• 한국신재생에너지학회:학술대회논문집
• /
• 한국신재생에너지학회 2009년도 춘계학술대회 논문집
• /
• pp.495-499
• /
• 2009

본 논문에서는 상호역회전 풍력발전기와 New Yaw System 실증시험에 대하여 제시한다. 상호역회전 풍력발전기는 공기의 유동을 가진 운동에너지의 공기역학적(aerodynamic) 특성을 이용하여 동일한 바람방향에 대해 상호 반대방향으로 회전하는 Front Blade와 Rear Blade를, Generator의 Rotor와 Stator에 각각 결합 형성한 것으로, Generator와 Dual Blade의 회전력이 원심력이 아닌 구심력으로 변환되어 무게중심이 균형을 이루게 한다. 이렇게 변환된 구심력은 회전구동부분의 편마모 현상, 소음발생 현상 및 불균형 톨크 발생 현상 감소효과가 공히 구현되도록 하여 풍력발전기의 구조적 안정성 및 발전효율 증대효과를 얻을 수 있도록 한 기술이다.

• 대한기계학회논문집A
• /
• 제35권11호
• /
• pp.1407-1413
• /
• 2011

소형풍력발전시스템의 복합재 블레이드에 대한 실규모 구조시험 및 이를 모사한 구조해석을 통하여 설계 타당성을 검증하였다. 먼저 IEC 61400-2 에 규정된 설계 요구조건의 만족을 위하여 정격 풍속 및 IEC 61400-2 Case H 의 최악 조건에 대한 구조해석을 수행하고 이를 통하여 적층 순서 및 적층 두께를 결정하였다. 또한 이러한 구조해석의 타당성 검증을 위하여 IEC 61400-23 에 따라 구조해석과 동일한 하중조건에서의 실규모 구조시험을 실시하였다. 이러한 실규모 구조시험을 통한 구한 블레이드의 하중-변위 선도 및 표면의 변형률 특성을 이용하여 블레이드의 구조적 안전성을 평가하였다.

• 대한기계학회논문집A
• /
• 제36권1호
• /
• pp.117-124
• /
• 2012

본 논문에서는 유한요소법을 이용하여 블레이드에서 발생하는 동력을 발전기로 전달하는 체결부에 대한 연구를 수행하였다. 블레이드 체결부의 유한요소 모델을 수립하기 위하여 실험적 모드해석을 이용하여 각 부품의 고유진동수 및 고유모드를 추출하였으며, 사용프로그램인 ANSYS를 이용한 모드해석을 통하여 추출된 유한요소 모델의 고유진동수와 고유모드 비교를 통하여 모델을 검증하였다. 검증된 유한요소 모델을 이용하여 정격풍속 상태와 한계풍속 상태에서 응력해석을 수행하였으며, 해석 시 작동상태의 경계조건과 중력 및 바람에 의한 하중이 고려되었다.

• 한국항공우주학회지
• /
• 제39권3호
• /
• pp.201-209
• /
• 2011

NREL Phase VI 수평축 풍력터빈 주위의 3차원 유동에 대하여 미끄럼 격자 기법을 사용한 비정상 RANS 해석을 수행하였다. 블레이드/타워의 간섭영향을 해석하기 위하여 로터단일과 로터/타워/나셀의 2가지 해석 모델을 구축하였다. 로터/타워/나셀의 해석 결과를 NREL의 실험데이터와 비교하여 CFD 해석모델의 유용성을 확인하였다. 두 모델에 의한 해석 결과의 비교를 통하여 비록 상풍형 풍력터빈으로서 작기는 하지만 타워/나셀의 영향이 확실히 나타나는 것을 확인하였다. 다른 가시화 결과와 토크를 포함한 적분 공력하중 등도 구축한 CFD 모델의 비정상 유동해석 능력이 효과적임을 보여주고 있다.

• 한국해양공학회지
• /
• 제32권3호
• /
• pp.202-207
• /
• 2018

This paper presents the efficiency of a floating vertical axis wind turbine with variable-pitch. A model was designed to use the lift force and drag force for blades with various pitch angles. The blade's pitch angle is controlled by the stopper. To validate the efficiency of the wind turbine discussed in this paper, a model test was carried out through a single model efficiency experiment and wave tank experiment. The parameters of the single model efficiency experiment were the wind speed, electronic load, and pitch angle. The wave tank experiment was performed using the most efficient pitch angle from the results of the single model efficiency experiment. According to the results of the wave tank experiment, the surge and pitch motion of a structure slightly affect the efficiency of a wind turbine, but the heave motion has a large effect because the heights of the wind turbine and wind generator are almost the same.

