Wind turbine with hinged blades having a hinge position between inner and outer tip end of the blades
11319921 · 2022-05-03
Assignee
Inventors
Cpc classification
F05B2240/2022
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F05B2240/313
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F03D7/0236
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F05B2240/21
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F03D1/0608
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F03D1/0625
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Y02E10/72
GENERAL 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
International classification
Abstract
A wind turbine (1) comprising a tower (2), a nacelle (3) and a hub (7) is disclosed. The hub (7) comprises a blade carrying structure (4) with one or more wind turbine blades (5) connected to thereto. Each of the wind turbine blades (5) defines an aerodynamic profile having a thickness which varies along a length of the wind turbine blade (5). Each of the wind turbine blades (5) is connected to the blade carrying structure (4) via a hinge (6) at a hinge position of the wind turbine blade (5), each wind turbine blade (5) thereby being arranged to perform pivot movements relative to the blade carrying structure (4) between a minimum pivot angle and a maximum pivot angle. The hinge position is arranged at a distance from the inner tip end (5a) and at a distance from the outer tip end (5b), and the thickness, or the thickness-to chord ratio, at the hinge position is larger than the thickness, or the thickness-to-chord ratio, at the inner tip end (5a) and larger than the thickness, or the thickness-to-chord ratio, at the outer tip end (5b).
Claims
1. A wind turbine comprising a tower, a nacelle mounted on the tower via a yaw system, a hub mounted rotatably on the nacelle, the hub comprising a blade carrying structure, and one or more wind turbine blades connected to the blade carrying structure, wherein each of the wind turbine blades extends along a longitudinal direction between an inner tip end and an outer tip end, and defines an aerodynamic profile with a suction side and a pressure side, each extending between a leading edge and a trailing edge, the leading edge and the trailing edge each extending between the inner tip end and the outer tip end, the aerodynamic profile further having a thickness which varies along the longitudinal direction of the wind turbine blade between the inner tip end and the outer tip end, and wherein each of the wind turbine blades is connected to the blade carrying structure via a hinge at a hinge position of the wind turbine blade, each wind turbine blade thereby being arranged to perform pivot movements relative to the blade carrying structure about a pivot axis arranged substantially perpendicular to the longitudinal direction of the wind turbine blade, between a minimum pivot angle and a maximum pivot angle, the hinge position being arranged at a distance from the inner tip end and at a distance from the outer tip end, and wherein the thickness at the hinge position is larger than the thickness at the inner tip end and larger than the thickness at the outer tip end.
2. The wind turbine according to claim 1, wherein the hinge position of each of the wind turbine blades is at a position defining a maximum thickness.
3. The wind turbine according to claim 1, wherein the thickness of the aerodynamic profile of each of the wind turbine blades decreases from the hinge position towards the inner tip end and from the hinge position towards the outer tip end.
4. The wind turbine according to claim 1, wherein each of the wind turbine blades has a centre of mass for the wind turbine blade at rest, the centre of mass being positioned between the hinge position and the inner tip end of the wind turbine blade.
5. The wind turbine according to claim 1, further comprising a balancing mass arranged on the nacelle at a position opposite to an attachment position of the hub.
6. The wind turbine according to claim 1, wherein the wind turbine is a downwind wind turbine.
7. The wind turbine according to claim 1, further comprising biasing means biasing the wind turbine blades towards a position providing a maximum rotor diameter of the wind turbine.
8. The wind turbine according to claim 1, further comprising end stop mechanisms arranged to slow pivot movements of the wind turbine blades in a region near the minimum pivot angle and/or in a region near the maximum pivot angle.
9. The wind turbine according to claim 8, wherein the end stop mechanism comprises a spring and/or a damper.
10. The wind turbine according to claim 1, further comprising a stop mechanism arranged to move the wind turbine blades to a safe pivot angle in the case of an emergency.
11. The wind turbine according to claim 10, wherein the safe pivot angle arranges the wind turbine blades in such a manner that each wind turbine blade extends along a direction which is substantially parallel to a rotational axis of the hub.
12. The wind turbine according to claim 10, wherein the stop mechanism comprises a release mechanism and at least one spring biased wire interconnecting the release mechanism and each of the wind turbine blades.
13. The wind turbine according to claim 1, wherein the blade carrying structure comprises one or more arms, and wherein each of the wind turbine blades is mounted on one of the arms of the blade carrying structure.
14. The wind turbine according to claim 1, wherein each of the wind turbine blades comprises an inner portion including the inner tip end and an outer portion including the outer tip end, and wherein the inner portion and the outer portion are joined to each other.
15. The wind turbine according to claim 14, wherein each of the wind turbine blades further comprises a hinge portion including the hinge position, and wherein the hinge portion interconnects the inner portion and the outer portion.
16. The wind turbine according to claim 1, wherein the hinge of each of the wind turbine blades is embedded in the wind turbine blade.
