A Thick Airfoil Family of Large Wind Turbine Blades

Abstract

The invention belongs to the field of design of horizontal axis wind power wings, and in particular, relates to a thick wing group of a large turbine blade. The thick wing group comprises eight wings with relative thicknesses of 0.35, 0.40, 0.45, 0.50, 0.55, 0.60, 0.65 and 0.70; the eight wings all have thicker blunt tail edges, and are suitable for the inner side and the root part of an above-MW-grade large turbine blade working under high reynolds number; the thick wing group is higher in rise coefficient, lift-to-drag ratio and stall attack angle compared with a traditional contrast wing, so that higher rise and torque are provided to the blade, the start air speed of a turbine is lower, the power coefficient is higher, and the output power is higher; the designed larger attack angle facilitates reduction of the twisting angle of the blade, and facilitates the structural design of the blade and the rigidity, strength and manufacturing of a blade girder, so that the turbine blade of the thick wing group is lighter; and meanwhile, the blunt tail edge design of the wing improves the blade manufacturability, and effectively reduces the production cost.

Description

technical field [0001] The invention belongs to the field of horizontal axis wind turbine airfoil design, in particular to the inside and root airfoils of large wind turbine blades above MW level working under high Reynolds number. Background technique [0002] The blade is the core component of the wind turbine to capture wind energy for energy conversion, and the airfoil is the most important component of the blade, especially the outer and tip airfoils of the blade, which have a decisive impact on the aerodynamic performance of the wind turbine, so people usually Only focus on the study of the outer and tip thin airfoils. With the maturity of wind turbine design technology, in recent years, people have also begun to pay attention to the research on the airfoil of the inner and root transition sections, and the shape of the transition section of the blade root is usually determined by the thickness of the blade (that is, near the root) and the airfoil. Interpolate between...

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