Horizontal axle windmill and method for making wind-powered unit vane
A technology of wind turbines and horizontal axes, which is applied in the direction of wind turbines, wind power generation, wind turbines, etc. in the same direction as the wind, and can solve the problems of reducing the sweeping area of the wind rotor, increasing the impact, and reducing the safety of the blades, etc.
- Summary
- Abstract
- Description
- Claims
- Application Information
AI Technical Summary
Problems solved by technology
Method used
Image
Examples
Embodiment 1
[0045] Example 1: A wind turbine blade 3 with a length of 37m. In the design target, the root shape of the blade 3 is shown as A in Fig. 11, α is the installation angle of the blade root, and the top shape is shown in B in Fig. 11, β It is the installation angle of the top of the blade. When the wind wheel is running, the line connecting the centroid of each airfoil in the radial direction is a straight line and is completely in the radial direction. In the radial direction, 7 is the line connecting the centroid of each airfoil in the radial direction, and the installation angle of each section is at the design position. Considering the influence of the stiffness, aerodynamic load, inertial force and prestress of the blade 3 on the deformation, the connection line of the airfoil centers of the blade 3 (8 in Figure 12) is inclined forward about 5 degrees from the root to the top. The top installation angle β torsion angle increases by about 5 degrees, linearly changing from root...
Embodiment 2
[0046] Example 2: A wind turbine blade 3 with a length of 80m. In the design target, the difference between the root installation angle and the top installation angle of the blade 3 is -45 degrees. When the wind turbine is running, the connection between the center of each airfoil is straight and It is completely radial and the installation angle is in the design position. Considering the stiffness, aerodynamic load and inertial force of the blade 3, the connecting line of the center of each airfoil of the blade bends forward from the root to the top. The bending law is:
[0047] l = a ( y - y h y t - y h ) 2 ,
[0048] Among them: y is the radial coordinate of blade 3, a is a coefficient calculated according to the material characteristics of blade 3 and the shape of blade 3, y h Is the radial coordinate of the root of blade 3, y t Is the radial coordinate of the top of blade 3. The torsion angle distribution law of blade 3 is:
...
PUM
Login to View More Abstract
Description
Claims
Application Information
Login to View More 