Patent Application
20090256359
The present invention generally relates to wind turbines and wind power installations, in particular to wind power installations of modular construction.
Different types of modular wind power installations are known. CH 668 623 A5 describes a wind power device with a plurality of stages carrying wind turbines, and wherein each stage can be oriented into the wind independently from the other stages. SU 1645603 A1 relates to a wind power installation wherein an arrangement of wind turbines is hanged from masts. U.S. Pat. No. 5,328,334 discloses a wind power installation, wherein propellers are mounted in series on a wind line that extends between posts. JP 04-350369 relates to an airship moored to ground that carries a plurality of wind turbines. U.S. Pat. No. 4,140,433 discloses wind-driven turbines and arrangements thereof. DE 39 05 337 A1 discloses a method for concentrating the wind stream at a wind turbine with a horizontal axis. WO 2004/099607 discloses a wind turbine a with a rotor, a stator supporting the rotor and a relatively short diffusing circular shroud extending circumferentially around the stator and the rotor, the length of the shroud amounting to about 0.23 times the maximum outer diameter of the shroud. The shroud defines an air channel having a certain air channel diameter at an inlet portion of the shroud amounting to about 0.83 of the maximum outer diameter of the shroud.
Wind power installations comprising a plurality of wind turbines currently suffer from different drawbacks. First of all, the efficiency of the installation may be low because of an adverse interference of neighbouring wind turbines due to eddies caused by the blades of the wind turbines. Second, the complexity of the installations makes it difficult to orient the wind turbines into the wind for optimising the efficiency of the installation. Third, the efficiency of the installations may be suboptimal because of to high a starting wind speed, i.e. the minimum wind speed for the wind turbines to operate. In addition, wind turbines constitute a serious danger for birds.
The invention provides an improved wind power installation module suitable for use in a wind power installation of modular construction.
The invention concerns wind power installation module comprising a substantially streamlined support body. The support body has a substantially drop-shaped horizontal cross section and comprises a nose body having a substantially hemielliptical horizontal cross section and a tail body located downwind of the nose body. The tail body has a junction with the nose body, at which the tail body and the nose body are arranged substantially flush with one another, and departing from which the tail body tapers in downwind direction in such a way that a contour of the tail body follows a parabolic course at least in the horizontal cross section. The wind power installation module further includes wind turbines arranged on the support body at the junction of said nose body and the tail body, each one of said wind turbines including a rotor with a certain number of blades, a stator supporting the rotor in such a way that the rotor may rotate on the turbine axis for generating electric energy and a shroud extending circumferentially around the stator and the rotor and supporting the stator so as to define an air channel that has a certain air channel diameter at an inlet portion of the shroud. The shroud has a maximum outer diameter such that the air channel diameter at the inlet portion of the shroud is comprised in the range from 0.82 to 0.9 times the maximum outer diameter of the shroud. This choice of dimensions provides for minimal aerodynamic losses when the air enters the air channel during operation of the wind turbine. Naturally, this increases the efficiency of the wind turbine. Furthermore, the shroud has a length in direction of the turbine axis that is comprised in the range from 0.1 to 0.25 times the outer diameter. It is worthwhile noting that in longitudinal direction, i.e. in direction of the turbine axis, the shroud not necessarily extends along the entire length of the stator. As will be appreciated, the arrangement of the turbines at the junction of the nose body and the tail body is advantageous in terms of efficiency and starting speed. The junction corresponds to the region where the transversal cross section of the support body is the most important so that the wind speed is increased in the region of the junction.
Preferably, the pitch of the blades is dynamically adjustable to wind speed.
In the wind turbines, the stator preferably includes a central nose portion arranged on the turbine axis upwind of the rotor (for the sake of clarity, the term “nose portion” is used herein for distinction with the “nose body”, which is part of the support body of the module). The central nose portion is preferably rotationally symmetrical with respect to the turbine axis and has the shape of a hemiellipsoid that is rotationally symmetrical about the turbine axis. The diameter of the central nose portion in direction perpendicular to the turbine axis is advantageously comprised in the range from 0.4 to 0.6 times the maximum outer diameter of the shroud, i.e. the air channel diameter, and the length of the central nose portion in direction of the turbine axis is advantageously comprised in the range from 0.4 to 0.5 times its diameter in perpendicular direction.
