MULTI-ROTOR WIND TURBINE
This invention relates to large electricity-generating wind turbines, particularly but not exclusively for use offshore, and to the method of mounting the turbines to reduce the capital installed cost, costs of maintenance, and thus cost of energy produced.
It is well known that wind turbines developed for onshore use can be deployed offshore, given an appropriate gravity or piled base that can be used to put in place the tower of the wind turbine via such as a flanged connection joint situated above the high water point at the site. Typically, the turbines are erected using floating or jack-up cranes; or, in more recent developments, by floating out completely assembled tower-nacelle-rotor units fixed to the deck of a barge and lifted into place each as an entire assembly by very large floating or jack-up cranes such as described by Seegers and Hoithausen (Reference 1).
The installation of large single-rotor wind turbines offshore -typically having rotors with three blades -is proving to be very expensive, because of the high capital cost and the high installation cost, involving as it does such large specialist crane equipment. Maintenance has also proven to be very expensive: in the event of a major component failure such as a blade, gearbox or generator, large floating jack-up cranes with the capacity to reach to the top of the support tower are again required and have to be brought in at substantial cost. Because there are few such cranes in existence, there can also be expensive delays both in installing new plant and in replacing that which has failed. These maintenance costs are said to add 25- 30% to the cost of each unit of energy generated by offshore wind installations.
The aim of the invention is to reduce the installed capital cost per unit of energy generated as well as the practicality and ease of maintenance. Applied to a twin rotor configuration, whether onshore or offshore, this invention enables the rotor and nacelle units to be brought down close to sea level, where they are more easily handled, without the need for large cranes. The invention proposes a number of improvements for the operation of a twin rotor configuration, which will further enhance the economic viability compared to present day single rotor turbines.
Applied to wind turbines with 3 or more rotors, additional inventive features enable operation, installation and maintenance in such a way that the overall cost of energy may be further reduced.
Twin rotor configurations have been proposed in various references (see References 2-7). The present invention relates to an arrangement where twin rotors are mounted atop a single tower, such that the orientation into alignment with the wind of the rotors is controlled by regulating the thrust of one rotor with respect to the other, by the use of full or partial blade pitch control. The advantage of such a system is that the twin rotors double the energy capture area of the turbine without a corresponding doubling of the cost of the installation, since there is only a single tower, base and installation operation.
The key aspect of the invention is the method of mounting the rotors and nacelles on a swivelling cross-beam which can be rotated in a substantially vertical plane to bring either rotor/nacelle unit close to the tower base, allowing simple access to the rotors and nacelle machinery, and siniplif'ing and making less costly installation and maintenance activities.
The specific advantages of the invention are: firstly the arrangement whereby the arms carrying the nacelle/rotor units brings these units down to near sea level and close to the tower is more practical than the one proposed by Alexandroff (Reference 2) -where the lowered arms end up substantially horizontal; and from the lowered position, components of the rotor or nacelle may be easily removed to a barge moored by the tower. Secondly, that in comparison to previous twin rotor proposals, the overturning loads on the yaw bearing, inasmuch as this is located at the top of the tower substantially at the same level as the rotors, are significantly reduced from previous proposals where the bearing is located near the ground.
With regard to wind turbines with 3 or more rotors, where the rotor area presented to the wind is large enoug1 to be susceptible to differential wind shear of gusts, another aspect of this invention relates to a means of control whereby the pitch of the blades of each rotor are regulated to maintain an appropriate balance between the thrusts generated by the rotors; whether in the process of starting up, normal running or shutting down; so that the resulting bending loads on critical points on the structure are minimised.
According to the first aspect of this invention, the apparatus comprises of a tower fixed to the sea bed and protruding above the sea surface, upon the top of which is located a cross beam structure on which electricity generating turbines powered by the wind are mounted. A second aspect of the invention comprises a rotor mounted on an arm that can be rotated or moved to bring the rotor close to the sea level for ease of assembly or maintenance. A third aspect of the invention comprises a mechanism of struts and support stays actuated by electric or hydraulic power that can provide movement to the arm and turbine.
