WO2002029247A1 - Method for regulating a windmill and an apparatus for the use of said method - Google Patents

Method for regulating a windmill and an apparatus for the use of said method Download PDF

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Publication number
WO2002029247A1
WO2002029247A1 PCT/DK2001/000622 DK0100622W WO0229247A1 WO 2002029247 A1 WO2002029247 A1 WO 2002029247A1 DK 0100622 W DK0100622 W DK 0100622W WO 0229247 A1 WO0229247 A1 WO 0229247A1
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WO
WIPO (PCT)
Prior art keywords
spoiler
blade
cavity
airflow
deactivated
Prior art date
Application number
PCT/DK2001/000622
Other languages
French (fr)
Inventor
Henrik Stiesdal
Original Assignee
Bonus Energy A/S
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Bonus Energy A/S filed Critical Bonus Energy A/S
Priority to AT01971723T priority Critical patent/ATE293213T1/en
Priority to US10/148,264 priority patent/US7419356B2/en
Priority to DE60110098T priority patent/DE60110098T2/en
Priority to AU2001291641A priority patent/AU2001291641A1/en
Priority to EP01971723A priority patent/EP1320680B1/en
Priority to DK01971723T priority patent/DK1320680T3/en
Publication of WO2002029247A1 publication Critical patent/WO2002029247A1/en

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Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F03MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
    • F03DWIND MOTORS
    • F03D7/00Controlling wind motors 
    • F03D7/02Controlling wind motors  the wind motors having rotation axis substantially parallel to the air flow entering the rotor
    • F03D7/0244Controlling wind motors  the wind motors having rotation axis substantially parallel to the air flow entering the rotor for braking
    • F03D7/0252Controlling wind motors  the wind motors having rotation axis substantially parallel to the air flow entering the rotor for braking with aerodynamic drag devices on the blades
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F03MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
    • F03DWIND MOTORS
    • F03D1/00Wind motors with rotation axis substantially parallel to the air flow entering the rotor 
    • F03D1/06Rotors
    • F03D1/0608Rotors characterised by their aerodynamic shape
    • F03D1/0633Rotors characterised by their aerodynamic shape of the blades
    • F03D1/0641Rotors characterised by their aerodynamic shape of the blades of the section profile of the blades, i.e. aerofoil profile
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F03MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
    • F03DWIND MOTORS
    • F03D7/00Controlling wind motors 
    • F03D7/02Controlling wind motors  the wind motors having rotation axis substantially parallel to the air flow entering the rotor
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05BINDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
    • F05B2240/00Components
    • F05B2240/20Rotors
    • F05B2240/30Characteristics of rotor blades, i.e. of any element transforming dynamic fluid energy to or from rotational energy and being attached to a rotor
    • F05B2240/305Flaps, slats or spoilers
    • F05B2240/3052Flaps, slats or spoilers adjustable
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05BINDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
    • F05B2240/00Components
    • F05B2240/20Rotors
    • F05B2240/30Characteristics of rotor blades, i.e. of any element transforming dynamic fluid energy to or from rotational energy and being attached to a rotor
    • F05B2240/306Surface measures
    • F05B2240/3062Vortex generators
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05BINDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
    • F05B2240/00Components
    • F05B2240/20Rotors
    • F05B2240/30Characteristics of rotor blades, i.e. of any element transforming dynamic fluid energy to or from rotational energy and being attached to a rotor
    • F05B2240/31Characteristics of rotor blades, i.e. of any element transforming dynamic fluid energy to or from rotational energy and being attached to a rotor of changeable form or shape
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05BINDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
    • F05B2240/00Components
    • F05B2240/20Rotors
    • F05B2240/30Characteristics of rotor blades, i.e. of any element transforming dynamic fluid energy to or from rotational energy and being attached to a rotor
    • F05B2240/32Characteristics of rotor blades, i.e. of any element transforming dynamic fluid energy to or from rotational energy and being attached to a rotor with roughened surface
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02EREDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E10/00Energy generation through renewable energy sources
    • Y02E10/70Wind energy
    • Y02E10/72Wind turbines with rotation axis in wind direction