Advantageously, the stator comprises a central tail portion arranged on the turbine axis downwind of the rotor that includes a substantially rotationally symmetrical tail fairing (for the sake of clarity, the term “tail fairing” is used herein for distinction with the “tail body”, which is part of the support body of the module). At the rotor, the tail fairing has a diameter substantially equal to the diameter of the nose portion. In downwind direction, the tail fairing tapers to the turbine axis so that, in a longitudinal cross section along the turbine axis, the contour of the tail fairing follows a parabolic course.
Most preferably, each one of the wind turbines comprise a protective grid for protection against birds mounted upwind of the rotor.
In a further aspect, the invention concerns wind power installations comprising or consisting of one or more wind power installation modules as discussed above. According to a preferred embodiment, a wind power installation module comprises the substantially streamlined support body, which is rotatably mounted with respect to a vertical axis and supports a plurality of the above wind turbines. The support body has the substantially drop-shaped horizontal cross section and is substantially rotationally symmetrical with respect to a longitudinal support body axis. The plurality of wind turbines are arranged circumferentially around the support body in a plane perpendicular to the support body axis. In addition, the support body comprises a nose body located upwind of the plane in which the wind turbines are arranged, and a tail body located downwind of this plane. The nose body has the shape of a hemiellipsoid rotationally symmetrical about the support body axis. At the plane of the wind turbines, the tail body is arranged substantially flush with the nose body, and it tapers in downwind direction to the support body axis so that, in a longitudinal cross section along the support body axis, a contour of the tail body follows a parabolic course.
According to another preferred embodiment, the support body of the wind power installation module, has the substantially drop-shaped horizontal cross section and substantially vertical outer walls. The first wind power installation module is substantially symmetrical with respect to a longitudinal vertical plane and comprises a nose body of substantially hemielliptical horizontal cross section and a tail body located downwind of the nose body. The tail body is arranged substantially flush with the nose body and tapers in downwind direction to the longitudinal vertical plane. Wind turbines are arranged on the first wind power installation module on both sides thereof with respect to the vertical plane of symmetry. Such modules can be assembled to a wind power installation with a substantially streamlined support body, wherein the support body extends substantially along a vertical axis and comprises a plurality of first wind power installation modules arranged one on top of the other. In order to achieve good efficiency, the wind power installation modules are rotatably mounted about the vertical axis.
According to yet another embodiment, the support body of the wind power installation module has the substantially drop-shaped horizontal cross section, a substantially semicircular transversal cross section and is substantially symmetrical with respect to a vertical, longitudinal plane. It comprises, furthermore, a rounded nose body and a tail body located downwind of the nose body. The tail body is arranged substantially flush with the nose body and tapers in downwind direction. Wind turbines are arranged in a substantially semicircular configuration on the second wind power installation module. Preferably, the turbines of the module are rotatable about a common vertical axis. It should be noted that the second wind power installation module may be arranged on top of a series of the previously discussed wind power installation modules as a terminal module or, alternatively, as a standalone module.
Preferred embodiments of the invention will now be described, by way of example, with reference to the accompanying drawings in which:
a, 7b are side views of a wind power installation similar to that of
a, 10b are side views of a variant of the wind power installation of
The central portion 20 of the stator 14 includes a nose portion 28 arranged upwind of the rotor 16 and a tail portion 30 located downwind of the rotor 16. The nose portion 28 is rotationally symmetrical with respect to the turbine axis 22 and has the shape of a hemiellipsoid of rotation about the turbine axis 22. The tail portion 30 comprises a tail fairing 30 that is rotationally symmetrical with respect to the turbine axis 22 and control surfaces 34.
A protective grid 12 is arranged upwind of the rotor 16, at the inlet of the annular wind channel to avoid that birds are dragged into the turbine by the air stream. The turbine 12 can be rotatably arranged on a mast 36. The protective grid 12 can, for instance, be made of caproic fibres (i.e. coal-plastic fibres). The mesh size of the grid and the material are chosen so that the aerodynamic losses are minimised while offering acceptable protection for birds. Preferably the clear area of the grid amounts to 96-98% of the cross sectional area of the air channel, so that the averaged hydraulic losses due to the grid are comprised in the range from 2-4%.
