• 제목/요약/키워드: Pitch Variation

검색결과 240건 처리시간 0.026초

전압원인버터를 이용한 계통연계형 풍력발전의 출력제어 모의 및 해석 (Modeling and Analysis of Control Scheme for Voltage Source Inverter Based Grid-connection of Wind Turbine)

  • 김슬기;김응상
    • 에너지공학
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    • 제12권2호
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    • pp.154-163
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    • 2003
  • 전력계통에 연계하기 위해서 풍력발전시스템은 계속해서 변하는 풍속에 응동하여 적정한 출력을 계통에 공급할 수 있을 뿐만 아니라, 연계되는 전력계통에서 허용될 수 있는 수준의 주파수와 전압크기를 갖는 출력을 제공할 수 있어야 하며, 이를 위해서는 풍력발전의 적절한 출력제어가 필수적으로 요구된다. 본 연구에서는 동기발전기가 전압원인버터로 구성된 AC-DC-AC 변환부를 거쳐 계통에 접속되는 계통연계형 풍력발전시스템의 출력제어 전략을 소개하며, 이를 전자기 과도현상 해석 프로그램인 PSCAD/EMTDC를 이용하여 모의하고 해석하였다. 블레이드를 통해 입력되는 풍속에 대하여 최대 에너지를 공급할 수 있도록 전압원인버터의 유효전력 출력제어가 이루어지며, 출력단 전압을 일정하게 유지하기 위한 무효전력 출력제어가 행해진다. 또한 60 Hz의 주파수 출력 및 고조파 저감을 위해 SPWM 스위칭 방식을 채택하였다. 풍속의 변동 및 부하의 변동에 대한 풍력발전시스템의 응동특성 및 출력변화를 모의하고 해석한다.

초정밀 이송테이블의 5 자유도 운동오차 측정 (Measurement of Five DOF Motion Errors in the Ultra Precision Feed Tables)

  • 오윤진;박천홍;황주호;이득우
    • 한국정밀공학회지
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    • 제22권11호
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    • pp.135-141
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    • 2005
  • Measurement of five DOF motion errors in a ultra precision feed table was attempted in this study. Yaw and pitch error were measured by using a laser interferometer and roll error was measured by using the reversal method. Linear motion errors in the vertical and horizontal directions were measured by using the sequential two point method. In this case, influence of angular motion errors was compensated by using the previously measured ones by the laser interferometer and the reversal method. The capacitive type sensors and an optical straight edge were used in the reversal method and the sequential two point method. Influence of thermal deformation on sensor jig was investgated and minimized by the periodic measurement according to the variation of room temperature. Deviation of gain between sensors was also compensated using the step response data. 5 DOF motion errors of a hydrostatic table driven by the linear motor werer tested using the measurement method. In the horizontal direction, measuring accuracies for the linear and angular motion were within ${\pm}0.02\;{\mu}m$ and ${\pm}0.04$ arcsec, respectively. In the vertical direction, they were within ${\pm}0.02{\mu}m$ and ${\pm}0.05$ arcsec. From these results, it was found that the introduced measurement method was very effective to measure 5 DOF motion errors of the ultra precision feed tables.

Analytical study on hydrodynamic motions and structural behaviors of hybrid floating structure

  • Jeong, Youn-Ju;Lee, Du-Ho;Park, Min-Su;You, Young-Jun
    • Ocean Systems Engineering
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    • 제3권1호
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    • pp.35-53
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    • 2013
  • In this study, a hybrid floating structure with cylinder was introduced to reduce the hydrodynamic motions of the pontoon type. The hybrid floating structure is composed of cylinders and semi-opened side sections to penetrate the wave impact energy. In order to exactly investigate the hydrodynamic motions and structural behavior of the hybrid floating structure under the wave loadings, integrated analysis of hydrodynamic and structural behavior were carried out on the hybrid floating structure. Firstly, the hydrodynamic analyses were performed on the hybrid and pontoon models. Then, the wave-induced hydrodynamic pressures resulting from hydrodynamic analysis were directly mapped to the structural analysis model. And, finally, the structural analyses were carried out on the hybrid and pontoon models. As a result of this study, it was learned that the hybrid model of this study was showed to have more favorable hydrodynamic motions than the pontoon model. The surge motion was indicated even smaller motion at all over wave periods from 4.0 to 10.0 sec, and the heave and pitch motions indicated smaller motions beyond its wave period of 6.5 sec. However, the hybrid model was shown more unfavorable structural behavior than the pontoon model. High concentrated stress occurred at the bottom slab of the bow and stern part where the cylinder wall was connected to the bottom slab. Also, the hybrid model behaved with the elastic body motion due to weak stiffness of floating body and caused a large stress variation at the pure slab section between the cylinder walls. Hence, in order to overcome these problems, some alternatives which could be easily obtained from the simple modification of structural details were proposed.

