Method and control device for a wind turbine, and computer program product, digital storage medium and wind turbine
10428795 ยท 2019-10-01
Assignee
Inventors
Cpc classification
F05B2270/802
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F03D7/0248
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F05B2270/309
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F05B2270/101
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F03D7/024
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F05B2270/328
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F05B2260/30
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F05B2270/1095
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F03D7/0264
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F05B2270/809
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F03D7/022
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F05B2260/902
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F03D7/046
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F05B2270/32
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
F05B2260/31
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F05B2260/903
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F05B2270/326
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F03D15/20
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F05B2260/901
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F05B2270/303
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F05B2270/327
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F03D7/0272
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F05B2260/301
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F03D7/042
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F03D80/50
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
International classification
F03D7/02
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F03D7/04
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F03D80/50
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F03D15/20
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Abstract
The invention concerns a method of operating a wind power installation in which the rotor is brought to a halt and fixed, comprising the steps: braking the rotor, positioning the rotor at a stopped position, and fixing the rotor in the stopped position. According to the invention it is provided that an end position is predetermined, the rotor is braked in regulated fashion to a stopped position associated with the end position, and for positioning for the predetermined end position the rotor is braked in an automated procedure until stopped at the stopped position, and for fixing in the stopped position a mechanical fixing device is applied, in particular automatically.
Claims
1. A method of operating a wind power installation, the method comprising: applying a braking operation on a rotor of a generator of the wind power installation; continuing the braking operation until the rotor gets to a predetermined end position; and stopping and fixing the rotor at the predetermined end position by using a mechanical fixing device configured to fix the rotor at the predetermined end position, wherein stopping the rotor at the predetermined end position comprises using a latching moment of the generator for stopping the rotor at the predetermined end position, wherein the predetermined end position of the rotor is predetermined by predetermining an angular position of the rotor and associating the angular position with a latching position of the generator, wherein the predetermined end position is determined by a discrete latching scale over an angle division on the generator that is predetermined by an arresting groove distribution or pole distribution over a generator ring of the generator, wherein an arresting position distribution is matched to the pole distribution or the arresting groove distribution in such a way that an arresting position of the arresting position distribution coincides with the latching position governed by the latching moment of the generator rotor, and wherein the mechanical fixing device is applied automatically, wherein stopping the rotor at the predetermined end position by the mechanical fixing device comprises engaging an arresting bolt in an arresting hole or groove.
2. The method according to claim 1 wherein fixing the rotor comprises fixing the rotor to a stator of the generator.
3. The method according to claim 1 wherein fixing the rotor comprises fixing a rotor hub housing to a machine house casing.
4. The method according to claim 2 wherein fixing the rotor comprises fixing at least one of a rotor hub and a bearing of the rotor to the stator.
5. The method according to claim 2 wherein fixing the rotor comprises arresting the rotor in a positively locking relationship with the stator.
6. The method according to claim 1 wherein stopping the rotor comprises using a mechanical brake.
7. The method according to claim 1 wherein applying the braking operation includes at least one of the following: activating a mechanical braking action in response to communication from a control device; activating an aerodynamic braking action in response to communication from a control device, and excitation of the generator.
8. The method according to claim 1 further comprising measuring at least one of: a rotary speed and a deceleration of the rotor using an incremental encoder, and using at least one of the rotor speed and the deceleration of the rotor for controlling the braking operation.
9. The method according to claim 1 wherein applying the braking operation comprises exciting pole shoes of the generator rotor with an excitation means that is predetermined in dependence on an excitation brake control value, wherein the excitation brake control value includes one or more values selected from the group of values including: rotary speed, deceleration, external temperature and wind speed.
10. The method according to claim 1 wherein applying the braking operation comprises applying an aerodynamic braking action that includes pitching a rotor blade of the rotor out of the wind and an air brake control value includes one or more values selected from the group of values including: rotary speed, deceleration, external temperature and wind speed.
11. The method according to claim 1 wherein applying the braking operation comprises applying a mechanical brake action that is predetermined by an application brake control in dependence on a brake application control value, wherein the brake application control value includes one or more values selected from the group of values including: rotary speed, deceleration, external temperature and wind speed.