During operation of the wind turbine 10, the wind enters the turbine 10 from the side of the nose portion 28. The streamlined nose portion 28 directs the incoming wind away from the turbine axis 22, through the protective grid 12, into the annular air channel between the central portion 30 and the shroud 26. The reduction of the cross section available for the wind causes an increase of the wind speed in the annular air channel. In case the streamlined stator blades 24 are located upwind of the rotor blades 18, a preliminary spin is created in the front of the rotor 16. It should be noted, however, that the streamlined stator blades may also be arranged downwind of the rotor 16. The rotor 16 which then transforms the kinetic energy of the wind into mechanical energy of rotation. The rotor 16 drives a shaft that is coupled with an electric generator. Having passed the stator blades 24 and the rotor blades 18, the air leaves the air channel and streams alongside the tail fairing 30 and the control surfaces 34, which turns the turbine 10 upwind.
The power P of wind having the density p, streaming at wind speed V through a cross section A is given by:
The power P1 of an incident airflow streaming through an area of the diameter D1 is
where V1, is the speed and p the density of the incoming airflow. The power P2 of the airflow streaming through the air channel is
where V2 is the air speed in the air channel, Do is the outer diameter of the air channel (i.e. the inner diameter of the shroud 26), Di is the inner diameter of the air channel (i.e. the diameter of the nose portion 28). The ratio P2/P1 depends on the Do, Di, V1 and V2. It should be noted that V2 depends on the speed of the incoming airflow V1. It has been found that the ratio P2/P1 is maximum if the ratio Di/Do lies in the range of 0.4 to 0.6 and if the ratio LN/Di of the length LN of the nose portion 28 to the diameter Di of the nose portion lies between 0.4 and 0.5. Choosing the dimensions Di/Do and LN/Di in the indicated ranges reduces by a factor 2 the starting wind speed, compared to a conventional wind turbine without a shroud, from approximately V1=4 m/s down to approximately 2 m/s.
In a longitudinal cross section of the turbine 10, as shown in
where x is the distance from the rotor on the turbine axis, d(x) the diameter of the tail fairing at the distance x from the rotor, Di the diameter of the tail fairing at the rotor and LT the length of the tail fairing. In practice, the length LT may be approximately equal to Di or comprised in the range from 1 to 2 times Di.
The length LS of the shroud 26 in the direction of the turbine axis corresponds to at least to the sum of the lengths of the stator blades 24 and the rotor blades 18 in the direction of the turbine axis. Experimental results indicate that an optimum value of the length LS is preferably comprised in the range from 0.1 to 0.25 times the outer diameter DS of the shroud 26. Furthermore, the outer diameter DS is chosen such that the outer air channel diameter Do (i.e. the inner diameter of the shroud 26) is comprised in the range from 0.82 to 0.9 times the outer diameter of the shroud 26.
The nose body 42 has substantially has the shape of a hemiellipsoid, such as e.g. a hemisphere, rotationally symmetrical about the support body axis 46. The plurality of wind turbines 10 are arranged circumferentially around the support body 40 in a plane 48 of greatest diameter of the support body 40, this plane 48 being perpendicular to the support body axis 46. The turbines are arranged so that their axes are substantially parallel with the support body axis 46.
The tail body 44 connects substantially flush to the nose body 42 at the plane 48. In downwind direction, the tail body 44 tapers to the support body axis in such a way that in the longitudinal cross section the contour of the tail body follows the course of a parabola given by:
where DSB is the diameter of the support body 40 at the plane 48, LTB the length of the tail body 44, x′ the coordinate on the support body axis 46 and d′(x) the diameter of the tail body 44 for the coordinate x′.
The length LNB of the nose body 42 in the direction of the support body axis 46 lies in the range from 0.4 to 0.6 times the diameter DSB, i.e. 0.4·DSB≦LNB≦0.6·DSB, more preferably in the range from 0.4 to 0.5 times this diameter DSB, i.e. 0.4·DSB≦LNB≦0.5·DSB. The length LTB of the tail body 44 lies in the range from 1 to 2 times the diameter DSB, i.e. DSB≦LTB≦2·DSB. The diameter DS of the wind turbines 10 lies in the range from 0.4 to 0.6 times the diameter DSB of the support body 40, i.e. 0.4·DSB≦DS≦0.6·DSB.
