• Title/Summary/Keyword: V-shape Blade

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Structural analysis of horizontal axis wind turbine blade

  • Tenguria, Nitin;Mittal, N.D.;Ahmed, Siraj
    • Wind and Structures
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    • v.16 no.3
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    • pp.241-248
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    • 2013
  • The wind turbine blade is a very important part of the rotor. Extraction of energy from wind depends on the design of blade. In this work, the analysis is done on a blade of length 38.95 m which is designed for V82-1.65 MW horizontal axis wind turbine (supplied by Vestas). The airfoil taken for the blade is NACA 634-221 which is same from root to tip. The analysis of designed blade is done in flap-wise loading. Two shapes of the spar are taken, one of them is of square shape and the other one is combination of square and cross shape. The blade and spar are of the same composite material. The Finite element analysis of designed blade is done in ANSYS. This work is focused on the two segments of blade, root segment and transition segment. Result obtained from ANSYS is compared with the experimental work.

A Study on the Wear of Rotary Blades (로타리 경운날의 마모에 관한 연구)

  • Choi, S.I.;Kim, J.H.;Lee, Y.K.
    • Journal of Biosystems Engineering
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    • v.18 no.1
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    • pp.15-20
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    • 1993
  • Wearness has been a major failure criterion in Korean-made rotary blade. However, few studies have been conducted to improve it. In this study, the fundamental data obtained from the measurement of wearness and failure of rotary blade were analyzed to provide a guideline for the design of rotary blades. For the straight part(about 20-23 em from bolt hole) from the bolt hole to bending point of rotary blade, modifications were proposed for improvements, however, for the portion from bending point to tip was made no design recommendations because the failure behavior of that portion was difficult to analyze with the experimental data. The results are summarized as follows. 1. The current V-shape section has to be moved about 5 em toward the bending point of rotary blade. 2. The section modulus at the portion about 5-7 em distant from bolt hole has to be increased about 15-20 %. 3. The V-shape section has to be changed into U-shape to reduce the on account of recieving initial stress in blades. 4. The radius of curvature of the neck(the portion about 5-7 cm apart from bolt hole) has to be made larger to decrease the stress concentration.

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An Experimental Study on the Vibrational Characteristics of the Rotor Blade with Fiber Reinforced Plastics (복합재료 FRP로 제작된 Rotor Blade 진동특성 분석에 관한 실험적 연구)

  • Paik, J.S.;Lee, K.S.;Park, J.V.;Lee, J.T.;Son, C.Y.
    • Transactions of the Korean Society for Noise and Vibration Engineering
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    • v.15 no.11 s.104
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    • pp.1232-1240
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    • 2005
  • The purpose of this paper is that investigates the dynamic behavior characteristic of W.T.S (wind turbine system) and carries out the evaluation analysis during operating W.T.S. To investigate the dynamic behavior characteristic of W.T.S, the experiments to measure vibration of the blade from the attached accelerometer on the flap and edge section of the blade that is one of the most important elements of dynamic characteristic of W.T.S are performed. Natural frequency and mode shape are calculated with commercial program ( ANSYS) using the measured vibration acceleration that receives the signal with F.F.T Analyzer from the accelerometer For validation of these experiments, the finite element analysis is performed with commercial F.E.M program (ANSYS) on the basis of the natural frequency and mode shape. The results indicate that experimental values have good agreements with the finite element analysis.

A Study of Wind Turbine by Using ANSYS Program (ANSYS 프로그램을 이용한 풍력발전에 관한 연구)

  • Lee, Dal-Ho;Park, Jung-Cheul
    • The Journal of Korea Institute of Information, Electronics, and Communication Technology
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    • v.11 no.5
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    • pp.565-571
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    • 2018
  • This paper designed the main blade in V-shape and tried to identify the design conditions by changing the main blade number and sub-blade number. Power output and power coefficient increased as main blade number increased. Sample 2 shows a 50% increase in power output compared to sample1. Sample 3 and sample4 increased by 92.8% and 114.7%, respectively. Sample 2 shows a 38.4% increase in power coefficient compared to sample1. Sample 3 and sample4 increased by 92.3% and 107.7%, respectively. Power output and power coefficient increased as sub-blade number increased. Sample 6 shows a 33.3% increase in power output compared to sample 5 and Sample 7 increased by 42.1%. Compared to sample5, efficiency increased by 35.3% for sample 5 and 47.1% for sample 7. The highest power output and power coefficient were measured when main blade and sub-blade were each 30 number. Sample 8 increased power output by 5.6% and power efficiency by 3.7% compared to sample 4. Compared to sample 7, sample 8 increased power efficiency by 12% and power output by 17.3%.