Definitions

  • the invention relates to a method for regulating the airflow around a windmill blade, said method comprising a step, whereby a spoiler, mounted on the outer side of the blade, is activated and deactivated in order to create a first and respectively second airflow around the blade.
  • the invention also relates to a device for use when regulating the airflow around a windmill blade, where said device comprises at least one spoiler, which is made from a flexible material, provided with a least one cavity, and where the cavity in a deactivated form has a first volume and in an activated form has a second volume, and where the volume of the cavity can be changed from the deactivated form to the acti- vated form by leading a fluid to the cavity.
  • the blades are fixed on the hub of the mill and can not be turned around their longitudinal axis.
  • the adjusting angle the blades have on the hub is adjusted once and for all during the mounting and commissioning of the mill.
  • the blades are designed so the airflow over them in itself provides a greater air resis- tance in high wind and thereby limits the power output. Because of this passive use of the aerodynamic characteristics of the blades the regulation is simple and robust under all conditions, with only few peak loads.
  • the stall effect also depends highly on the design of the front edge of the blade. Small manufacturing tolerances in the form of the front edges can cause considerable differences in the power output level that a windmill stall regulates at.
  • the blades are mounted on bearings on the hub of the mill, so they can be turned around their longitudinal axis. In high wind the adjusting angle is always adjusted away from stall, so the lift is limited to provide the exact desired power output. With the active regulation it is possible to compensate for air density, surface roughness of the blade and influence from manufacturing tolerances.
  • Pitch regulation has the disadvantage that it demands a relatively complicated, active regulation, which in high wind can be sensitive to turbulence. Therefore, pitch regulation in practice presupposes a special generator with a completely or partly variable number of rotation, so the mill can speed up a bit up in case of wind gusts. Otherwise the active regulation cannot keep up with the variations in the wind, which results in too large peak loads.
  • Pitch regulation also has the disadvantage compared to stall regulation with fixed adjusted blades in that the blades must be mounted rotably on the hub of the mill and, therefore, have to be provided with bearings and actuator systems. These components must be able to transfer great loads, and involve increased service needs.
  • a newer regulation form is active stall regulation.
  • the two normal methods for limiting the power output are combined.
  • pitch regulation there are bearings between the blades and the hub of the mill, so that the entrance angle is adjustable, but the actual limiting of the power output in high wind is effected through stall.
  • active stall regulation has its own disadvantages compared to passive stall regulation with fixed adjusted blades.
  • the blades have to be mounted rotably on the hub of the mill and, therefore, have to be supplied with bearings and actuator systems.
  • These components have to transfer great loads, and involve increased service needs.
  • active stall regulation the regulation is slower than with pitch regulation, and the demands on the acrua- tor systems are, therefore, smaller, but the complexity is, however, considerably larger than with passive stall regulation.
  • spoilers on fixed adjusted blades are also known, where the regulation takes places through the spoiler effect, normally completely or partly supported by stalling of the blade.
  • the spoiler can typically be designed as a rail, arranged over the suction side of the blade, and which by extension provides increased air resistance and turbulence, and maybe also trips an actual stall.
  • Such spoilers were used on the windmills erected by FL. Smith in Denmark during the Second World War.
  • Spoiler systems of this kind normally have the disadvantages that they include mechanical parts far out on the blade. According to experience, is it difficult to maintain a high disposal level on such systems since the operating conditions are very difficult, and since the actuator mechanisms for the spoiler normally are badly suited to with- stand the hundreds of millions of exposures that the system is subjected to during normal operation. In addition to this spoilers arranged over the blade surface, also when not activated, normally exhibit a certain constant spoiler effect, which reduces the aerodynamic efficiency of the blade. The external mounting can also result in a significant contribution to the noise.
  • Deposited spoilers normally have the disadvantage that they demand special blade structures with recesses and cavities. Furthermore, they can normally only with difficulty be carried out at the actual front edge, where the air forces are powerful, but must be arranged further back on the suction side of the profile. Here the operating conditions are better, but the effect of the spoiler is in return more limited and, therefore, the spoiler has too be substantially larger. Noise problems may arise at the separating surfaces between the main blade and the spoiler, and the effect can be uncertain during icing and heavy pollution with dust etc., where extending and depositing can be restricted.
  • a spoiler type which consists of a flexible membrane arranged radially along a windmill blade approximately at the middle of the suction side of the blade, and which by inflating triggers stall on those sections of the blade, which are provided with this spoiler.
  • Spoiler systems of this kind has the disadvantage that the effect of a stall triggered at the middle of the suction side normally will not be sufficient to provide a substantial regulation.
  • this spoiler type presupposes a recessed channel on the blade in an area, where an unbroken and continued structure is needed for strength reasons.
  • the purpose with the present invention is to provide a method and a device for regu- lating the power output of a windmill with fixed adjusted blades, which reduces the disadvantages which are connected with the known methods.
  • This purpose is achieved by using a method of the aforementioned type, which is peculiar in that said first airflow is used to suppress a flow regulation, which is estab- lished by a flow regulating unit, which is arranged in connection with the spoiler and in that said flow regulation eliminates a unintended spoiler effect of said spoiler in its deactivated state.
  • the device according to the invention is characterised in that said at least one spoiler is mounted on a surface of the blade, and that a flow regulating unit is provided associated with said at least one spoiler.
  • the invention is thus based on a flexible spoiler, which is arranged on the suction side of the blade built together with or arranged associated with another type of flow regu- lating unit, and which is activated by filling it with a liquid or a gaseous medium.
  • This method is, surprisingly, very effective, and has a lot of advantages compared to the known systems.
  • the spoiler can avoid those recesses and cavities, which normally are connected with deposited spoilers. By not having separating surfaces between the spoiler and the main blade, the function of the spoiler also remains reliable under icing and heavy pollution with dust etc.
  • a particular advantage of the invention originates from the mounting on the surface of the blade. This has the effect that the spoiler can be retrofitted, so that the method for regulation can be introduced to existing windmills. Normally, this is not possible with the known spoiler types, maybe excepting the original type, which is mounted a bit above the surface of the blade.
  • the spoiler and the flow regulating unit can be dimensioned mutually in such a manner that the spoiler, when activated, completely or partly eliminates the effect of the flow regulating unit.
  • the method is characterised in that the flow regulation provides the aerodynamic profile with a higher lift coefficient or otherwise leads to the fact that stall first occurs at a higher wind velocity.