During operation of the wind power installation 38, the wind blows from the side of the nose body 42, which directs the incoming wind away from the support body axis 46 towards the turbines 10 arranged in a circle around the support body 40 in the plane 48, in which the diameter of the support body 40 is largest. The reduction of available cross section causes the speed of the airflow to increase along the nose body 42. The speed reaches a maximum at the plane 48. Even at low wind speed, the speed of the airflow at the turbines may thus be high enough to start operation of the wind power installation.
To enable orientation of the wind power installation 38 into the wind, the support body 40 is rotatably mounted with respect to a vertical axis 50. This axis 50 preferably intersects with the nose body 42 or with a part of the tail body 44 that is close to the nose body. In this case, the wind power installation can be oriented by the forces of the wind. If the support body axis 46 is not aligned with the direction of the wind, the forces of the wind will create a moment on the support body 40 that turns the wind power installation 38 with the nose body 42 into the wind.
Each wind power installation module 56 has support body with a substantially drop-shaped horizontal cross section, substantially vertical outer walls 58 and is symmetrical with respect to a vertical longitudinal plane 60. Each module 56 has a nose body 62 that normally faces into the wind during operation of the wind power installation 52 and a tail body 64 that normally faces away from the wind during operation of the wind power installation 52. The nose body has a substantially hemielliptical horizontal cross section, whereas the tail body tapers in downwind direction to the plane 60. Each module 56 further comprises, arranged on both sides thereof, with respect to the plane 60, wind turbines 10, whose turbine axes are substantially parallel to the plane 60 and horizontal. The turbines 10 are arranged on the support bodies where width thereof perpendicular to the plane 60 is maximum.
The length LNB′ of the nose body 62 lies in the range from 0.4 to 0.6 times the width DSB′ of the modules, i.e. 0.4·DSB′≦LNB′≦0.6·DSB′, more preferably in the range from 0.4 to 0.5 times this width DSB′, i.e. 0.4·DSB′≦LNB′≦0.5·DSB′. The length LTB′ of the tail body 64 lies in the range from 1 to 2 times the width DSB′, i.e. DSB′≦LTB′≦2·DSB′. The diameter DS of the wind turbines 10 lies in the range from 0.4 to 0.6 times the width DSB′, i.e. 0.4·DSB′≦DS≦0.6·DSB′.
During operation of the wind power installation 52, the wind blows from the side of the nose bodies 62 of the individual modules 56, which directs the incoming wind away from the respective plane 60 towards the turbines 10 arranged laterally on the modules 56 with respect to the direction of the wind. The reduction of available cross section causes the speed of the airflow to increase along the nose bodies 62. The speed reaches a maximum at the planes 60. Even at low wind speed, the speed of the airflow at the turbines 10 may thus be high enough to start operation of the wind power installation 62.
As the support body 52 is rotatably mounted with respect to the vertical axis 54, the wind power installation 52 may orient itself into the wind. For each module 56, the axis 54 preferably intersects with the nose body 62 or with a part of the tail body 64 that is close to the nose body 62. In this case, the modules 56 can be oriented by the forces of the wind. Preferably, the modules 56 can rotate about the axis 54 independently from each other to enable optimal orientation in case of the wind blowing from different directions at different heights from ground. One can also limit the angular motion of neighbouring modules 56 to a certain angle.
During operation, the tail body 72 orients itself downwind under the action of the forces of the wind, so that the turbines 10 become aligned with the wind direction. The nose body 70 remains immobile while the tail body 72 may pivot about the axis of symmetry of the nose body 70.
The horizontal diameter of the nose body 70 substantially corresponds to the lateral diameter of the tail body 72. Indeed, the tail body 72 is substantially flush with the nose body 70. The length LTB″ of the tail body 72 lies in the range from 1 to 2 times the width DTB″, i.e. DTB″≦LTB″≦2·DTB″. The diameter DS of the wind turbines 10 lies in the range from 0.4 to 0.6 times the width DTB″, i.e. 0.4·DTB″≦DS≦0.6·DTB″.
The wind power installation shown in
The module 75 is preferably rotatably mounted about an axis 82. It should also be noted that the module 75 can be arranged as a terminal module on top of a series of modules 56, as shown in
| Number | Date | Country | Kind |
|---|---|---|---|
| 06113881.4 | May 2006 | EP | regional |
| Filing Document | Filing Date | Country | Kind | 371c Date |
|---|---|---|---|---|
| PCT/EP07/54521 | 5/10/2007 | WO | 00 | 10/29/2008 |