Optimization of Stacking Line and Blade Profile for Design of Axial Flow Fan Blade (중첩선과 단면형상을 고려한 축류 송풍기 날개의 최적설계)

  • Samad, Abdus;Lee, Ki-Sang;Jung, Sang-Ho;Kim, Kwang-Yong
    • 한국전산유체공학회:학술대회논문집
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    • 2008.03b
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    • pp.420-423
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    • 2008
  • This present work is to find optimum design of a NACA65 axial fan blade with weighted average surrogate model. The numerical analysis by Reynolds-average Navier-Stokes equations with shear stress turbulence(SST) is discretized by finite volume approximations and solved on hexahedral grids for flow analysis. The blade aerodynamic shape is modified by six design variables for the optimization. The blade profile as well as stacking line is modified to enhance blade total efficiency. Six design variables, airfoil maximum camber, maximum camber location, leading edge radius, trailing edge radius, lean angle at 50% span and lean angle at 100% span, are selected for blade profile to enhance the total efficiency. The PBA model which is basically weighted average of the basis surrogates is used to find the optimal design in the design space from the constructed response surface model for the objective function. By the optimization, the total efficiency is increased by 1.4%.

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A comparative study of early leaf development in the Viola albida complex

  • CHOI, Yong Kuk;WHANG, Sung Soo
    • Korean Journal of Plant Taxonomy
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    • v.49 no.1
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    • pp.1-7
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    • 2019
  • Early leaves within the Viola albida complex were investigated by scanning electron microscopy in order to determine the morphological segments during morphogenesis. The early leaf development of V. albida var. albida could be morphologically divided into the eight stages in the following order: I, the initiation of shoot germination; II, the conical growth directionally of the leaf; III, the adaxial and abaxial formation of the leaf; IV, the initiation of the stipule; V, the formation of a transitional zone between the leaf blade and petiole; VI, the expansion of the upper part of the leaf blade; VII, the formation of almost all parts of the early leaf; VIII, the early simple leaf. Viola albida var. takahashii differs from V. albida var. albida by additional stages, i.e., V-1, the initiation of the first lateral lobe at the both lateral parts of the leaf after the stage V and an early lobed leaf. Viola albida var. chaerophylloides is also distinguished from two taxa by two developmental features, V-2, the initiation of a second lateral lobe below of the first lateral lobe, and an early palmately compound leaf. These findings suggest that the Viola albida complex would be in the process of peramorphosis, showing developmental changes in a chain of events, leading to a different leaf shape. These data would also be useful for isolating genes that give rise to different leaf morphogenesis outcomes among the taxa in the Viola albida complex.

A study on design and aerodynamic characteristics of a spiral-type wind turbine blade (스파이럴형 풍력터빈 블레이드의 설계 및 공력특성에 관한 연구)

  • Lu, Qian;Li, Qiang;Kim, Yoon-Kee;Kim, Kyung-Chun
    • Journal of the Korean Society of Visualization
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    • v.10 no.1
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    • pp.27-33
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    • 2012
  • This paper describes a new design of small-scale horizontal wind blade, called spiral wind turbine blade. Theoretical and numerical approaches on the prediction of aerodynamic performance of the blade have been conducted. A theoretical equation is successfully derived using the angular momentum equation to predict aerodynamic characteristics according to the design shape parameters of spiral blade. To be compared with the theoretical value, a numerical simulation using ANSYS CFX v12.1 is performed on the same design with the theoretical one. Large scale tip vortex is captured and graphically presented in this paper. The TSR-$C_p$ diagram shows a typical parabolic relation in which the maximum efficiency of the blade approximately 25% exists at TSR=2.5. The numerical simulation agrees well with that of the theoretical result except at the low rotational speed region of 0~20 rad/s.