• Structural Engineering and Mechanics
• /
• 제28권1호
• /
• pp.107-127
• /
• 2008

Wind turbine blades are increasing in magnitude without a proportional increase of stiffness for which reason geometrical and inertial nonlinearities become increasingly important. Often these effects are analysed using a nonlinear truncated expansion in undamped fixed base mode shapes of a blade, modelling geometrical and inertial nonlinear couplings in the fundamental flap and edge direction. The purpose of this article is to examine the applicability of such a reduced-degree-of-freedom model in predicting the nonlinear response and stability of a blade by comparison to a full model based on a nonlinear co-rotating FE formulation. By use of the reduced-degree-of-freedom model it is shown that under strong resonance excitation of the fundamental flap or edge modes, significant energy is transferred to higher modes due to parametric or nonlinear coupling terms, which influence the response and stability conditions. It is demonstrated that the response predicted by such models in some cases becomes instable or chaotic. However, as a consequence of the energy flow the stability is increased and the tendency of chaotic vibrations is reduced as the number of modes are increased. The FE model representing the case of infinitely many included modes, is shown to predict stable and ordered response for all considered parameters. Further, the analysis shows that the reduced-degree-of-freedom model of relatively low order overestimates the response near resonance peaks, which is a consequence of the small number of included modes. The qualitative erratic response and stability prediction of the reduced order models take place at frequencies slightly above normal operation. However, for normal operation of the wind turbine without resonance excitation 4 modes in the reduced-degree-of-freedom model perform acceptable.

• 한국정밀공학회지
• /
• 제33권11호
• /
• pp.911-918
• /
• 2016

A conical roll-shaping process was proposed for fabrication of a metallic spiral blade applied to a small-scale wind turbine system. A spiral blade has continuously different curvatures, with a range of 100 to 350 mm radius. To fabricate this complex shape, we developed a conical roll-shaping process having two main conical rollers for feeding a blank sheet, and two cylindrical side rollers for control of local bending. For clear understanding of the process parameters, numerical analyses were conducted using a commercial code, Pam-Stamp. This study optimized the effects of process parameters, such as gap and angle between the main rollers and side rollers, and also the movement of side rollers. In order to increase the forming efficiency, a central rotation point was also calculated by the analytical approach. This developed rolling process can thus be utilized in a sheet metal forming process for obtaining spirally curved sheet metal shapes.

• 대한기계학회:학술대회논문집
• /
• 대한기계학회 2001년도 추계학술대회논문집B
• /
• pp.746-751
• /
• 2001

We used a cylindrical model which simulates turbine blade leading edge to investigate the effects of free-stream turbulence intensity and blowing ratio on film cooling of turbine blade leading edge. Tests are carried out in a low-speed wind tunnel on a cylindrical model with three rows of injection holes. Mainstream Reynolds number based on the cylinder diameter was $7.1\times10^4$. Two types of turbulence grid are used to increase a free-stream turbulence intensity. The effect of coolant blowing ratio was studied for various blowing ratios. For each blowing ratios, wall temperatures around the surface of the test model are measured by thermocouples installed inside the model. Results show that blowing ratios have small effect on spanwise-averaged film effectiveness at high free-stream turbulence intensity. However, an increase in free-stream turbulence intensity enhances significantly spanwise-averaged film effectiveness at low blowing ratio.

• Smart Structures and Systems
• /
• 제24권3호
• /
• pp.379-390
• /
• 2019

In this research, we propose an energy harvesting structure with a flexible blade element vibrating at its first mode to maximize the power output of the piezoelectric material. For this purpose, a piezoelectric patch was attached on the blade element used in a small-scale wind turbine, and air load was applied with a suitable angle of attack in the stall zone. The aerodynamic load created by air excitation vibrates the blade element in its first natural frequency and maximizes the voltage output of the piezoelectric patch. The variation of power outputs with respect to electrical resistance, air speed, and extra mass is experimentally investigated for various cases. An analytical model is constituted using a single-mode blade element with piezoelectric patch dynamics, and the power outputs of the obtained model are compared with experimental results.

• 대한기계학회논문집
• /
• 제17권12호
• /
• pp.3148-3165
• /
• 1993

A cascade wind tunnel test for a turbine nozzle, which was designed for a small turbo jet engine in a previous study, has been conducted to evaluate its aerodynamic performance and losses. The large-scale blades were based on the mid-span profile of the nozzle. Oil film flow structure, and then 3-dimensional velocity components were measured in the flow passage with a 5-hold pressure probe, in addition to turbulent intensities at mid-span of cascade exit using a hot-wire anemometer. From this study, 3-dimensional growth of horseshoe and passage vortices in the downstream direction was clearly understood with near-wall flow phenomena. In addition, secondary flow and losses associated with the blade configuration were obtained in detail.