These and other features of the invention will be apparent from the following description of a preferred embodiment illustrated, by way of example only, in the accompanying drawings in which: Figure 1 is a schematic view of one embodiment of the invention, showing a twin rotor turbine with the nacelle/rotor units mounted at opposite ends of a cross-beam Figure 2 illustrates the embodiment of Figure 1 with one nacelle/rotor lowered to just above sea level Figure 3 is a side view of Figure 2 showing the relative positioning of the lowered nacelle Figure 4 shows an alternative embodiment of the invention, with two nacelle/rotor units mounted on individual pivoted arms Figure 5 illustrates the embodiment of Figure 4 with the rotors lowered to just above sea level Figure 6 illustrates the embodiment of Figures 4 and 5 from the side view, showing how the rotors stow one in front of the tower and one behind Figure 7 illustrates an alternative embodiment with arm pivot points displaced vertically one from the other Figure 8 illustrates the embodiment of Figure 7 with arms lowered, showing how the rotors stow with one nacelle higher than the other Figure 9 illustrates the embodiment of Figure 7 and 8 from the side view, showing how the rotors stow in front of the tower Figure 10 illustrates the embodiments of Figures 4 and 7 showing how the entire tower, arms, nacelles and rotors may be lifted into place from a barge Figure 11 illustrates an alternative embodiment with the nacelle/rotor units supported below the cross arms Figure 12 further illustrates the embodiment of Figure 11 showing how one nacelle/rotor unit may be lowered to a barge Figure 13 illustrates an alternative embodiment with three nacelle/rotor units supported on a three-arm stmcture Figure 14 further illustrates the embodiment of Figure 13, showing a side view with the three-arm assembly rotated to lower a nacelle to a platform.
According to the arrangement illustrated in Figure 1, rotors I and nacelles 2 are supported on a crossbeam 3 which is mounted by a pivot 27 to a yaw bearing unit 4 that can turn in a horizontal plane to follow the wind. The yaw bearing unit 4 is mounted atop a tower 5 located on a subsea base 6. The crossbeam 3 may be supported by stays 7 attached to a central column 8. In the preferred embodiment the rotors 1 are both mounted upwind of crossbeam 3 so that the rotor blades turn in a predominantly undisturbed airflow. The rotors preferably rotate in opposite directions so as that their torques decrease rather than increase the gravity loads on cross-beam 3. It is also envisaged that it can be arranged for the rotors to rotate in the same direction. Crossbeam 3 may be profiled so as to minimise even further disturbance to the upstream airflow on the rotor. The rotors may either be fixed or teetered with respect to the hub of the drive transmission.
The cross-beam with rotors and drive units can preferably be arranged so that the centre of gravity of the rotatable assembly is located close to the centre of the tower so as to minimise gravity moments on the yaw bearing.
In another aspect of this invention, the rotors may be arranged to run downwind of the supporting crossbeam 3. In this case it will be desirable to profile the arms so as to reduce disturbance to the airflow striking the downwind rotor blades Figure 2 shows how crossbeam 3 may be rotated to a near-vertical alignment so that one nacelle/rotor unit lies alongside the main tower a short distance above the sea surface where it can conveniently be accessed for removal or replacement. The main access platform 9 may be positioned to be at a convenient height for working on the nacelle or rotor. A lifting jib-arm attached to the tower may be used to remove components from the nacelle or rotor and lower to them to a moored boat for replacement.
It will be noted that this arrangement makes possible the approximately even distribution of component masses about the yaw bearing so that overturning moments are kept low -for example from Figures 2 and 3, it can be seen that crossbeam 3 is raked forward at its outer ends so that the lower part is located behind the tower near its pivot point, but in front of the tower at its outer end where the lower rotor I and nacelle 2 are carried.