  • the maximum power output of the windmill will increase compared to what would have been the case if the second flow regulating unit was not mounted on the outer side of the blade.
  • the method is, according to further embodiments, characterised in that the spoiler's change in the airflow around the blade changes the flow regulation established by a vortex generator and that the change in the flow of air around the blade is regulated, so that the power output from the windmill is maintained at a certain level in high wind.
  • the device according the invention can be made in different ways, so that: - the spoiler consist of a foil with a outer side, which is determined to face outwards in relation to the surface of the blade, and a inner side, which is determined to face in- wards in relation to the surface of the blade, that said inner side of the foil is determined to be fastened to the surface of the blade, and that the cavity is formed between the outer side and the inner side of the foil; - the foil has a centre area, where the cavity is formed, which has a thickness T, that said centre area converges against the edge areas, which have a thickness t, and that said thickness t is smaller than the thickness T;
  • the centre area of the spoiler when the spoiler assumes its deactivated form, has a outer side which converges continuously towards the edge areas, and that the centre area of the spoiler, when the spoiler assumes its activated form, at least provides a changed profile for the blade, preferably showing a discontinuity in relation to the surface of the blade;
  • passageways which extend in narrower channels in the cavity, and which run between wider channels in the cavity, that the passage- ways are folded together, when the spoiler assumes its deactivated form, and said passageways are enlarged, when the spoiler assumes its activated form;
  • the spoiler is brought from its deactivated form to its activated form by filling the cavity with a given volume of fluid, preferably compressed air or another pressurised gas, alternatively hydraulic oil or another fluid;
  • a given volume of fluid preferably compressed air or another pressurised gas, alternatively hydraulic oil or another fluid;
  • the spoiler is brought from its activated form back to its deactivated form by emptying the cavity of fluid with aid from the airflow, which acts on the surface of the blade and on the outer side of the foil, and/or with aid from the centrifugal force acting on the fluid;
  • the spoiler is disposed on the suction side of the blade on only a part of the blade; - the spoiler is disposed in radial positions from innermost 0-30% to outermost 30-
  • the spoiler is placed immediately in front of a series of vortex generators with a height in the area of 3-50 mm;
  • the spoiler is manufactured from rubber, alternatively manufactured from plastic, and mainly is manufactured from an extruded profile of silicone rubber and with a width of 50-250 mm.
  • Figure 1 shows a windmill blade with an extern spoiler of known, older type.
  • the blade profile 1 is provided with spoiler rail 2, which is carried by a series fittings 3 with hinges 4.
  • the spoiler is shown in its normal deactivated position, where no spoiler effect is desired.
  • Figure 2 shows the same spoiler in an activated position, where the spoiler is turned to maximum effect by mechanical means.
  • FIG 3 shows a windmill blade with a built-in spoiler of known, newer type.
  • the blade profile 5 is provided with a spoiler rail 6, which is deposited in a cavity 7 in the blade surface, and which can turn about a hinge 8.
  • the spoiler is shown in its normal deactivated position, where no spoiler effect is desired.
  • Figure 4 shows the same spoiler in an activated position, where the spoiler is turned to maximum effect by mechanical means.
  • Figure 5 shows a windmill blade with a built-in flexible spoiler of known, newer type.
  • the blade profile 9 is provided with a cavity 10, which is covered with a flexible membrane 11.
  • the cavity 10 extends along a part of the blade length, and is closed inwards against the base of the blade and outwards against the tip of the blade with valves, which are not shown on the figure.
  • the spoiler is shown in its normal, deacti- vated position, where no spoiler effect is desired.
  • Figure 6 shows the same spoiler in its activated position, where the spoiler membrane is inflated to maximum effect.
  • the activation takes place by opening the innermost valve and closing the outermost.
  • the inflation is then caused by the overpressure, which originates from the centrifugal force on the air column, which stands in the blade cavity.
  • Deactivation takes place by closing the innermost valve and open the outermost.
  • Figure 7 shows a flow regulating unit in the form of vortex generators mounted on the suction side of a windmill blade. By producing whirls, which pump energy into the boundary layer, the vortex generators delay the occurrence of stall.
  • Figure 8 shows a passive stall regulated windmill power output curve with and without vortex generators. It is shown how the wind speed at which the regulation really limits the increase in power output, increases with vortex generators, and how the maximum power output increases correspondingly.
  • FIG 9 shows a windmill blade with a spoiler according the invention.
  • the blade profile 12 is provided with a flexible spoiler 13, which extends along a part of the blade length.
  • the spoiler has a cross section with a cavity 14.
  • the cavity 14 is partly closed outwards against the tip of blade, and is connected inwards against the base of the blade to a compressed air system, which can apply a larger or smaller pressure on the spoiler cavity.
  • the spoiler is shown in its normal deactivated position, where no spoiler effect is desired.
  • a flow regulating unit 15 is arranged, here embodied as vortex generators.
  • the flow regulating unit is here arranged between the spoiler and the back edge of the blade, but can also be arranged between the spoiler and the front edge of the blade. It is shown how a small whirl from the front edge of the spoiler is completely suppressed by the much larger whirls from the vortex generators.
  • Figure 10 shows same spoiler in its activated position, where the spoiler is blown up to the maximum effect.
  • the activating normally occurs by applying pressure to the cavity of the spoiler.
  • the spoiler can be inflated without steps, depending on the applied pressure.
  • the deactivating occurs by reducing filling pressure. Emptying is reinforced by the centrifugal effect on the air column standing in the spoiler cavity, possibly supplied with the ejector effect from passing airflow at the outermost end of the spoiler.
  • the spoiler is activated to such a high degree that the airflow deflects around the flow regulating unit, which then becomes ineffective. All intermediate stages of activation are possible, so the effect of the flow regulating unit can be influenced to a larger or smaller degree.
  • Figure 11 shows examples of cross sections of spoilers according the invention, before the spoilers are mounted on the blade.
  • the spoilers can for example be extruded in silicone rubber or in EPDM Shore 45, whereby they easily can be mounted on suction sides with different curvatures.
  • a normal preferred embodiment 16 may include a number of ribs 17, which maintain the form of the cavity during an possible underpressure from the suction effect under the centrifugal effect, but which, however provides a good access for air to inflation.
  • a third preferred embodiment 18 can exhibit an uneven cross section of the cavity, where one part 19 has a large material thickness of the side, which expands when inflated, while another part 20 has a lesser material thickness.
  • the cavity can be divided in two or more parallel channels, which may be inflated to different pressures.
  • the form differentiates further, and a larger part of the spoiler can be imparted a form, which is favourable for the replacing.
  • Figure 12 shows a example of a power output curve for a mill provided with a spoiler according the invention.
  • the two graphs shows the power output curve respectively with and without active spoiler regulation.