12. The method according to claim 11 wherein the application brake control is calibrated.
13. The method according to claim 11 wherein the application brake control provides learning optimization for optimizing the brake application, including on the basis of a plurality of operational braking operations.
14. The method according to claim 1 wherein the rotor is fixed at the predetermined end position by frictional engagement and positively locking engagement.
15. The method according to claim 1 wherein the mechanical fixing device automatically fixes the rotor at the predetermined end position and forms a positively locking relationship with a stator of the generator.
16. A control device for a wind power installation adapted to carry out the method according to claim 1.
17. A non-transitory computer-readable storage medium having stored thereon executable instructions that, when executed by a control device, cause the control device to perform the steps of the method according to claim 1.
18. A non-transitory digital storage medium for linking to a computer system or a control device, with electronically readable computer-implementable instructions that are configured to co-operate with a computer system or the control device in such a way to implement the method according to claim 1.
Description
BRIEF DESCRIPTION OF THE SEVERAL VIEWS OF THE DRAWINGS
(1) Embodiments of the invention will now be described with reference to the drawing. They are intended not only to necessarily represent the embodiments true to scale, but rather the drawing which serves for description is in diagrammatic and/or slightly distorted form. In regard to additional aspects of the teachings which can be found directly from the drawing, attention is directed to the relevant state of the art. In that respect it is to be borne in mind that many different modifications and alterations concerning the form and the detail of an embodiment can be implemented without departing from the general idea of the invention. The features of the invention disclosed in the description, the drawing and the claims can be essential for further development of the invention both individually and also in any combination. In addition the scope of the invention embraces all combinations of at least two of the features disclosed in the description, the drawing and/or the claims. The general idea of the invention is not limited to the exact form or the detail of the preferred embodiment described and illustrated hereinafter or to a subject-matter which would be restricted in comparison with the subject-matter claimed in the claims. In the case of specified measurement ranges values within the specified limits are also intended to be disclosed as non-equilibrium values and are intended to be used and claimed as desired. Further advantages, features and details of the invention will be apparent from the description hereinafter of the preferred embodiments and with reference to the drawing in which:
(2)
(3)
(4)
(5)
(6)
(7)
(8)
DETAILED DESCRIPTION
(9)
(10) When the rotor 3 is rotating a rotor hub housing 5 rotates relative to a machine house casing 14 which encloses the machine house of the pod 2. In the present case the rotor hub 9 and the blade bearing 8 engage into the rotor hub housing 5. The generator rotor 7.1 is carried in rotatably mounted relationship on a shaft journal 19, like the rotor hub 9, in such a way that a rotary movement of the rotor 3 drives the generator rotor in rotation.
(11) A platform 21 of the machine house 20 carries a number of azimuth motors 22 for actuation of an azimuth bearing in order to orient the pod 2 with its axis A in accordance with a wind direction. On the platform 21 the wind power installation is locally controllable by way of a terminal 31 and a control device 30 of the wind power installation, shown diagrammatically in
(12) If it should be desired to perform measures in the rotor hub housing 15 in a service situationand this possibly applies also to other measures on the wind power installationit is necessary for the rotor 3 to be brought to a halt and arrested in the stopped condition, with the aim of substantially preventing a movement of the rotor but also preventing the wind power installation from re-starting. By way of example
(13) To prepare for the service operation, a wind power installation 1000, 1000A, 1000B is decelerated until the rotor 3 is stationary, due to the operating circumstances involved, by the rotor 3 being mechanically and/or aerodynamically braked. Without the controlled approach of the concept described herein, the rotor 3 would have to be brought to a halt at a rest position which is afforded more or less by estimation, by the braking operation. If that rest position should not coincide with the stopped position in which the rotor can be arrested, the rotor 3 would have to be moved from the inappropriate rest position into an arrestable stopped position. One or more embodiments aim to avoid the rotor 3 coming to a halt in the above-mentioned inappropriate rest position, for then additional effort is required to move the rotor from the inappropriate rest position to the arrestable stopped position.