In the embodiment illustrated in Figure 4, rotors I and nacelles 2 are supported on near-horizontal arms 12 which are in turn located via a hinge system 26 to a yaw bearing unit 4 that can turn to follow the wind. The yaw bearing unit 4 is mounted atop a tower 5 located on a subsea base 6. The arms 12 are supported by stays 13 attached to a central column 14. In the preferred embodiment, rotors 1 are both mounted upwind of the supporting arms 12 so that the rotor blades turn in a predominantly undisturbed airflow. The rotors preferably rotate in opposite directions so as that their torques decrease rather than increase the gravity loads on arms 12, but it is envisaged that the rotors can also be arranged to rotate in the same direction. Arms 12 may be profiled so as to minimise even further disturbance to the upstream air flow on the rotor. The rotors may either be fixed or teetered with respect to the hub of the drive transmission.
In another aspect of this invention, the rotors may be arranged to run downwind of supporting arms 12. In this case it will be desirable to profile the arms so as to reduce disturbance to the airflow striking the downwind rotor blades.
Figure 5 shows how arms 12 may be lowered by stays 13 to a near-vertical alignment alongside the main tower with the rotor/nacelle units carried a short distance above the sea surface where they can conveniently be accessed for removal or replacement via platform 9. Struts 15, cantilevered from the inboard ends of arms 12 assist the stability and control of this process. The stays 13 may be operated by electric winch and cable from within the tower causing a change in length and thus the position the anns are drawn to. This can be in unison or as separate actions thus lowering one arm or the other. The initial installation of the rotor/nacelle units can be accomplished by attaching the rotor/nacelle to the arms and then raising them to the operating position. Platforms 9 may be constructed and attached to the main tower to provide a safe working area above the wave tops and as a convenient temporary location of the rotor/nacelle units. An alternative method of actuating the ann movement can be by such as hydraulic rams acting to move central column 14 vertically and react against a fixed length stay thus causing the stay cable to pull the arms up or allow them to be lowered.
Figure 6 further shows how with reference to Figures 4 and 5, the axes of the pivots on yaw unit 4 carrying arms 3 are arranged so that the nacelles and rotors are lowered fore and afi of the tower so as not to clash either with the tower or with each other.
Another aspect of this invention is illustrated in Figure 7 where the pivots on yaw unit 4 are displaced vertically one from the other. The operational positions of the nacelles and rotors are arranged to still be symmetrical, but when lowered to near-sea level one nacelle/rotor unit fits behind and above the other, both in front of (or both behind) the tower. This is illustrated in Figures 8 and 9. This effect can also be achieved by differential spacing of the pivots away from the tower -thus keeping the arms 12 in the same plane when largely horizontal.
From all the positions described, components of the rotor or nacelle may be removed to a barge moored by the tower.
Figure 10 illustrates a further advantage of this arrangement; whereby the tower and arms, nacelles and rotors in their lowered positions are lifted as a single unit from the deck of a barge 16 on to the pre-prepared subsea base 6. The advantage of this arrangement over the traditional single turbine lift described above is that the centre of gravity of the assembly is now so low that a smaller reach crane can be used to carry out the lift, with lower resulting cost and the greater availability of
suitable means.
Figure 11 shows a further embodiment of the invention where the rotors I and nacelles 2 are supported underneath arms 12 to facilitate them being lifted or removed individually by winches mounted temporarily or permanently to the turbine structure.
Figure 12 shows how, in the embodiment of Figure 11, the rotor and nacelle unit may be lowered to a barge 16 for removal or maintenance. Alternatively the rotor and nacelle may be removed directly to a vessel or attached platform when the arm 12 is in the lowered vertical position.
In another aspect of this invention, three bladed rotors rather than two-bladed rotors may be fitted. Lowering of the arms to the side of the tower will then require removal of one blade so that the other two may be parked pointing upwards for full lowering.
In another aspect of this invention, and referring to the arrangement illustrated in Figure 1, the yaw about the tower of the crossarm 3 or arms 12 carrying the nacelle and rotor units is controlled at zero or low wind speed by yaw drives fitted between the arms and the top of the tower. These allow for initial positioning of the rotors into the wind as the rotors start up, for cable unwinding and for fixing of the yaw for safe maintenance access. At higher windspeeds, with both rotors turning, the yaw is released or over-ridden by controlling the differential thrust moments of the rotors about the yaw axis.