Abstract

The invention relates to a method and a device for regulating the airflow around a blade of a windmill. The device comprise a spoiler, which is provided with a cavity. The spoiler is mounted to a surface of the blade in connection with an another flow regulating unit, and the spoiler can change the airflow around the blade by assuming different forms. When the spoiler is in a deactivated form no particular changes of the airflow takes place, as the spoiler runs continually and follows the contour of the blade. When the spoiler is in an activated form the airflow, however, is changed in that the spoiler no longer follows the contours of the blade and creates a discontinuity or at least changes the profile of the blade in such way that the airflow conditions are changed. In particular the airflow conditions can be changed so the effect of the second flow regulating unit completely or partly is eliminated. The change of the form takes place by supplying a fluid, such as compressed air or hydraulic oil, to the cavity in the spoiler. The change of the airflow is an advantage in that is thus is possible to regulate the speed of rotation of the rotor, which the blade is mounted on.

Description

METHOD FOR REGULATING A WINDMILL, AND AN APPARATUS FORTHE USE OF SAID METHOD
Background of the invention The invention relates to a method for regulating the airflow around a windmill blade, said method comprising a step, whereby a spoiler, mounted on the outer side of the blade, is activated and deactivated in order to create a first and respectively second airflow around the blade.
The invention also relates to a device for use when regulating the airflow around a windmill blade, where said device comprises at least one spoiler, which is made from a flexible material, provided with a least one cavity, and where the cavity in a deactivated form has a first volume and in an activated form has a second volume, and where the volume of the cavity can be changed from the deactivated form to the acti- vated form by leading a fluid to the cavity.
It is known that one has to limit the power output of every mill in high wind, otherwise the mill can be overloaded. The normal methods for limiting the power output are stall regulation and pitch regulation.
With ordinary stall regulation, the blades are fixed on the hub of the mill and can not be turned around their longitudinal axis. The adjusting angle the blades have on the hub is adjusted once and for all during the mounting and commissioning of the mill. The blades are designed so the airflow over them in itself provides a greater air resis- tance in high wind and thereby limits the power output. Because of this passive use of the aerodynamic characteristics of the blades the regulation is simple and robust under all conditions, with only few peak loads.
Ordinary stall regulation has the disadvantage that the maximum power output de- pends on the air density and the surface roughness of the blade. There will, therefore, be changes in the power output from summer to winter, and when the blades are dirty.
The stall effect also depends highly on the design of the front edge of the blade. Small manufacturing tolerances in the form of the front edges can cause considerable differences in the power output level that a windmill stall regulates at.
With pitch regulation the blades are mounted on bearings on the hub of the mill, so they can be turned around their longitudinal axis. In high wind the adjusting angle is always adjusted away from stall, so the lift is limited to provide the exact desired power output. With the active regulation it is possible to compensate for air density, surface roughness of the blade and influence from manufacturing tolerances.
Pitch regulation has the disadvantage that it demands a relatively complicated, active regulation, which in high wind can be sensitive to turbulence. Therefore, pitch regulation in practice presupposes a special generator with a completely or partly variable number of rotation, so the mill can speed up a bit up in case of wind gusts. Otherwise the active regulation cannot keep up with the variations in the wind, which results in too large peak loads. Pitch regulation also has the disadvantage compared to stall regulation with fixed adjusted blades in that the blades must be mounted rotably on the hub of the mill and, therefore, have to be provided with bearings and actuator systems. These components must be able to transfer great loads, and involve increased service needs.
A newer regulation form is active stall regulation. Here the two normal methods for limiting the power output are combined. Like with pitch regulation there are bearings between the blades and the hub of the mill, so that the entrance angle is adjustable, but the actual limiting of the power output in high wind is effected through stall.
Compared with ordinary stall regulation active stall regulation has the advantage that the maximum power output with certainty can be maintained at the desired level, regardless of air density, possible dirt on the blades and the influence from manufacturing tolerances. Compared with pitch regulation active stall regulation has the advan- tage that the actual regulation is effected with the use of stall, consequently through a passive use of the aerodynamic characteristics of the blade, so the sensibility to turbu- lence remains small. It is, therefore, not necessary to use special generators, variable rpm or the like in order to avoid high peak loads.
Nevertheless, active stall regulation has its own disadvantages compared to passive stall regulation with fixed adjusted blades. Like with pitch regulation there is the disadvantage that the blades have to be mounted rotably on the hub of the mill and, therefore, have to be supplied with bearings and actuator systems. These components have to transfer great loads, and involve increased service needs. With active stall regulation the regulation is slower than with pitch regulation, and the demands on the acrua- tor systems are, therefore, smaller, but the complexity is, however, considerably larger than with passive stall regulation.
Apart from the regulation systems based on the turning of whole blades, spoilers on fixed adjusted blades are also known, where the regulation takes places through the spoiler effect, normally completely or partly supported by stalling of the blade. The spoiler can typically be designed as a rail, arranged over the suction side of the blade, and which by extension provides increased air resistance and turbulence, and maybe also trips an actual stall. Such spoilers were used on the windmills erected by FL. Smith in Denmark during the Second World War.
Spoiler systems of this kind normally have the disadvantages that they include mechanical parts far out on the blade. According to experience, is it difficult to maintain a high disposal level on such systems since the operating conditions are very difficult, and since the actuator mechanisms for the spoiler normally are badly suited to with- stand the hundreds of millions of exposures that the system is subjected to during normal operation. In addition to this spoilers arranged over the blade surface, also when not activated, normally exhibit a certain constant spoiler effect, which reduces the aerodynamic efficiency of the blade. The external mounting can also result in a significant contribution to the noise.
There are other spoiler systems, which consist of rails or bellows deposited in the blade surface. The effect again depends on increased air resistance and turbulence, but in comparison to external spoilers the mechanism is somewhat better protected. Such spoilers are, among others, used in the early windmills of the WindMatic type in Denmark. By being deposited in the blade surface this type of spoilers has the advantage that they not in any noticeable way reduce the aerodynamic efficiency of the blade, when they not are extended.
Deposited spoilers normally have the disadvantage that they demand special blade structures with recesses and cavities. Furthermore, they can normally only with difficulty be carried out at the actual front edge, where the air forces are powerful, but must be arranged further back on the suction side of the profile. Here the operating conditions are better, but the effect of the spoiler is in return more limited and, therefore, the spoiler has too be substantially larger. Noise problems may arise at the separating surfaces between the main blade and the spoiler, and the effect can be uncertain during icing and heavy pollution with dust etc., where extending and depositing can be restricted.
From European patent application EP 0 394 882 Al a spoiler type is known, which consists of a flexible membrane arranged radially along a windmill blade approximately at the middle of the suction side of the blade, and which by inflating triggers stall on those sections of the blade, which are provided with this spoiler. Spoiler systems of this kind has the disadvantage that the effect of a stall triggered at the middle of the suction side normally will not be sufficient to provide a substantial regulation. In addition there is the disadvantage that this spoiler type presupposes a recessed channel on the blade in an area, where an unbroken and continued structure is needed for strength reasons.
From European patent application EP 0 283 730 Al a flow body is known, where at least the one side is covered with a membrane, which can change form as a function of a inner pressure media. Through inflation this body can assumably change its aerody- namic characteristics to such a high degree that a certain regulation can take place. A membrane system of this kind has the disadvantage that it covers large parts of the blade surface, and that the effect of the regulation can be difficult to control because of the large surfaces.
It is known that the air flow over a windmill blade can be regulated with flow regulat- ing means. Examples of such means are for example described in the Danish utility model application DK 95 00238 W. Here, among other things, vortex generators are illustrated (figure 5).
The purpose with the present invention is to provide a method and a device for regu- lating the power output of a windmill with fixed adjusted blades, which reduces the disadvantages which are connected with the known methods.
This purpose is achieved by using a method of the aforementioned type, which is peculiar in that said first airflow is used to suppress a flow regulation, which is estab- lished by a flow regulating unit, which is arranged in connection with the spoiler and in that said flow regulation eliminates a unintended spoiler effect of said spoiler in its deactivated state.
The device according to the invention is characterised in that said at least one spoiler is mounted on a surface of the blade, and that a flow regulating unit is provided associated with said at least one spoiler.
The invention is thus based on a flexible spoiler, which is arranged on the suction side of the blade built together with or arranged associated with another type of flow regu- lating unit, and which is activated by filling it with a liquid or a gaseous medium.
This method is, surprisingly, very effective, and has a lot of advantages compared to the known systems.
By being based on an active regulation the disadvantages normally connected with passive stall regulation with fixed adjusted blades are avoided. With the active regula- tion it is possible to compensate for air density, surface roughness of the blade and the influence from manufacturing tolerances.
