• Title/Summary/Keyword: Aerodyanmic Design

Search Result 2, Processing Time 0.015 seconds

Aerodynamic and Structural Design on Small Wind Turbine Blade Using High Performance Configuration and E-Glass/Epoxy-Urethane Foam Sandwich Composite Structure (고성능 형상 및 유리섬유/에폭시-우레탄 샌드위치 구조를 사용한 소형 풍력발전 블레이드의 공력 및 구조설계)

  • Chang-Duk Kong;Jo-Hyug Bang
    • Journal of the Korean Society of Propulsion Engineers
    • /
    • v.8 no.1
    • /
    • pp.70-80
    • /
    • 2004
  • This study proposes a development result for the 1-kW class small wind turbine system, which is applicable to relatively low wind speed regions like Korea and has the variable pitch control mechanism. In the aerodynamic design of the wind turbine blade, parametric studies were carried out to determine an optimum aerodynamic configuration which is not only more efficient at low wind speed but whose diameter is not much larger than similar class other blades. A light composite structure, which can endure effectively various loads, was newly designed. In order to evaluate the structural design of the composite blade, the structural analysis was peformed by the finite element method. Moreover both structural safety and stability were verified through the full- scale structural test.

A Numerical Method & Experiments for the Aerodynamic Design of High Performance 2-Stage Axial Flow Fans (고성능 2단 축류송풍기의 공력설계를 위한 수치해석 및 실험에 관한 연구)

  • Cho, Jinsoo;Han, Cheolhui;Cho, Leesang
    • Transactions of the Korean Society of Mechanical Engineers B
    • /
    • v.23 no.8
    • /
    • pp.1048-1062
    • /
    • 1999
  • A numerical method and experiments for the aerodynamic design of high performance two-stage axial flow fans was carried out. A vortex ring element method used for the aerodynamic analysis of the propellers was extended to the fan-duct system. Fan Performance and velocity profiles at the fan inlet and outlet are compared with experimental data for the validations of numerical method. Performance test was done based on KS B 6311(testing methods for turbo-fans and blowers). The velocity profile was obtained using a 5-hole pitot tube by the non-nulling method. The two stage axial flow fan configurations for the optimal operation conditions were set by using the experimental results for the single rotating axial flow fan and the single stage axial flow fan. The single rotating axial flow fan showed relatively low efficiency due to the swirl velocities behind rotor exit which produced pressure losses. In contrast, the single stage and the two-stage axial flow fans showed performance improvements due to the swirl velocity reduction by the stator. The peak efficiency of the two stage axial flow fan was improved by 21% and 6%, compared to the single rotating axial flow fan and the single stage axial flow fan, respectively.