The approach to three-rotor turbines is illustrated by Figure 13. In this embodiment, two nacelle/rotor units 17 and 18 are mounted symmetrically about the yaw axis and the third nacelle/rotor unit 19 in line with it. The arms 20 carrying the nacelle/rotor units are joined rigidly together and mounted by a pivot to the yaw bearing 21 atop tower 22. The pivot enables the entire arm/rotor/nacelle assembly to be rotated for purposes of erection, maintenance or disassembly. The pivot carrying the arms is angled so that at least one of the side nacelle/rotor units passes behind the tower so that rotation may continue to bring the top rotor down to the level of the maintenance platform.
Figure 14 shows the side view, in which one side nacelle/rotor unit is passing S behind the tower. When in the position for nacelle or rotor maintenance, access can be obtained from platform 23.
Four or more rotors can be accommodated by combinations of one or more crossarms with one or more pivoted arms according to the methods described herein for two or three rotor turbines.
In another aspect of this invention, the correct orientation of the rotors to the prevailing wind is controlled by an algorithm regulating blade pitch. This allows alignment with the wind by for instance measurement of rotor speed, power level, blade pitch angle, absolute nacelle orientation about a vertical axis, and wind direction error (ie wind direction relative to the rotor axis). In near-fixed-speed rotor operation (usually fixed speed operation with controlled slip), pitch is controlled so as to spill power from the rotor moving into the wind, as detected by the yaw error signal. The measurement of absolute yaw position is necessary to ensure damping of the response so that unacceptable oscillations about the yaw axis do not develop. It can also be used to moderate the power-spilling response so that energy loss from blade pitching is minimised. In variable speed operation, the rotational speed of the rotor moving into the wind can be reduced so as to limit thrust so that energy is not lost through blade pitching. In this case the algorithm will rely on rotor speed and power measurements in addition to those of pitch, absolute yaw, and yaw error.
In the case of off-power operation, for instance while starting or stopping the rotors, the differential thrusts on the rotor may be calculated from measurement of rotor speed, rotor acceleration and pitch angle; and reduced by making balancing adjustments to pitch angle as before. It will be appreciated that when a rotor is working to maximise power, its thrust is also near to maximum, so that to achieve thrust balance between two rotors it will generally be required to reduce the thrust of the one generating the most power.
With regard to control of rotor thrust for yaw alignment and differential load reduction when three rotors are used, it is another aspect of this invention that thrust balance can be achieved between the rotors so that not only do the side rotors balance each other to achieve alignment with the wind, but that the third rotor balances its thrust with respect to the side rotors so that the pitching moments of the three rotors are balanced about the yaw bearing. In the turbine illustrated in Figure 13, for example may be applied to the control of the pitch of rotors 17 and 18 by the means described above for two rotors so that all three rotors are steered in alignment with the wind direction. In addition, in order to reduce the bending loads at yaw bearing 21, the thrust of rotor 19 with respect to rotors 17 and 18 can also be adjusted so that the thrusts balance. The methods described are used so that the thrusts balance under conditions of start-up, normal generating operation, and shut-down. As before, in very light winds or with the rotors stopped, the yaw position may be held by a light duty drive which may be over-ridden or released when differential rotor thrust exceeds a predetermined magnitude.
A combination of all the features covered in this patent can be envisaged for some applications.
References 1. Seegers and Hoithausen:-Method and apparatus for placing at least one wind turbine on open water; UK Patent GB2390632B 2. Ajexandroff:-Aerogenerator Birotor; European Patent EP0761964A1, 1996 (lapsed) 3. Deiji:-Windkraftanlage; German Patent DE3113247A1, 1982 4. Honnef:-Windkraftmaschine, deren Treibflugelspitzen durch einen Radkranz miteinander in Verbindung stehen; German Patent DE549618C1, 1932 5. Freidmund:-Bezeichnung des Gegenstandes Windkrafianlage; German Patent DE9419057, 1994 6. Struble:-Improvements in Wind Motor Power Plants; UK Patent GB33 1683, 1930.