Rotor blade of a wind turbine comprising a lift modifying device and method for installing thereof
A rotor blade of a wind turbine is provided, the rotor blade including a lift modifying device having at least one fluid jet module and at least one compressed fluid source, wherein the at least one fluid jet module includes multiple fluid jets, which are fluidically connected to the at least one compressed fluid source, whereby the at least one fluid jet module is mounted as an add-on onto an outer surface of the suction side or the pressure side of the rotor blade. Also provided is a method for installing this rotor blade, whereby a rotor blade is provided and the at least one fluid jet module is mounted as an add-on onto the outer surface of the suction side or the pressure side of the rotor blade.
1. A rotor blade of a wind turbine, the rotor blade comprising:
a lift modifying device having at least one fluid jet module and at least one compressed fluid source, wherein the at least one fluid jet module is a panel and comprises multiple fluid jets, which are fluidically connected to the at least one compressed fluid source,
wherein the panel of the at least one fluid jet module is mounted as an add-on onto an outer surface of a suction side or a pressure side of the rotor blade, the panel of the at least one fluid jet module having a first surface and a second surface opposite of the first surface, the first surface located on the outer surface of the rotor blade, further wherein the first surface and the second surface each having a shape that corresponds to a shape of a portion of the outer surface of the rotor blade to which the at least one fluid jet module is mounted;
wherein vortex generators are attached to the second surface of the panel of the at least one fluid module, and, in a chordwise direction, the multiple jets formed by orifices in the panel are located between a leading edge of the rotor blade and the vortex generators;
wherein, during a normal operation of the rotor blade, the vortex generators increase a lift coefficient of the rotor blade, and in response to operational or environmental conditions, the lift modifying device is configured to be activated such that the at least one compressed fluid source provides an injection of fluid through the multiple jets which generates a fluid curtain that separates air flow around an airfoil of the rotor blade creating a stalled flow after the multiple jets, which reduces the lift coefficient of the rotor blade and inhibits a vortex generation process of the vortex generators placed after the multiple jets.
2. The rotor blade according to claim 1 , wherein the fluid curtain separates the air flow on the suction side or the pressure side of the rotor blade, when the at least one compressed fluid source supplies compressed fluid to the at least one fluid jet module.
3. The rotor blade according to claim 1 , wherein the panel has a curved profile defined by a curved outer shape of the second surface.
4. The rotor blade according to claim 1 , wherein the at least one fluid jet module is mounted by at least one adhesive, at least one tape, and/or mechanical fasteners onto the outer surface of the rotor blade.
5. The rotor blade according to claim 1 , wherein the at least one fluid jet module is mounted reversibly onto the outer surface of the rotor blade.
6. The rotor blade according to claim 1 , wherein the at least one fluid jet module is embedded in a recess of a shell of the rotor blade.
7. The rotor blade according to claim 1 , wherein the at least one fluid jet module comprises a fluid flow channel fluidically communicating with the multiple fluid jets.
8. The rotor blade according to claim 1 , wherein the orifices are fluidically connected to the at least one compressed fluid source.
9. The rotor blade according to claim 1 , wherein ramps, spoilers, and/or flaps are attached to the at least one fluid jet module.
10. The rotor blade according to claim 1 , wherein at least one fluid supply line fluidically connecting the at least one fluid jet module with the at least one compressed fluid source is at least partially arranged in an inside of the rotor blade, attached to a spar web of the rotor blade.
11. The rotor blade according to claim 10 , wherein the at least one fluid supply line is attached externally to the outer surface of the rotor blade and routed to a feed hole inside of a shell of the rotor blade, by which the at least one fluid supply line is fed into the inside of the rotor blade.
12. The rotor blade according to claim 11 , wherein the rotor blade comprises at least one structural reinforcement at a location of the feed hole.
13. A method for forming a rotor blade for a wind turbine, the method comprising:
providing the rotor blade; and
adding at least one fluid jet module onto an outer surface of a suction side or a pressure side to arrive at the rotor blade according to claim 1 .
14. The method according to claim 13 , wherein a shell of the rotor blade has a recess, into which the at least one fluid jet module is fitted.
15. The rotor blade according to claim 1 , wherein the first surface of the at least one fluid jet module achieves a form fit with the outer surface of the rotor blade.
16. The rotor blade according to claim 1 , wherein the second surface is located a distance above the outer surface of the rotor blade, the distance corresponding to a thickness of the at least one fluid jet module.