A large thickness blunt trailing edge airfoil blade of a large wind turbine

A technology of airfoil blades and large thickness, which is applied in wind turbines, wind turbine components, engines, etc. It can solve the problems of low wind energy utilization rate and heavy structure weight, and achieve the reduction of self-weight, increase of static stiffness, and improvement of blade structure efficiency effect

Active Publication Date: 2015-09-02
GUODIAN UNITED POWER TECH
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] The technical problem to be solved by the present invention is to provide a large-thickness blunt trailing edge airfoil blade of a large-scale fan, so that its structural rigidity is high, the weight is reduced, and the comprehensive performance of the fan is improved, thereby overcoming the existing structure with heavy weight and low utilization rate of wind energy lack of

Method used

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  • A large thickness blunt trailing edge airfoil blade of a large wind turbine
  • A large thickness blunt trailing edge airfoil blade of a large wind turbine
  • A large thickness blunt trailing edge airfoil blade of a large wind turbine

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Embodiment Construction

[0017] refer to figure 1 , figure 2 , the present invention provides a blade airfoil with a relative thickness of 50% (named UP50). The profile line 3 and the pressure surface profile line 4 are composed of the front edge 1 is a circular arc, the front edge 1 is respectively connected with the suction surface profile line 3 and the pressure surface profile line 4, the curvature at the connection point is continuous, and the end of the suction surface profile line 3 11 is connected with the end 13 of the pressure surface profile line 4 to form the trailing edge 2.

[0018] first of all, yes figure 1 The names of the various parts are defined as follows:

[0019] 1. Middle arc 10: Make a series of inscribed circles of suction surface profile 3 and pressure surface profile 4 in the airfoil, and the line connecting the centers of these inscribed circles is called the center arc 10 of the airfoil.

[0020] 2. Chord length: the connecting line between the front and rear ends of...

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Abstract

The invention relates to a big-thickness blunt trailing edge airfoil-shaped blade for a large-scale blower. The outer contour of the cross section of the blade root part of the blade is divided into a front edge, a trailing edge, a suction surface molded line and a pressure surface molded line, wherein the distance from the front edge to the trailing edge is the chord length; the maximum thickness of the cross section is 50.0% to 55.0% of the chord length; the distance from the part with the maximum thickness to the front edge is 30% to 35% of the chord length; the maximum camber of the cross section is 0.5% to 1.5% of the chord length; the distance from the part with the maximum camber to the front edge is 85% to 95% of the chord length; the radius of the front edge is 25.0% to 35.0% of the chord length; the thickness of the end surface of the trailing edge is 10% to 14% of the chord length. The airfoil section creates a pioneer of special airfoil sections, with the relative thickness larger than 40%, of domestic wind turbines, and the application of the airfoil section not only enhances the static rigidity of the blade, but also reduces the structural weight, and lays an import technical foundation for the development of large-scale high-efficient and low-cost wind turbines.

Description

technical field [0001] The invention relates to the field of wind power generation, in particular to a large thickness blunt trailing edge airfoil blade of a large fan. Background technique [0002] As energy and environmental problems become more and more prominent, people pay more and more attention to the abundant, pollution-free and renewable wind energy, and the development of wind power is particularly rapid. Regardless of whether it is for onshore or offshore wind turbines, the capacity of the unit is showing an increasing trend. Correspondingly, the length of the blade, which is a key component, has also increased from about 20 meters (1 MW unit) a few years ago to About 60 meters (5 MW units) and even the current maximum of about 75 meters (10 MW units). However, as the length of the blade increases, the flexibility increases, and the corresponding structural rigidity is greatly reduced, which weakens its ability to resist the influence of various external loads, a...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): F03D11/00
CPCY02E10/722Y02B10/30
Inventor 周文明代海涛刘丹
Owner GUODIAN UNITED POWER TECH
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