(14) There is also the disadvantageous possibility of abruptly stopping the rotor 3, while it is still rotating, with a not inconsiderable residual torque, by the rotor being manually caught directly at the arrestable stopped position; that is also referred to as dynamic catching. Dynamic catching is therefore effected by the rotor 3, while still rotating, first being brought to a halt by an arresting action in the stopped position. That procedure transmits considerable loads and moments to a fixing device by means of which the rotor 3 is arrested, and can seriously damage the fixing device; that is therefore to be avoided and is preferably already to be excluded as much as possible, because of the technical aspects involved.
(15) To decelerate the wind power installation to the stopped condition of the rotor, an aerodynamic braking action of the rotor 3 can be used, with a suitable pitch angle, which can be set by pitch motors 61, of the rotor blades 3.1, 3.2, 3.3, which can be implemented by a diagrammatically symbolically illustrated aerodynamic brake 60.
(16) In addition to such an aerodynamic brake 60, it is also possible to use a mechanical operating brake in operation of the rotorthat is to say when the rotor 3 is rotating. A mechanical operating brake can preferably engage a rotating part which is driven by the rotor 3, like for example (this is not the case here and is not shown) directly a rotating shaft. In the case of a drive train of a wind power installation with a stationary axle journal 19 (shown here), the operating brake 40 can basically engage the generator rotor this is preferably shown here and is described hereinafter with reference to
(17) In a modification an operating brake could engage a bearing on the axle journal 19, in particular on a bearing between the generator rotor 7.1 and the axle journal 19 (this is not the case here and is not shown).
(18) A further mechanical operating brake 40 shown by way of example here can be provided additionally or alternatively between a rotating part of the pod 2 and a stationary part of the pod 2, for example between the rotor hub housing 15 and the machine house casing 12.
(19) Additionally or alternatively to at least one of the mechanical operating brakes 40, 40 which are diagrammatically shown by way of example in
(20) Hereinafter the arresting device 50 is described in greater detail with reference to
(21) In general further to illustrate a frictional engagement, brake pads or shoesmounted to a rotating part of the wind power installation 1000can engage a brake disc mounted on a stationary part of the wind power installation 1000 to stop or arrest the rotating part of the wind power installation. Similarly brake pads or shoes of a stationary part of the wind power installation which engage a brake disc on a rotating part of a wind power installation can be used for a mechanical operating brake. In particular in the present case it is possible to implement a mechanical operating brake 40 in combination with an arresting means. In the present case the mechanical operating brake 40 is used in an enlarged functionality with further increased operating brake pressure, as the first part of an arresting action.
(22) The arresting means which is possibly also implemented alone, that is to say also without the above-mentioned mechanical operating brake 40, is described hereinafter by means of the fixing device 50 of
(23) Hereinafter the same reference is used for identical or similar features or features of an identical or similar function, for the sake of simplicity; in particular the fixing device 50 is described in relation to
(24)
(25) The generator stator 7.2 is held by a number of stator carrier arms 17 fixed to a stator star 18. The axle journal 19 and the stator star are carried by a machine carrier 24 on an azimuth bearing in the machine house 20.
(26) To illustrate the fixing device 50 the generator rotor 7.1 has at the edge of a carrier structure 17P a fixing arm 16 with a number of fixing grooves 16N and a friction surface 16S. It should be noted that such a fixing arm which is not identified in greater detail here can also be formed at an edge of the rotor hub housing. In the present case the fixing arm 16 co-operates with a fixing means 14 to represent the above-mentioned fixing device 50 (or in a modification to represent a fixing device 50 between the machine house casing 12 and the rotor hub housing 15). The fixing device 50 (or fixing device 50) is described generally with reference to
(27)
(28) In general, to represent a positively locking connection, for example an arresting bolt 51 can engage into an arresting groove 52 in a rotating part of the wind power installation 1000 to stop the rotating part of the wind power installation. A second part of an arresting means can be formed in that way.