17. The wind turbine according to claim 1, wherein each of the wind turbine blades is provided with at least one winglet.
18. The wind turbine according to claim 1, further comprising at least one deployable airbrake.
19. The wind turbine according to claim 1, wherein the hinge position of each of the wind turbine blades is at a position defining a maximum chord of the wind turbine blade.
20. A wind turbine comprising a tower, a nacelle mounted on the tower via a yaw system, a hub mounted rotatably on the nacelle, the hub comprising a blade carrying structure, and one or more wind turbine blades connected to the blade carrying structure, wherein each of the wind turbine blades extends along a longitudinal direction between an inner tip end and an outer tip end, and defines an aerodynamic profile with a suction side and a pressure side, each extending between a leading edge and a trailing edge, the leading edge and the trailing edge each extending between the inner tip end and the outer tip end, the aerodynamic profile further having a thickness which varies along the longitudinal direction of the wind turbine blade between the inner tip end and the outer tip end, and wherein each of the wind turbine blades is connected to the blade carrying structure via a hinge at a hinge position of the wind turbine blade, each wind turbine blade thereby being arranged to perform pivot movements relative to the blade carrying structure about a pivot axis arranged substantially perpendicular to the longitudinal direction of the wind turbine blade, between a minimum pivot angle and a maximum pivot angle, the hinge position being arranged at a distance from the inner tip end and at a distance from the outer tip end, and wherein a thickness-to-chord ratio at the hinge position is larger than a thickness-to-chord ratio at the inner tip end and larger than a thickness-to-chord ratio at the outer tip end.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
(1) The invention will now be described in further detail with reference to the accompanying drawings in which
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DETAILED DESCRIPTION OF THE DRAWINGS
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(15) Each wind turbine blade 5 defines an aerodynamic profile having a thickness which varies along the length of the wind turbine blade 5 between an inner tip end 5a and an outer tip end 5b. The hinge 6 is arranged at a hinge position of the wind turbine blade 5, the hinge position 6 being at a distance from the inner tip end 5a as well as at a distance from the outer tip end 5b, and the thickness of the wind turbine blade 5 is larger at the hinge position than at the inner tip end 5a as well as at the outer tip end 5b.
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(18) The pivoting of the wind turbine blades 5 between the position shown in
(19) In the situation illustrated in
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(22) The left most drawing shows the wind turbine 1 at a low wind speed. In this case the rotational speed of the hub 7 is low, and therefore the centrifugal force acting on the wind turbine blades 5 is small. Accordingly, the rotor diameter is maximum.
(23) The middle drawing shows the wind turbine 1 at a wind speed which is higher than the wind speed of the left most drawing. Accordingly, the rotational speed of the hub 7 is higher, and the centrifugal force acting on the wind turbine blades 5 is larger. Additionally, the aerodynamic forces acting on the wind turbine blades 5 are also larger. As a consequence, the wind turbine blades 5 have been pivoted towards a position defining a smaller rotor diameter.
(24) The right most drawing shows the wind turbine 1 at a high wind speed. In this case the rotational speed of the hub 7 is very high, and therefore the centrifugal force acting on the wind turbine blades 5 is large. In addition, the aerodynamic forces at the high wind speed push the wind turbine blades 5 into the shown position. This has the consequence that the wind turbine blades 5 have been pivoted to a position defining a minimum rotor diameter. It can be seen that the wind turbine blades 5 are arranged substantially parallel to a rotational axis of the hub 7. This position is sometimes referred to as ‘barrel mode’.
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(26) An end stop mechanism 11 in the form of a resilient pad is mounted on the blade carrying structure 4. When the wind turbine blade 5 is pivoted to a position defining a minimum pivot angle 10, the wind turbine blade 5 abuts the end stop mechanism 11, resulting in a soft stop for the pivot movement. Thereby collisions between the wind turbine blade 5 and the blade carrying structure 4 are avoided.
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(30) In the left part of
(31) In the right part of
(32) During normal operation, the deployable airbrake 13 may be in the retracted position illustrated in the left part of
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(35) The part of the blade carrying structure 4 which is shown in
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(37) In the wind turbine 1 of
(38) It should be noted that the winglets 18 could, alternatively, extend towards the blade carrying structure 4 and towards the suction side of the wind turbine blades 5. As another alternative, the wind turbine blades 5 could be provided with winglets 18 at the inner tip end 5a extending towards the pressure side as well as towards the suction side of the wind turbine blades 5.
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(40) In the wind turbine 1 of
(41) It should be noted that the winglets 19 could, alternatively, extend towards the pressure side of the wind turbine blades 5. As another alternative, the wind turbine blades 5 could be provided with winglets 19 at the outer tip end 5b extending towards the pressure side as well as towards the suction side of the wind turbine blade 5.
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(43) In the wind turbine 1 of
(44) It should be noted that, even though the winglets 18, 19 illustrated in
(45) It should further be noted that the winglets 18, 19 illustrated in