requirements.

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유도전동기 로터바의 손상과 인버터 제어특성에 관한 연구 (A Study on The Broken Rotor Bars in Induction Motor and The Controll Characteristics in Inverter)

  • 김근웅;권중록;이잠재;최경수;이호석;장서건
    • 전력전자학회:학술대회논문집
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    • 전력전자학회 2001년도 전력전자학술대회 논문집
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    • pp.464-466
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    • 2001
  • The advantage of the squirrel cage induction motor is the brushless rotor. This advantage for operation and maintenance turns out to be a disadvantage for the detection of the cage rotor bar and endring defects, which means that the detection of cage faults is due to the measurement and analysis of only the stator input signals. The monitoring task in an inverter drive is complicated mainly because the voltage and current waveforms are nonsinusoidal and the high dv/dt values from fast switching inverterd distort the measurements. in this paper, we are going to discuss the detection method of broken rotor bar of squirrel cage induction motor by the motor current signal analysis(MCSA).

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체공성능 향상을 위한 확장날개 틸트로터 무인기의 제어법칙설계 (Control Law Design for a Tilt-rotor Unmanned Aerial Vehicle with a Nacelle Mounted WE (Wing Extension))

  • 강영신;박범진;조암;유창선
    • 제어로봇시스템학회논문지
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    • 제20권11호
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    • pp.1103-1111
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    • 2014
  • The results of control law design for a tilt-rotor unmanned aerial vehicle that has a nacelle mounted wing extension (WE) are presented in this paper. It consists of a control surface mixer, stability and control augmentation system (SCAS), hold mode for altitude / speed / heading, and a guidance mode for preprogram and point navigation which includes automatic take-off and landing. The conversion corridor and the control moments derivatives between the original tilt-rotor and its variant of the nacelle mounted WE were compared to show the effectiveness of the WE. The nacelle conversion of the original tilt-rotor starts when the airspeed is greater than 30 km/h but its WE variant starts at 0 km/h in order to reduce the drag caused by the high incidence angle of the WE. The stability margins of the inner loop are presented with the optimization approach. The outer loops for the hold mode are designed with trial and error methods with linear and nonlinear simulation. The main control parameter for altitude control of the helicopter mode is thrust command and it is transferred to the pitch attitude command in airplane mode. Otherwise, the control parameter for the speed of the helicopter mode is the pitch attitude command and it is transferred to the thrust command in airplane mode. Therefore the speed and altitude hold mode are coupled to each other and are engaged at the same time when an internal pilot engages any of the altitude or speed hold modes. The nonlinear simulation results of the guidance control for the preprogrammed mode and point navigation are also presented including automatic take-off and landing in order to prove the full control law.