By being based on a spoiler effect the disadvantages normally connected with turning blade systems are avoided. Compared to the substantial costs for blade bearings and actuator systems, which must be able to transfer large loads, the cost of the spoiler system is completely marginal, likewise the service needs are heavily reduced.
By being based on a flexible spoiler type, mounted on the surface of the blade, the dis- advantages normally connected with spoilers of the known type are avoided.
There is no loss of aerodynamic efficiency, when the spoiler is not extended, and by forming of the edges appropriately, so the height of the passage to the surface of the blade is small in comparison with the boundary layer, the risk of noise problem can be minimised. By being mounted on the surface of the blade the spoiler can avoid those recesses and cavities, which normally are connected with deposited spoilers. By not having separating surfaces between the spoiler and the main blade, the function of the spoiler also remains reliable under icing and heavy pollution with dust etc.
A particular advantage of the invention originates from the mounting on the surface of the blade. This has the effect that the spoiler can be retrofitted, so that the method for regulation can be introduced to existing windmills. Normally, this is not possible with the known spoiler types, maybe excepting the original type, which is mounted a bit above the surface of the blade.
By virtue of the fact that the spoiler is built together with or arranged in connection to another type flow regulating unit, a particularly favourable result of the interaction between the spoiler and the flow regulating unit can be obtained.
This particularly favourable interaction will occur, where the flow regulating unit in itself is of the type, which completely or partly delays the aerodynamic stall of the blade profile, for example embodied as vortex generators. The interaction can then be expressed in two ways.
Firstly a possibly smaller, unwanted spoiler effect of the spoiler in its non-active state will be eliminated when the spoiler is arranged in connection to the flow regulating unit, as long as this has sufficient capacity to override a such undesired and unfortunate spoiler effect in non-active state.
Secondly the spoiler and the flow regulating unit can be dimensioned mutually in such a manner that the spoiler, when activated, completely or partly eliminates the effect of the flow regulating unit.
If the flow regulating unit has a considerable influence on the aerodynamic characteristics of the blade, a large regulating effect can be achieved with the spoiler.
According to a particular embodiment the method is characterised in that the flow regulation provides the aerodynamic profile with a higher lift coefficient or otherwise leads to the fact that stall first occurs at a higher wind velocity. Hereby the maximum power output of the windmill will increase compared to what would have been the case if the second flow regulating unit was not mounted on the outer side of the blade.
The method is, according to further embodiments, characterised in that the spoiler's change in the airflow around the blade changes the flow regulation established by a vortex generator and that the change in the flow of air around the blade is regulated, so that the power output from the windmill is maintained at a certain level in high wind.
The device according the invention can be made in different ways, so that: - the spoiler consist of a foil with a outer side, which is determined to face outwards in relation to the surface of the blade, and a inner side, which is determined to face in- wards in relation to the surface of the blade, that said inner side of the foil is determined to be fastened to the surface of the blade, and that the cavity is formed between the outer side and the inner side of the foil; - the foil has a centre area, where the cavity is formed, which has a thickness T, that said centre area converges against the edge areas, which have a thickness t, and that said thickness t is smaller than the thickness T;
- the centre area of the spoiler, when the spoiler assumes its deactivated form, has a outer side which converges continuously towards the edge areas, and that the centre area of the spoiler, when the spoiler assumes its activated form, at least provides a changed profile for the blade, preferably showing a discontinuity in relation to the surface of the blade;
- through the cavity between the outer side of the spoiler and the inner side of the spoiler reinforcing ribs are formed, which are able to maintain a given minimum distance between the outer side and the inner side of the spoiler, when the device is in its deactivated form;
- through the cavity there are formed passageways, which extend in narrower channels in the cavity, and which run between wider channels in the cavity, that the passage- ways are folded together, when the spoiler assumes its deactivated form, and said passageways are enlarged, when the spoiler assumes its activated form;
- the spoiler is brought from its deactivated form to its activated form by filling the cavity with a given volume of fluid, preferably compressed air or another pressurised gas, alternatively hydraulic oil or another fluid; - the spoiler is brought from its activated form back to its deactivated form by emptying the cavity of fluid with aid from the airflow, which acts on the surface of the blade and on the outer side of the foil, and/or with aid from the centrifugal force acting on the fluid;
- the spoiler is disposed on the suction side of the blade on only a part of the blade; - the spoiler is disposed in radial positions from innermost 0-30% to outermost 30-
80% of the blade length;
- the spoiler is placed immediately in front of a series of vortex generators with a height in the area of 3-50 mm; or
- the spoiler is manufactured from rubber, alternatively manufactured from plastic, and mainly is manufactured from an extruded profile of silicone rubber and with a width of 50-250 mm. Description of the drawings
In the following the invention is described in more detail with reference to the figures.
Figure 1 shows a windmill blade with an extern spoiler of known, older type. The blade profile 1 is provided with spoiler rail 2, which is carried by a series fittings 3 with hinges 4. The spoiler is shown in its normal deactivated position, where no spoiler effect is desired.
Figure 2 shows the same spoiler in an activated position, where the spoiler is turned to maximum effect by mechanical means.
Figure 3 shows a windmill blade with a built-in spoiler of known, newer type. The blade profile 5 is provided with a spoiler rail 6, which is deposited in a cavity 7 in the blade surface, and which can turn about a hinge 8. The spoiler is shown in its normal deactivated position, where no spoiler effect is desired.
Figure 4 shows the same spoiler in an activated position, where the spoiler is turned to maximum effect by mechanical means.
Figure 5 shows a windmill blade with a built-in flexible spoiler of known, newer type. The blade profile 9 is provided with a cavity 10, which is covered with a flexible membrane 11. The cavity 10 extends along a part of the blade length, and is closed inwards against the base of the blade and outwards against the tip of the blade with valves, which are not shown on the figure. The spoiler is shown in its normal, deacti- vated position, where no spoiler effect is desired.
Figure 6 shows the same spoiler in its activated position, where the spoiler membrane is inflated to maximum effect. The activation takes place by opening the innermost valve and closing the outermost. The inflation is then caused by the overpressure, which originates from the centrifugal force on the air column, which stands in the blade cavity. Deactivation takes place by closing the innermost valve and open the outermost. Figure 7 shows a flow regulating unit in the form of vortex generators mounted on the suction side of a windmill blade. By producing whirls, which pump energy into the boundary layer, the vortex generators delay the occurrence of stall.
Figure 8 shows a passive stall regulated windmill power output curve with and without vortex generators. It is shown how the wind speed at which the regulation really limits the increase in power output, increases with vortex generators, and how the maximum power output increases correspondingly.
Figure 9 shows a windmill blade with a spoiler according the invention. The blade profile 12 is provided with a flexible spoiler 13, which extends along a part of the blade length. The spoiler has a cross section with a cavity 14. The cavity 14 is partly closed outwards against the tip of blade, and is connected inwards against the base of the blade to a compressed air system, which can apply a larger or smaller pressure on the spoiler cavity. The spoiler is shown in its normal deactivated position, where no spoiler effect is desired. Associated with the spoiler a flow regulating unit 15 is arranged, here embodied as vortex generators. The flow regulating unit is here arranged between the spoiler and the back edge of the blade, but can also be arranged between the spoiler and the front edge of the blade. It is shown how a small whirl from the front edge of the spoiler is completely suppressed by the much larger whirls from the vortex generators.
Figure 10 shows same spoiler in its activated position, where the spoiler is blown up to the maximum effect. The activating normally occurs by applying pressure to the cavity of the spoiler. The spoiler can be inflated without steps, depending on the applied pressure. The deactivating occurs by reducing filling pressure. Emptying is reinforced by the centrifugal effect on the air column standing in the spoiler cavity, possibly supplied with the ejector effect from passing airflow at the outermost end of the spoiler. Here, the spoiler is activated to such a high degree that the airflow deflects around the flow regulating unit, which then becomes ineffective. All intermediate stages of activation are possible, so the effect of the flow regulating unit can be influenced to a larger or smaller degree. Figure 11 shows examples of cross sections of spoilers according the invention, before the spoilers are mounted on the blade. The spoilers can for example be extruded in silicone rubber or in EPDM Shore 45, whereby they easily can be mounted on suction sides with different curvatures. A normal preferred embodiment 16 may include a number of ribs 17, which maintain the form of the cavity during an possible underpressure from the suction effect under the centrifugal effect, but which, however provides a good access for air to inflation. A third preferred embodiment 18 can exhibit an uneven cross section of the cavity, where one part 19 has a large material thickness of the side, which expands when inflated, while another part 20 has a lesser material thickness. Hereby can the form of the inflated spoiler be adjusted to provide the most advantageous replacement of the air flow. In a fourth preferred embodiment the cavity can be divided in two or more parallel channels, which may be inflated to different pressures. Thus, the form differentiates further, and a larger part of the spoiler can be imparted a form, which is favourable for the replacing.
Figure 12 shows a example of a power output curve for a mill provided with a spoiler according the invention. The two graphs shows the power output curve respectively with and without active spoiler regulation.