전산유체해석과 다구찌 방법을 연계한 공기 가열식 히터 시스템의 난방속효성 최적화에 관한 연구 (A Study on the Optimum Design of Warm-up rate in a Air-Heated Heater System by Using CFD Analysis and Taguchi Method)

  • 김민호
    • 한국자동차공학회논문집
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    • 제13권2호
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    • pp.72-82
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    • 2005
  • The objective of this paper is to describe the optimization of design parameters in a large-sized commercial bus heater system by using CFD(computational fluid dynamics) analysis and Taguchi method. In order to obtain the best combination of each control factor which results in a desired performance of heater system, the parameter design of the Taguchi method is adopted for the robust design considering the dynamic characteristic. The research activity may be divided into four phases. The first one is analyzing the problem, i.e., ascertaining the influential factors. In the second phase the levels were set in such a way that their variation would significantly influence the response. In the third phase the experimental runs were designed. In the final phase the planned runs were carried out numerically to evaluate the optimal combination of factors which is able to provide the best response. In this study, eight factors were considered for the analysis: one with two level and seven with three level combinations comprising the $L_{18}(2^1{\times}3^7)$ orthogonal array. The results of this study can be summarized as follows ; (i)The optimum condition of control factor is a set of <$A_2\;B_1\;C_3\;D_3\;E_1\;F_2\;G_3\;H_2$> where A is shape of the outer fin, B is pitch of the outer fin, C is height of the outer fin, D is the inner fin number, E is the inner fin height, F is length of the flame guide, G is diameter of the heating element and H is clearance between air guide and heating element. (ii)The heat capacity of heated discharge air under the optimum condition satisfies the equation y=0.6M w here M is a signal factor. (iii)The warm-up rate improves about three times, more largely as com pared with the current condition, which results in about 9.2minutes reduction.

베인과 블레이드 사이의 상대위치 변화에 따른 터빈 블레이드 표면에서의 열/물질전달 특성 (Effect of Relative Position of Vane and Blade on Heat/Mass Transfer Characteristics on Stationary Turbine Blade Surface)

  • 이동호;조형희
    • 유체기계공업학회:학술대회논문집
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    • 유체기계공업학회 2004년도 유체기계 연구개발 발표회 논문집
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    • pp.140-150
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    • 2004
  • In this study, the effect of relative position of the blade for the fixed vane has been investigated on blade surface heat transfer. The experiments were conducted in a low speed stationary annular cascade, and heat transfer of blade was examined for six positions within a pitch. Turbine test section has one stage composed of sixteen guide vanes and blades. The chord length of the tested blade is 150 mm and the mean tip clearance of the blade having flat tip is about $2.5\%$ of the blade chord. For the detailed mass transfer measurements on the blade surfaces, a naphthalene sublimation technique was used. The inlet flow Reynolds number is fixed to $1.5{\times}10^5$. Complex heat transfer characteristics are observed on the blade surface due to various flow characteristics, such as separation bubble, relaminarization, transition to turbulence and leakage vortices. The distributions of velocity and turbulence intensity change significantly with the relative position due to the blockage effect of the blade. This causes the variation of heat transfer patterns on the blade surface. The results show that the flow near the leading edge get highly disturbed and deflected toward the either side of the blade when the blade leading edge is positioned close to the trailing edge of the vane. Therefore, separation bubble disappears on the pressure side and overall heat transfer on the relaminarization region is increased. But, due to reduced tip gap flow at the upstream region, the effect of leakage flow on the upstream region of the blade surface is weakened. Thus, the heat transfer characteristics significantly change with the blade positions.

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주름높이의 변화를 고려한 판형열교환기의 완전발달유동 및 열전달 수치해석 (Numerical Simulation of the Fully Developed Flow and Heat Transfer of a Plate Heat Exchanger Taking into Account Variation in the Corrugation Height)

  • 모정하
    • 대한기계학회논문집B
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    • 제36권1호
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    • pp.1-8
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    • 2012
  • 본 연구에서는 주름높이가 고려된 판형열교환기의 완전발달유동 및 열전달특성을 수치적으로 해석하였다. 여러 개의 단위셀(5개 또는 7개)을 연결한 다중셀에 입구부와 출구부가 부착된 모델을 기본으로 P/H비 변화($2.0{\leq}P/H{\leq}4.0$)에 따른 모델에 대하여 수치해석을 수행하였다. 작동유체는 물이며, 수치조건은 쉐브론각 $20^{\circ}$, $300{\leq}Re{\leq}1,500$이다. 그리고 마찰인자는 $f=CRe^m$의 형태로, Colburn 계수는 $j=CRe^m$의 형태로 상관관계식을 제시하였다. 수치해석 결과 완전발달유동은 세 번째 셀부터 시작되었으며, 누셀트수는 P/H비가 작을수록 큰 값을 나타냈다.

