Blade extension for rotor blade in wind turbine
AssigneeGeneral Electric Company
InventorPeter James Fritz
Life of this patent
Estimating the term…
Abstract
A rotor blade assembly is disclosed. The rotor blade assembly includes a rotor blade and a blade extension. The rotor blade has a pressure side, a suction side, a leading edge, and a trailing edge extending between a tip and a root. The rotor blade further has an aerodynamic profile. The blade extension is mounted to the rotor blade. The blade extension includes a cutaway mounting portion for mounting the blade extension to the rotor blade such that the blade extension is generally flush with at least one of the pressure side or the suction side of the rotor blade. The cutaway mounting portion defines a notch configured to locate the blade extension relative to the rotor blade.
Claims18
A wind turbine rotor blade assembly, comprising:
- a rotor blade having a pressure side, a suction side, a leading edge, and a trailing edge extending between a tip and a root, the rotor blade further having an aerodynamic profile;
- and,
- a blade extension mounted to the rotor blade,
- wherein the blade extension includes a cutaway mounting portion for mounting the blade extension to one of the pressure side or the suction side of the rotor blade such that the blade extension is generally flush with at least one of the pressure side or the suction side of the rotor blade, the cutaway mounting portion defining a notch configured to locate the blade extension relative to the rotor blade, and
- wherein the cutaway mounting portion tapers such that the blade extension generally corresponds with the aerodynamic profile of the other of the pressure side or the suction side of the rotor blade.
A wind turbine comprising:
- a plurality of rotor blades, each of the rotor blades having a pressure side, a suction side, a leading edge, and a trailing edge extending between a tip and a root, each of the rotor blades further having an aerodynamic profile;
- and,
- a blade extension mounted to at least one of the plurality of rotor blades,
- wherein the blade extension includes a cutaway mounting portion for mounting the blade extension to one of the pressure side or the suction side of the at least one rotor blade such that the blade extension is generally flush with at least one of the pressure side or the suction side of the at least one rotor blade, the cutaway mounting portion defining a notch configured to locate the blade extension relative to the at least one rotor blade, and
- wherein the cutaway mounting portion tapers such that the blade extension generally corresponds with the aerodynamic profile of the other of the pressure side or the suction side of the at least one rotor blade.
Dependencies are inferred from the claim text.