(29) In a present embodiment shown in
(30) The brake pad 41 is adapted for application to the brake disc 42 and is firstly part of a mechanical operating brake 40. When the rotor 3 is stopped and with an increased brake pad contact pressure, the brake pad 41 in combination with the brake disc 42 serves as the first part of a mechanical fixing device 50 by means of which the rotor 3 can be fixed. Additionally the brake disc 42 has a number of above-mentioned grooves 16N as arresting grooves 52, which are associated with a number of arresting bolts 51 engageable into the arresting grooves 52. The combination of arresting bolts 51 and arresting grooves 52 as the second part of the mechanical fixing device 50 forms a genuine arresting means whichonce setstops the rotor 3 securely and independently of external circumstances (like wind speed and network availability) and avoids the risk of movement, and indeed re-starting.
(31) In that respect there is basically the problem described generally hereinbefore, that in particular, in the case of a parking brake implemented by positively locking engagement, or the like arresting deviceas with the described second part of the mechanical fixing device 50there are only given stopped positions, for example P1, P2 in
(32) To overcome the described problems on the example of the wind power installation 1000
(33) The brakes 40, 40, 50 as well as 60 and 70 are controllingly connected to the control device 30. In the present case a braking system 200 is connected to the system 100, referred to as the rotor-generator assembly, comprising pod 2, generator 7 and rotor 3, namely to one or more of the brakes 40, 40, 50, 60 and/or 70 which is controllingly connected to a braking module 210 in the control device 30, by way of interfaces 240, 250, 260, 270, for actuation of the brake or brakes; that is to say for controlling of the electrically and/or hydraulically applicable mechanical operating brake 40, for automatically implementing the arresting action by means of the mechanical fixing device 50, for actuation of the aerodynamic brake 60 and for actuation of the electromagnetic brake 70. The braking module 210 can be operated by way of suitable control lines shown in broken line, which can be operated by way of terminals 31, 31, 31. A keyboard and/or a monitor are connected as an input terminal to the control device 30, which makes it possible to input a desired end position of the rotor 3.
(34) The braking module 210 receives measurement values in relation to controlling parameters from a sensor system 230 which has at least a wind speed sensor Sv, a rotary speed sensor Sn and a deceleration sensor Sa. The braking module 210 can be calibrated by way of a calibration module 220.
(35) In principle the braking system 200 makes it possible for the system 100 comprising rotor 3 and generator 7 at/in the pod 2 of the wind power installation 1000, that is to say the rotor 3 and the generator 7, to be braked in automated fashion in operation and braked down to a stopped condition at the end position in positionally accurate relationship, by means of one or more of the controlled brakes 40, 40 and 60 and 70 and by way of the arresting means as part of the mechanical fixing device 50 (in a modification additionally or alternatively the fixing device 50) to arrest it in the stopped condition practically at the desired end position.
(36)
(37) The stationary part of the wind power installation 1000A, 1000B can be formed by a machine house casing 12. The part of the wind power installation that is movable as part of the rotor 3, that is to say that rotates, can be the rotor hub housing 15 of the rotor 3.
(38) In the preferred embodiment in
(39) The arresting bolt 51 with the arresting groove 52 forms the arresting device in the form of the second part of the mechanical fixing device 50. The arresting bolt 51 can be applied to the arresting groove 52 in the radial direction R by way of a motor means 53for example an electric motor or a hydraulic means or a pneumatic means or a magnetic actuatorand with suitable relative positioning along the periphery Uthat is to say with coincident angular positions of an arresting groove 52 and an arresting bolt 51the arresting bolt 51 can be moved into the arresting groove 52, by actuation of the motor means 53. The motor means 53 can possibly also be such that it already moves along the radius R when the arresting bolt 51 is only partially disposed at the angular position of the arresting groove 52. The arresting groove 52 has opening flanks 52.1, 52.2 which can receive the arresting bolt 51 in a funnel configuration, so that it can self-adjustingly move into the arresting groove 52. Correspondingly the arresting bolt 51 has an outside surface 51.1 which tapers substantially in a conical shape and which is of an inclination which is substantially the same in magnitude or which is somewhat steeper, than the flanks 52.1, 52.2 of the arresting groove 52.