MATLAB/Simulink에서 계통연계 풍력발전시스템의 특성해석에 대한 시뮬레이션 (Simulation for Characteristics Analysis of Grid-connected Wind Power Generation System on MATLAB/Simulink)

  • 노경수;안해준
    • 조명전기설비학회논문지
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    • 제22권8호
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    • pp.18-25
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    • 2008
  • 본 논문은 HATLAB/Simulink에서 계통연계 풍력발전시스템의 특성해석을 위한 모델링을 제안하여 시뮬레이션을 수행한다. 이를 위해 풍속의 변화에 따른 발전기의 출력제어를 위해 피치제어를 수행하며, 연계변압기의 결선방법에 따른 고장전류의 변화를 살펴봄으로 하여 연계변압기의 결선방법과 고장전류와의 상관관계를 제시하였다. 아울러 풍력발전시스템의 연계변압기 중성점접지방식이 고장전류에 미치는 영향을 살펴본다. 계통에서의 1선 지락고장에 대해 연계변압기의 4가지 결선방식의 차이에 따른 고장전류, 전압 및 발전기의 특성 변화를 확인할 수 있었으며 중성점 접지방식의 차이에 따른 고장전류의 변화를 확인하였다. 사례연구를 통하여 제안한 Simulink에서의 시뮬레이션 모델의 효용성을 입증하였다.

LED 백라이트 설계에서 입광부처리에 따른 휘도분포의 광학적 해석 (Study on Luminance Characteristics in a Design of LED Backlight by the Light-Entering Face Treatment)

  • 한정민;김병용;김종연;김종환;김영환;이상극;옥철호;강동훈;서대식
    • 한국전기전자재료학회:학술대회논문집
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    • 한국전기전자재료학회 2007년도 하계학술대회 논문집 Vol.8
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    • pp.429-429
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    • 2007
  • In this study, it was investigated about the variation of luminance properties in LED backlight with geometrical shape such as prism or lens shape on the light-entering face. Generally, LED light source has the loss in backlight system because it has horizontal direction light. PMMA(Poly-Methyl-Meta-Acrylate) is used LGP(Light-Guide-Plate) in conventional backlight system. PMMA has low refraction angle. so that. horizontal direction light was not used in backlight system. The addition of geometrical shape in light-entering face in LGP improves the luminance characteristics because it prevents horizontal direction light generation in light-entering-face. Prism or lens shape in same pitch disposition was almost same without these treatment such as the value of 1% rising. Besides. It is particular that the gap of these shape such as the value of 0.407~0.22mm prevents horizontal direction light, so then it contributes luminance rising at 5.6%.

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고정된 터빈 블레이드의 베인에 대한 상대위치 변화가 끝단면 및 슈라우드의 열/물질전달 특성에 미치는 영향 (Effect of Vane/Blade Relative Position on Heat/Mass Transfer Characteristics on the Tip and Shroud for Stationary Turbine Blade)

  • 이동호;조형희
    • 대한기계학회논문집B
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    • 제30권5호
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    • pp.446-456
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    • 2006
  • The effect of relative position of the stationary turbine blade for the fixed vane has been investigated on blade tip and shroud heat transfer. The local mass transfer coefficients were measured on the tip and shroud fur the blade fixed at six different positions within a pitch. A low speed stationary annular cascade with a single turbine stage was used. The chord length of the tested blade is 150 mm and the mean tip clearance of the blade having flat tip is 2.5% of the blade chord. A naphthalene sublimation technique was used for the detailed mass transfer measurements on the tip and the shroud. The inlet flow Reynolds number based on chord length and incoming flow velocity is fixed to $1.5{\times}10^5$. The results show that the incoming flow condition and heat transfer characteristics significantly change when the relative position of the blade changes. On the tip, the size of high heat/mass transfer region along the pressure side varies in the axial direction and the difference of heat transfer coefficient is up to 40% in the upstream region of the tip because the position of flow reattachment changes. On shroud, the effect of tip leakage vortex on the shroud as well as tip gap entering flow changes as the blade position changes. Thus, significantly different heat transfer patterns are observed with various blade positions and the periodic variation of heat transfer is expected with the blade rotation.

나노미터 영역 길이 측정 위한 미터 소급성을 갖는 원자간력 현미경 개발 (Development of a Metrological Atomic Force Microscope for the Length Measurements of Nanometer Range)

  • 김종안;김재완;박병천;엄태봉;홍재완
    • 한국정밀공학회지
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    • 제21권11호
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    • pp.75-82
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    • 2004
  • A metrological atomic force microscope (M-AFM) was developed fur the length measurements of nanometer range, through the modification of a commercial AFM. To eliminate nonlinearity and crosstalk of the PZT tube scanner of the commercial AFM, a two-axis flexure hinge scanner employing built-in capacitive sensors is used for X-Y motion instead of PZT tube scanner. Then two-dimensional displacement of the scanner is measured using two-axis heterodyne laser interferometer to ensure the meter-traceability. Through the measurements of several specimens, we could verify the elimination of nonlinearity and crosstalk. The uncertainty of length measurements was estimated according to the Guide to the Expression of Uncertainty in Measurement. Among several sources of uncertainty, the primary one is the drift of laser interferometer output, which occurs mainly from the variation of refractive index of air and the thermal stability. The Abbe error, which is proportional to the measured length, is another primary uncertainty source coming from the parasitic motion of the scanner. The expanded uncertainty (k =2) of length measurements using the M-AFM is √(4.26)$^2$+(2.84${\times}$10$^{-4}$ ${\times}$L)$^2$(nm), where f is the measured length in nm. We also measured the pitch of one-dimensional grating and compared the results with those obtained by optical diffractometry. The relative difference between these results is less than 0.01 %.