Claims

1. Method for regulating the airflow around a windmill blade, said method comprising a step, whereby a spoiler, mounted on the outer side of the blade, is activated and deactivated in order to create a first and respectively second airflow around the blade, characterised in that said first airflow is used to suppress a flow regulation, which is established by a flow regulating unit, which is arranged in connection with the spoiler and in that said flow regulation eliminates a unintended spoiler effect of said spoiler in its deactivated state.
2. Method according to claim 1, characterised in that the flow regulation provides the aerodynamic profile with a higher lift coefficient or otherwise delays stall to first take place with a higher wind velocity.
3. Method according to claim 1 or claim 2, characterised in that the spoilers change of airflow around the blade changes the flow regulation established by a vortex generator.
4. Method according to any of the claims 1-3, characterisedin that the change of airflow around the blade is regulated so that the power output from the windmill is maintained at a certain level in high wind.
5. Device for use when regulating the airflow around a windmill blade, where said device comprises at least one spoiler, which is made from a flexible material, provided with a least one cavity, and where the cavity in a deactivated form has a first volume and in an activated form has a second volume, and where the volume of the cavity can be changed from the deactivated form to the activated form by leading a fluid to the cavity, characterised in that said at least one spoiler is mounted on a surface of the blade, and that a flow regulating unit is provided associated with said at least one spoiler.
6. Device according to claim 5, characterised in that the spoiler constitutes a foil with a outer side, which is determined to face outwards in relation to the surface of the blade, and a inner side, which is determined to face inwards in relation to the surface of the blade, that said inner side of the foil is determined to be fastened to the surface of the blade, and that the cavity is formed between the outer side and the inner side of the foil
7. Device according to claim 5 or claim 6, characterised in that the foil has a centre area, where the cavity is formed, and which has a thickness T, that said centre area converges against the edge areas, which have a thickness t, and that said thickness t is less than the thickness T.
8. Device according to any of the claims 5-7, characterisedin that the centre area of the spoiler, when the spoiler assumes its deactivated form, has a outer side which converges continuously towards the edge areas, and that the centre area of the spoiler, when the spoiler assumes its activated form, at least provides a changed profile for the blade, preferably showing a discontinuity in relation to the surface of the blade.
9. Device according to any of the claims 5-8, characterisedin that through the cavity between the outer side of the spoiler and the inner side of the spoiler there are formed reinforcing ribs, which are able to maintain a given minimum distance between the outer side and the inner side of the spoiler, when the device is in its deactivated form.
10. Device according to any of the claims 5-9, characterised in that through the cavity there are formed passageways extending in narrower channels in the cavity, and which runs between wider channels in the cavity, that said passageways are folded together, when the spoiler assumes its deactivated form, and that said passageways are enlarged, when the spoiler assumes its activated form.
11. Device according to any of the claims 5-10, characterised in that the spoiler is brought from its deactivated form to its activated form by filling the cavity with a given volume of fluid, preferably compressed air or another pressurised gas, alternatively hydraulic oil or another fluid.
12. Device according to claims 11, characterised in that the spoiler is brought from its activated form back to its deactivated form by emptying the cavity of fluid with aid from the airflow, which acts on the surface of the blade and on the outer side of the foil, and/or with aid from the centrifugal force acting the fluid.
13. Device according to any of the claims 5-12, characterised in that the spoiler is placed on the suction side of the blade on only a part of the blade.
14. Device according to 13, characterised in that the spoiler is placed in radial positions from innermost 0-30% to outermost 30-80% of the blade length.
15. Device according to 14, characterised in that the spoiler is placed immediate in front of a series of vortex generators with a height in the area of 3-50 mm.
16. Device according to any of the claims 5-15, characterised in that the spoiler is manufactured from rubber, alternatively manufactured from plastic, and preferably is manufactured from an extruded profile of silicone rubber and with a width of 50- 250 mm.
PCT/DK2001/000622 2000-09-29 2001-09-28 Method for regulating a windmill and an apparatus for the use of said method WO2002029247A1 (en)