(40) The mechanical operating brake 40 is in the form of a disc brake; it therefore has a functionality provided by the co-operation of brake pads 41 and brake disc 42. The only symbolically illustrated brake pads 41 can also exert friction on the brake disc 42 in operation of a wind power installation 1000, that is to say with the rotor 3 rotating or with the rotor housing 15 rotating, in frictional engagement.
(41) Particularly in combination with the aerodynamic brake 60 this supports a highly effective possible way of bringing the rotor 3 rapidly to a halt, including in emergency situations. Usually the aerodynamic brake 60 is sufficient to decelerate the rotor to a freewheeling movement in a normal process of decelerating the wind power installation, and then using the mechanical operating brake 40 to bring the rotor 3 to a halt. Bringing the mechanical operating brake 40 into operation when the rotor 3 is still rotating, particularly in an emergency situation, when the rotor 3 is still rotating for example in the load range, means that the mechanical operating brake 40 increases the load moment on the rotor 3, that is to say deceleration thereof, to a quite considerable extent. In a serious situation the mechanical operating brake 40 represents a reliable means of bringing the rotor 3 to a halt, even when there is no network load.
(42) It has been found that in additionbut possibly not in every case, in particular not for example when there is no networkload an electromagnetic brake 70 can be used to provide for automatic positioning of the rotor 3 relative to the stationary part of the pod 2 in such a way that arresting bolts 51 and arresting grooves 52 are identical in their angular positions. It has been found that controlled braking of the rotor 3 to the stopped condition, by means of controlling excitation, is comparatively easily possible. As a result, it is then possible to use as the brake, an aerodynamic brake 60 and the mechanical operating brake 40 (also referred to as the holding brake) and, possibly when there is a network supply, also an electromagnetic brake 70.
(43) The particularly preferred method of braking the rotor 3 in an automated procedure provides in a first basic part of the method S-I, automated braking by means of the aerodynamic brake 60, particularly preferably utilizing excitation of the generator rotor 7.1, that is to say an electromagnetic brake 70. If the situation is not an emergency situation, a mechanical brake 40 can additionally decelerate the residual rotary movement of the rotor, beneath a certain threshold speed of the rotor, that is to say when it is only still freewheeling or is rotating only very slowly. Then, in a second basic part of the method S-II, automatic positioning of the rotor 3 relative to the stationary part of the pod 2 is effected, in particular in such a way that an arresting groove 52 comes to a stop practically opposite an arresting bolt 51; at any event however, at approximately the same angular position. It has been found that a latching moment of the generator 7 can advantageously be used in the positioning operation to stop the rotor within a latching unit. It has been found that the operation of braking the rotor 7 to the stopped condition can be effected by means of control/regulation of the excitation of the generator rotor and/or by means of control/regulation of the mechanical operating brake 40, more specifically in such a way that, with a residual movement, the result is exact positioning in the stopped condition, which makes it possible to provide an arresting action in the third basic part of the method S-III.
(44) In the third basic part of the method S-III automatic or manualhere automaticbolting engagement of the rotor is effected by introducing an automatic arresting bolt 51 into an arresting groove 52, as generally shown in
(45) The combination of an arresting means in accordance with the mechanical fixing device 50 and also a holding brake or operating brake 40 of mechanical nature has proven particularly good in the context of a disc brake as shown here. For that purpose a brake disc 42 of the disc brake has not only a brake surface (for example the above-mentioned friction surfaces 16S) which can be gripped in frictional engagement by brake pads 41, but in addition a number of arresting grooves 52 (above-mentioned grooves 16N) into which a or a number of arresting bolts 51 can engage. The reference to a number is basically used to mean one or more, that is to say one, two, three and so forth.
