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WIND TURBINE BLADE WITH PLURALITY OF LONGITUDINALLY EXTENDING FLOW GUIDING DEVICE PARTS

  • US 20120195764A1
  • Filed: 10/08/2010
  • Published: 08/02/2012
  • Est. Priority Date: 10/08/2009
  • Status: Active Grant
First Claim
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1. A blade (10) for a rotor of a wind turbine (2) having a substantially horizontal rotor shaft, said rotor comprising a hub (8), from which the blade (10) extends substantially in a radial direction when mounted to the hub (8), the blade having a longitudinal direction (r) with a tip end (14) and a root end (16) and a transverse direction, the blade further comprising:

  • a profiled contour (40, 42, 50) including a pressure side and a suction side, as well as a leading edge (18) and a trailing edge (20) with a chord having a chord length extending there between, the profiled contour, when being impacted by an incident airflow, generating a lift, wherein the profiled contour is divided into;

    a root region (30) having a substantially circular or elliptical profile closest to the hub,an airfoil region (34) having a lift-generating profile furthest away from the hub, anda transition region (32) between the root region (30) and the airfoil region (34), the transition region (32) having a profile gradually changing in the radial direction from the circular or elliptical profile of the root region to the lift-generating profile of the airfoil region, characterised in thatthe blade is provided with a plurality of longitudinally extending flow guiding device parts (70), which are grouped together to form a first flow guiding device group (77) in the transition region (32) of the blade (10), the first flow guiding device group extending along at least a longitudinal part of the transition region (32), whereineach of the flow guiding device parts (70) is added to the profiled contour (40, 42, 50) of the blade on the pressure side (52) of the blade (10), and whereinthe flow guiding device parts (70) are arranged so as to generate a separation of airflow from the pressure side of the blade at a point between the flow guiding device parts (70) and the trailing edge (20) of the blade, when the blade is impacted by the incident airflow.

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