Priority Applications (6)

Application Number Priority Date Filing Date Title
AT01971723T ATE293213T1 (en) 2000-09-29 2001-09-28 CONTROL METHOD FOR A WIND TURBINE AND CONTROL DEVICE THEREFOR
US10/148,264 US7419356B2 (en) 2000-09-29 2001-09-28 Method for regulating a windmill, and an apparatus for the use of said method
DE60110098T DE60110098T2 (en) 2000-09-29 2001-09-28 CONTROL METHOD FOR A WIND TURBINE AND REGULATORY EQUIPMENT THEREFOR
AU2001291641A AU2001291641A1 (en) 2000-09-29 2001-09-28 Method for regulating a windmill and an apparatus for the use of said method
EP01971723A EP1320680B1 (en) 2000-09-29 2001-09-28 Method for regulating a windmill and an apparatus for the use of said method
DK01971723T DK1320680T3 (en) 2000-09-29 2001-09-28 A method for regulating a wind turbine and a device for use in the method

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DK200001450A DK174261B1 (en) 2000-09-29 2000-09-29 Device for use in regulating air flow around a wind turbine blade
DKPA200001450 2000-09-29

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AT (1) ATE293213T1 (en)
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DK (2) DK174261B1 (en)
ES (1) ES2240519T3 (en)
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Cited By (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2006177354A (en) * 2004-12-23 2006-07-06 General Electric Co <Ge> Active flow modification on wind power turbine blade
US7469750B2 (en) 2004-09-20 2008-12-30 Owen Oil Tools Lp Expandable seal
WO2009080316A2 (en) * 2007-12-21 2009-07-02 Vestas Wind Systems A/S Active flow control device and method for affecting a fluid boundary layer of a wind turbine blade
CN101539119A (en) * 2008-03-07 2009-09-23 歌美飒创新技术公司 A wind turbine blade
EP2128385A2 (en) 2008-05-16 2009-12-02 Frontier Wind, LLC. Wind turbine with deployable air deflectors
US8061986B2 (en) 2010-06-11 2011-11-22 General Electric Company Wind turbine blades with controllable aerodynamic vortex elements
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Families Citing this family (52)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE10348060B4 (en) 2003-10-16 2016-10-27 Windreich GmbH Rotor blade of a rotor of a wind energy plant
US7582977B1 (en) * 2005-02-25 2009-09-01 Clipper Windpower Technology, Inc. Extendable rotor blades for power generating wind and ocean current turbines within a module mounted atop a main blade
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US7708519B2 (en) * 2007-03-26 2010-05-04 Honeywell International Inc. Vortex spoiler for delivery of cooling airflow in a turbine engine
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DE102007059285A1 (en) * 2007-12-08 2009-06-10 Nordex Energy Gmbh Rotor blade for use in rotor of wind turbine, has profile flown from leading edge to trailing edge, where leading edge is formed by rotational body in longitudinal section of blade, and body is rotatably supported about symmetric axis
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US20110142676A1 (en) * 2010-11-16 2011-06-16 General Electric Company Rotor blade assembly having an auxiliary blade
WO2012082324A1 (en) 2010-12-16 2012-06-21 Inventus Holdings, Llc A method for determining optimum vortex generator placement for maximum efficiency on a retrofitted wind turbine generator of unknown aerodynamic design
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US20120141271A1 (en) * 2011-09-13 2012-06-07 General Electric Company Actuatable spoiler assemblies for wind turbine rotor blades
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US10677217B2 (en) * 2012-10-03 2020-06-09 General Electric Company Wind turbine and method of operating the same
US9759068B2 (en) * 2013-02-28 2017-09-12 General Electric Company System and method for controlling a wind turbine based on identified surface conditions of the rotor blades
US9464532B2 (en) * 2013-03-05 2016-10-11 Bell Helicopter Textron Inc. System and method for reducing rotor blade noise
DE102013204879A1 (en) * 2013-03-20 2014-09-25 Senvion Se Rotor blade of a wind turbine, wind turbine and method for operating a wind turbine
DE102013210733B4 (en) * 2013-06-10 2021-03-25 Senvion Gmbh Rotor blade and vortex generator
US20150003985A1 (en) * 2013-06-27 2015-01-01 General Electric Company Moveable surface features for wind turbine rotor blades
US9267491B2 (en) 2013-07-02 2016-02-23 General Electric Company Wind turbine rotor blade having a spoiler
US20150211487A1 (en) * 2014-01-27 2015-07-30 Siemens Aktiengesellschaft Dual purpose slat-spoiler for wind turbine blade
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Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0283730A1 (en) * 1987-03-14 1988-09-28 Mtb Manövriertechnisches Büro Aerodynamic body surrounded with air or water
EP0394882A1 (en) * 1989-04-25 1990-10-31 Astrid Holzem Aerodynamic brake for wind turbine blade
DE4446031A1 (en) * 1994-12-23 1996-06-27 Deutsche Forsch Luft Raumfahrt Wing with means for changing the profile
WO2000075508A1 (en) * 1999-06-07 2000-12-14 Bonus Energy A/S Method on regulating the air flow around the windmill wing and device for use in such method