(46)
(47) The method follows the basic structure with braking of the rotor 3 in a first part of the method S-I, positioning the rotor 3 at a stopped position in a second part of the method S-II and arresting the rotor 3 in the stopped position P1, P2 in a third part of the method S-III. In specific terms it is provided here that in a first part S-I, automated braking is effected by means of an aerodynamic brake 60 (by means of the pitch angle of the rotor blades 3.1, 3.2, 3.3), preferably in combination with braking by excitation of the rotor by way of an electromagnetic brake 70. In specific terms it is provided here that in the second part S-II, automatic positioning of the rotor relative to the stationary part of the pod (for example positioning of the arresting grooves relative to the arresting bolts) is effected, in particular by means of the latching moment of the generator 7, and controlled braking of the rotor 3 to the stopped condition (control of excitation by way of an electromagnetic brake 70 and control of the holding brake in the form of the mechanical operating brake 40, 40). In specific terms it is provided here that in the third part S-III an automatic or manual bolting operation on the rotor is effected by means of the mechanical fixing device 50 (for example by introducing the arresting bolts into the arresting grooves=positively locking engagement) or the arresting action is produced by the holding brake (frictional engagement); this is with the aim of reliably preventing the rotor from re-starting.
(48) In a first step S1 the wind power installation is put into the service status. In a second step S2 a selection of the required end position, that is to say the holding position, is effected by way of a key, keyboard or display and other man-machine interface (MMI) for bolting/arresting the installation. That holding position can be specified for example, having regard to the relative orientation of the generator rotor 7.1 relative to the generator stator 7.2, as the stopped position. Thus a position between 0 and 360 can be selected for a given rotor blade, for example for the rotor blade 3.1, as its end position, for example rotor blade 3.1 at the 12 o'clock position, and is then to be associated with a stopped position latched by way of the relative orientation of the generator rotor 7.1 relative to the generator stator 7.2.
(49) In a third step S3 an aerodynamic brake 60 can be actuated by operating the pitch motors 61 to rotate the rotor blades 3.1, 3.2, 3.3 of the rotor 3 out of the wind. The rotor 3 freewheels; deceleration of the rotor occurs by means of the aerodynamic brake 60, as a consequence of turbulence and eddy separation phenomena.
(50) In a fourth step S4 the rotary speed and deceleration of the installation can be ascertained.
(51) In a fifth step S5 an additional excitation is applied to the pole shoes of the rotor 3 to increase the deceleration; in particular by means of the electromagnetic brake 70. The excitation is automatically selected in dependence on the prevailing rotary speed n and the prevailing deceleration a. In that way it is possible to implement controlled but at any event controlled braking of the rotor 3. Regulation of excitation can be found to be faster and more accurate than regulation of the mechanical operating brake 40.
(52) The steps S2 to S5 substantially correspond to the automated braking operation in the first part of the method S-I. The steps S6 to S8 and S10 substantially correspond to the automated positioning operation in the second part S-II. Steps S1 and S9 substantially correspond to the automated arresting operation in the third part S-III.
(53) In a sixth step S6 software or the like computer program product can be made available, which automatically calculates the rotary speed n and the position S at which the mechanical brake 40 is applied. That can be implemented by simultaneous braking by means of the electromagnetic brake 70, for example by excitation of the generator, in particular the generator rotor 7.1. In that way the rotor 3 is brought to a stop in a controlled fashion in such a way that the stopped position which is approached in accordance with the preset end position is associated in coincident relationship with an arresting position which is predetermined in fixed relationship with the installation, in particular in the case of a fixing device which is automatically applied with positively locking engagement thereof. To facilitate matters, arresting position distribution is matched to an arresting groove and/or pole distribution in such a way that an arresting position of the arresting position distribution is coincident with a latching position, governed by a latching moment, of the generator rotor. The last positioning operation can therefore be implemented by a latching moment of the generator 7. In the
(54) In particular for that purpose a seventh step S7 for calculating the necessary deceleration values of the braking system 200 by way of the incremental encoder generally a sensor Sn, Sa of the sensor system 230 involves ascertaining values in a preliminary stage in a test braking operation, and providing for correction or optimization in the following braking operations. In that way it is possible to provide for calibration or continuous adaptations in ongoing operation of the deceleration values of the mechanical brake 40 and/or the electromagnetic brake 70, for example in a calibration module 220 of the controlling device 30; this is also in regard to the acute condition of a brake of the braking system 200 and possibly also in dependence on an outside temperature or a wind speed (measured by the sensor Sv) of the wind power installation 1000.