A Study of Vertical Axis Wind Turbine by Simulation (시뮬레이션을 통한 수직축 풍력발전에 관한 연구)

  • Park, Jung-Cheul;Won, Woo-Yeon
    • The Journal of Korea Institute of Information, Electronics, and Communication Technology
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    • v.11 no.3
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    • pp.241-245
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    • 2018
  • This paper designed the main blade in V-shape and tried to identify the best design conditions by changing the main blade angle and wind speed. When the main blade open angle was maintained at $120^{\circ}$ and the sample2 with an angle changed by $30^{\circ}$ was compared with the sample3 changed by $60^{\circ}$, the power output of sample2 was 3.8[kW], the power coefficient was 0.12, and the power output of sample3 was 6.0[kW], the power coefficient was measured as 0.18. So the power output of sample 3 was 58% higher than that of sample2, and the power coefficient was increased by 50%. The power coefficient was 0.18 and the wind speed was changed to 10[m/s] at 6.0[kW] at wind speed of 7[m/s] by fixing main blade open angle of $120^{\circ}$ and angle of $60^{\circ}$. The output was measured at 7.7[kW] and the power coefficient at 0.23. When the wind speed was high, the power output increased by 28% and the power coefficient increased by 83%. Also, sample4 was 103% higher in output and 92% more in efficiency than sample2.

Blade Type Field Vs Probe for Evaluation of Soft Soils (연약지반 평가를 위한 블레이드 타입 현장 전단파 속도 프로브)

  • Yoon, Hyung-Koo;Lee, Chang-Ho;Eom, Yong-Hun;Lee, Jong-Sub
    • Journal of the Korean Geotechnical Society
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    • v.23 no.12
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    • pp.33-42
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    • 2007
  • The assessment of shear wave velocity($V_s$) in soft soils is extremely difficult due to the soil disturbances during sampling and field access. After a ring type field $V_s$ probe(FVP) has been developed, it has been applied at the southern coastal area of the Korean peninsular. This study presents the upgraded FVP "blade type FVP", which minimizes soil disturbance during penetration. Design concerns of the blade type FVP include the tip shape, soil disturbance, transducers, protection of the cables, and the electromagnetic coupling between transducers and cables. The cross-talking between cables is removed by grouping and extra grounding of the cables. The shear wave velocity of the FVP is simply calculated by using the travel distance and the first arrival time. The large calibration chamber tests are carried out to investigate the disturbance effect due to the penetration of FVP blade and the validity of the shear waves measured by the FVP. The blade type FVP is tested in soils up to 30m in depth. The shear wave velocity is measured every 10cm. This study suggests that the upgraded blade type FVP may be an effective device for measuring the shear wave velocity with minimized soil disturbance in the field.

Shape Optimization of Impeller Blades for Bidirectional Axial Flow Pump (양방향 축류펌프용 임펠러 블레이드의 형상최적설계)

  • Baek, Seok Heum;Jung, Won Hyuk;Kang, Sangmo
    • Transactions of the Korean Society of Mechanical Engineers B
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    • v.36 no.12
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    • pp.1141-1150
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    • 2012
  • This paper describes the shape optimization of impeller blades for an anti-heeling bidirectional axial flow pump used in ships. In general, a bidirectional axial pump has efficiency much lower than that of a classical unidirectional pump because of the symmetry of the blade type. In this study, by focusing on a pump impeller, the shape of the blades is redesigned to develop a bidirectional axial pump with higher efficiency. The commercial code employed in this simulation is CFX v.13. The CFD result of the pump torque, head, and hydraulic efficiency was compared. The orthogonal array (OA) and analysis of variance (ANOVA) techniques and surrogate-model-based optimization using orthogonal polynomials are employed to determine the main effects and their optimal design variables. According to the optimal design, we confirm an effective design variable for impeller blades and explain the optimal solution as well as the usefulness of satisfying the constraints of the pump torque and head.