Vortex generators responsive to ambient conditions
US-9789956-B2 · Oct 17, 2017 · US
US10598149B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-10598149-B2 |
| Application number | US-201715638871-A |
| Country | US |
| Kind code | B2 |
| Filing date | Jun 30, 2017 |
| Priority date | Jul 5, 2016 |
| Publication date | Mar 24, 2020 |
| Grant date | Mar 24, 2020 |
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A rotor blade of a wind turbine including at least one vortex generator is provided. The vortex generator is attached to the surface of the rotor blade and is located at least partially within the boundary layer of the airflow flowing across the rotor blade. The vortex generator is exposed to a stagnation pressure, which is caused by the fraction of the airflow passing over the vortex generator and of which the magnitude depends on the velocity of the fraction of the airflow passing over the vortex generator. The vortex generator is arranged and prepared to change its configuration depending on the magnitude of the stagnation pressure acting on the vortex generator. Furthermore, an aspect relates to a wind turbine for generating electricity with at least one such rotor blade.
Opening claim text (preview).
The invention claimed is: 1. A rotor blade of a wind turbine comprising at least one vortex generator, wherein the at least one vortex generator is attached to a surface of the rotor blade, the at least one vortex generator is located at least partially within a boundary layer of an airflow flowing across the rotor blade, the at least one vortex generator is exposed to a stagnation pressure, which is caused by a fraction of the airflow passing over the at least one vortex generator and of which a magnitude depends on a velocity of the fraction of the airflow passing over the at least one vortex generator, wherein a configuration of the at least one vortex generator changes depending on the magnitude of the stagnation pressure acting on the at least one vortex generator and not depending upon an actively driven actuator, wherein when the magnitude of the stagnation pressure acting on the vortex generator increases, the stagnation pressure changes the configuration of the vortex generator to decrease generation of vortices, and wherein when the magnitude of the stagnation pressure on the vortex generator decreases, the stagnation pressure changes the configuration of the vortex generator to increase generation of vortices. 2. The rotor blade according to claim 1 , wherein the at least one vortex generator is situated in an outboard half of the rotor blade. 3. The rotor blade according to claim 1 , wherein the at least one vortex generator comprises an inflatable element, selected from a hose or a pressure chamber. 4. The rotor blade according to claim 3 , wherein the rotor blade comprises a pressure tube extending upstream from the at least one vortex generator for guiding a portion of the fraction of the airflow flowing across the rotor blade to the inflatable element. 5. The rotor blade according to claim 3 , wherein the at least one vortex generator is at least partially embedded into the surface of the rotor blade. 6. The rotor blade according to claim 1 , wherein the at least one vortex generator is able to bend depending on a value of the stagnation pressure acting on the at least one vortex generator. 7. The rotor blade according to claim 6 , wherein an elastic portion of the at least one vortex generator enables the at least one vortex generator to bend or straighten. 8. A wind turbine for generating electricity with at least one rotor blade according to claim 1 . 9. The rotor blade according to claim 1 , wherein the at least one vortex generator is situated in an outboard third of the rotor blade. 10. A vortex generator, wherein the vortex generator is attached to a surface of a rotor blade, wherein the vortex generator is located on the surface of the rotor blade such that the vortex generator is located at least partially within a boundary layer of an airflow flowing across the rotor blade, wherein the vortex generator is configured to be acted upon by a stagnation pressure caused by a fraction of the airflow passing over the vortex generator, the stagnation pressure having a magnitude dependent on a velocity of the fraction of the airflow passing over the vortex generator, wherein the stagnation pressure acting upon the vortex generator directly changes a configuration of the vortex generator without an actively driven actuator, wherein when the magnitude of the stagnation pressure on the vortex generator increases, the stagnation pressure changes the configuration of the vortex generator to decrease generation of vortices, and wherein when the magnitude of the stagnation pressure on the vortex generator decreases, the stagnation pressure changes the configuration of the vortex generator to increase generation of vortices. 11. The vortex generator according to claim 10 , wherein the stagnation pressure acting upon the vortex generator and directly changing the configuration of the vortex generator passively activates and deactivates the vortex generator in response to variations in the stagnation pressure. 12. The vortex generator according to claim 10 , wherein the vortex generator comprises an inflatable element, wherein the inflatable element receives a portion of the fraction of the airflow flowing across the rotor blade through a pressure tube extending upstream from the vortex generator. 13. A rotor blade of a wind turbine comprising: a vortex generator, wherein the vortex generator is attached to a surface of the rotor blade, wherein the vortex generator is located on the surface of the rotor blade such that the vortex generator is located at least partially within a boundary layer of an airflow flowing across the rotor blade, wherein the vortex generator comprises an inflatable element, wherein the vortex generator is configured to be acted upon by a stagnation pressure caused by a fraction of the airflow passing over the vortex generator, the stagnation pressure having a magnitude dependent on a velocity of the fraction of the airflow passing over the vortex generator, and wherein a configuration of the vortex generator is configured to change depending on the magnitude of the stagnation pressure acting upon the vortex generator, such that, with increasing stagnation pressure in the boundary layer, the configuration of the vortex generator changes to decrease generation of vortices, and with decreasing stagnation pressure in the boundary layer, the configuration of the vortex generator changes to increase generation of vortices, and a pressure tube extending upstream from the vortex generator for guiding a portion of the fraction of the airflow flowing across the rotor blade to the inflatable element. 14. The rotor blade of a wind turbine according to claim 13 , wherein the configuration of the vortex generator changes configuration without an actively driven actuator.
by changing the active surface of the wind engaging parts, e.g. reefing or furling · CPC title
Adjusting aerodynamic properties of the blades · CPC title
of changeable form or shape · CPC title
of the blades · CPC title
of the blades · CPC title
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