(55) In an eighth step S8 the rotor 3 then automatically comes to rest, more specifically at that stoppage position which is associated with the end position defined in step S2, wherein a holding brake can be activated in the stopped position not only by frictional engagement (for example by frictionally closing the brake pads 41 against the brake disc 42) but also an arresting action (for example by applying at least one arresting bolt 51 to an arresting groove 52 in positively locking relationship).
(56) In a ninth step S9 a bolting-in engagement operation or other arresting of the rotating part relative to the non-rotating part here the rotor hub housing 15 relative to the machine house casing 12can be effected manually or automatically, by means of the mechanical fixing device 40, in the form of the arresting device, as shown by way of example in
(57) If however for operational reasons, the controlling procedure in step S10 should have to be interrupted and an assumed stopped position in step S9 should not have been arrestable, the parts S-II and S-III of the method for positioning and arresting the rotor 3 can be repeated, or one or more blades 3.1, 3.2, 3.3 can be pitched into the wind at times in order to increase the rotary speed n again and finally to arrive at an arrestable stopped position. An advantage with the method is the degree of reliability in the context of the controlling loop so that this can be automatically repeated without endangering the service personnel P. In particular, by making use of excitation, deceleration of the mechanical brake 40 and/or the aerodynamic brake 60 can additionally be achieved, so that the deceleration of the rotor 3 can be controlled markedly more accurately. For, the electromechanical brake 40 as the operating brake basically has only two conditionsclosed or openwhile excitation can be adapted continuously or stepwise, for example in a ramp or the like, and for example can be set at 30% or another suitable value of maximum excitation. Thus a controlling circuit with the controlling device 30 and the sensor system 230 and braking system 200 (mechanical brake 40 and/or electromagnetic brake 70 and/or aerodynamic brake 60) permits pin-point positioning of the rotor 3 in the stopped condition at an arrestable stopped position and then automatic arresting thereof in the stopped position, without any problem.
LIST OF REFERENCES
(58) 1 pylon 2 pod 3 rotor 3.1, 3.2, 3.3 rotor blades 4 spinner 5 rotor head 7 generator 7.1 generator rotor 7.2 generator stator 7P poles 7S stator winding 8 blade bearing 9 rotor hub 12 machine house casing 14 fixing means 15 rotor hub housing 16 fixing arm 16N, 16S grooves, friction surface 17S, 17P stator carrier arm, carrier structure 18 stator star 19 axle journal 20 machine house 21 platform 22 azimuth motors 23 azimuth bearing 24 machine carrier 30 sensor 30 controlling device 31, 31, 31 terminal 40, 40 operating brake, in particular disc brake 41 brake pad 42 brake disc 45 aerodynamic brake 50 fixing device, operating brake with arresting 51 arresting bolt 51.1 outside surface 52 arresting groove 52.1, 52.2 opening flanks 53 motor means 60 aerodynamic brake 61 pitch motor 70 electric brake 100 system comprising rotor 3, generator 7 and pod 2 200 braking system 210 braking module 220 calibration module 230 sensor system 240, 250, 260, 270 interfaces 1000, 1000A, 1000B wind power installation A axis a deceleration n rotor rotary speed P service personnel P1, P2 stopped position R radial direction r radius S position Sv, Sn, Sa sensors for measuring wind speed v, deceleration a, rotor speed n S-I, S-II, S-III parts of the method U periphery S1-S10 method steps 1 to 10
(59) The various embodiments described above can be combined to provide further embodiments. All of the U.S. patents, U.S. patent application publications, U.S. patent applications, foreign patents, foreign patent applications and non-patent publications referred to in this specification and/or listed in the Application Data Sheet are incorporated herein by reference, in their entirety. Aspects of the embodiments can be modified, if necessary to employ concepts of the various patents, applications and publications to provide yet further embodiments.
(60) These and other changes can be made to the embodiments in light of the above-detailed description. In general, in the following claims, the terms used should not be construed to limit the claims to the specific embodiments disclosed in the specification and the claims, but should be construed to include all possible embodiments along with the full scope of equivalents to which such claims are entitled. Accordingly, the claims are not limited by the disclosure.