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4715782A (en) * 1985-12-24 1987-12-29 Fayette Manufacturing Corp. Hydraulic control device for wind turbine

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0283730A1 (en) * 1987-03-14 1988-09-28 Mtb Manövriertechnisches Büro Aerodynamic body surrounded with air or water
EP0394882A1 (en) * 1989-04-25 1990-10-31 Astrid Holzem Aerodynamic brake for wind turbine blade
DE4446031A1 (en) * 1994-12-23 1996-06-27 Deutsche Forsch Luft Raumfahrt Wing with means for changing the profile
WO2000075508A1 (en) * 1999-06-07 2000-12-14 Bonus Energy A/S Method on regulating the air flow around the windmill wing and device for use in such method

Cited By (30)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7469750B2 (en) 2004-09-20 2008-12-30 Owen Oil Tools Lp Expandable seal
EP1674723A3 (en) * 2004-12-23 2011-05-04 General Electric Company Active flow modification on wind turbine blades
JP2006177354A (en) * 2004-12-23 2006-07-06 General Electric Co <Ge> Active flow modification on wind power turbine blade
WO2009080316A2 (en) * 2007-12-21 2009-07-02 Vestas Wind Systems A/S Active flow control device and method for affecting a fluid boundary layer of a wind turbine blade
WO2009080316A3 (en) * 2007-12-21 2010-04-29 Vestas Wind Systems A/S Active flow control device and method for affecting a fluid boundary layer of a wind turbine blade
CN101539119A (en) * 2008-03-07 2009-09-23 歌美飒创新技术公司 A wind turbine blade
EP2098721A3 (en) * 2008-03-07 2011-05-04 Gamesa Innovation & Technology, S.L. A wind turbine blade
US8192161B2 (en) 2008-05-16 2012-06-05 Frontier Wind, Llc. Wind turbine with deployable air deflectors
US8267654B2 (en) 2008-05-16 2012-09-18 Frontier Wind, Llc Wind turbine with gust compensating air deflector
EP2128385A3 (en) * 2008-05-16 2012-04-25 Frontier Wind, LLC. Wind turbine with deployable air deflectors
EP2128385A2 (en) 2008-05-16 2009-12-02 Frontier Wind, LLC. Wind turbine with deployable air deflectors
US10844837B2 (en) 2008-05-16 2020-11-24 Ge Infrastructure Technology, Llc Wind turbine with deployable air deflectors
CN102278288A (en) * 2010-06-11 2011-12-14 通用电气公司 Wind turbine blades with controllable aerodynamic vortex elements
EP2394911A1 (en) * 2010-06-11 2011-12-14 General Electric Company Wind turbine blades with controllable aerodynamic vortex elements
CN102278288B (en) * 2010-06-11 2015-09-16 通用电气公司 With the wind turbine blade of controlled aerodynamic vortex elements
US8061986B2 (en) 2010-06-11 2011-11-22 General Electric Company Wind turbine blades with controllable aerodynamic vortex elements
EP2444658A1 (en) * 2010-10-21 2012-04-25 Siemens Aktiengesellschaft Blade of a wind turbine
WO2012093022A3 (en) * 2011-01-06 2012-08-30 Siemens Aktiengesellschaft Load mitigation device for wind turbine blades
EP2484895A1 (en) * 2011-02-04 2012-08-08 LM Wind Power A/S Vortex generator vane pair with trapezium-shaped base
EP2484898A1 (en) * 2011-02-04 2012-08-08 LM Wind Power A/S Vortex generator device with tapered sections for a wind turbine
EP2503143A3 (en) * 2011-03-22 2015-01-21 General Electric Company System and method for increasing energy capture by wind turbines
CN102434393A (en) * 2011-12-31 2012-05-02 深圳市风发科技发展有限公司 Vertical axis wind turbine brake device
ES2388514A1 (en) * 2012-05-18 2012-10-16 Manuel Torres Martínez Wind turbine blade of variable geometry with passive control
WO2015132882A1 (en) * 2014-03-04 2015-09-11 中国電力株式会社 Wind power generation device
JPWO2015132882A1 (en) * 2014-03-04 2017-03-30 中国電力株式会社 Wind power generator
EP3667068A1 (en) * 2018-12-13 2020-06-17 Siemens Gamesa Renewable Energy A/S Adaptable spoiler for a wind turbine blade
WO2020120005A1 (en) * 2018-12-13 2020-06-18 Siemens Gamesa Renewable Energy A/S Adaptable spoiler for a wind turbine blade
TWI745792B (en) 2018-12-13 2021-11-11 丹麥商西門子歌美颯再生能源公司 Adaptable spoiler for a wind turbine rotor blade, wind turbine rotor blade and wind turbine
US11761423B2 (en) 2018-12-13 2023-09-19 Siemens Gamesa Renewable Energy A/S Adaptable spoiler for a wind turbine blade
US11767822B2 (en) 2018-12-13 2023-09-26 Siemens Gamesa Renewable Energy A/S Wind turbine blade flow regulation

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ES2240519T3 (en) 2005-10-16
DK1320680T3 (en) 2005-07-11
DE60110098D1 (en) 2005-05-19
EP1320680A1 (en) 2003-06-25
DK174261B1 (en) 2002-10-21
AU2001291641A1 (en) 2002-04-15
EP1320680B1 (en) 2005-04-13
DK200001450A (en) 2002-03-30
ATE293213T1 (en) 2005-04-15
US7419356B2 (en) 2008-09-02
US20030091436A1 (en) 2003-05-15
DE60110098T2 (en) 2006-05-18

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