Brake system, generator and wind turbine
09906099 · 2018-02-27
Assignee
Inventors
Cpc classification
F03D7/0248
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
H02K2213/12
ELECTRICITY
F05B2260/31
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F03D80/70
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F03D80/00
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F05B2260/902
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
H02K7/1838
ELECTRICITY
F03D9/25
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F03D80/88
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
F03D9/00
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F03D7/02
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
H02K7/18
ELECTRICITY
F16D63/00
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F03D80/00
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F03D9/25
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Abstract
A brake system, especially for a generator, including a rotor assembly, a stator assembly and a rotation axis is disclosed. The rotor assembly includes an outer portion which is located radially outward of the stator assembly. The outer portion includes a brake disc, and the stator assembly comprises at least one frictional member operatively configured for frictionally engaging at least a portion of the brake disc.
Claims
1. A wind turbine generator comprising: a horizontal axis of rotation; a stator assembly; a rotor assembly which comprises an outer portion located radially outward of the stator assembly and rotatable about the horizontal axis of rotation; a brake disc extending radially inward from the outer portion of the rotor assembly towards the axis of rotation, the brake disc comprises a plurality of radial segments; the stator assembly comprises a frictional member, which is operatively configured for frictionally engaging at least a portion of the brake disc, the frictional member comprises a brake caliper system, the caliper system comprises at least two brake calipers which are located on each side of the brake disc opposite to each other; and a radial distance between the brake disc and the frictional member is less than an air gap formed between the rotor and the stator, wherein the brake calliper system is aligned to the brake disc so that no bending moment is experienced at a fixation point of the brake calliper system.
2. The wind turbine generator as claimed in claim 1, wherein the rotor assembly comprises a flange and the brake disc is fastened to the flange.
3. The wind turbine generator as claimed in claim 1, wherein the stator assembly comprises a stationary shaft with a center line of the longitudinal portion of the stationary shaft at the axis of rotation, and wherein the frictional member is connected to the stationary shaft.
4. The wind turbine generator as claimed in claim 1, wherein the stator assembly comprises a bed frame of a wind turbine and frictional member is connected to the bed frame.
5. The wind turbine generator as claimed in claim 1, wherein the stator assembly comprises a stator support structure and the frictional member is connected to the stator support structure.
6. The wind turbine generator as claimed in claim 1, wherein the at least two brake calipers extend radially outward regarding the axis or rotation such that a frictional part of each of the at least two brake calipers is perpendicular to the axis of rotation.
7. The wind turbine generator as claimed in claim 1, wherein the brake system comprises a rotor lock system.
8. The wind turbine generator as claimed in claim 7, wherein the brake disc comprises a plurality of recesses and wherein the stator assembly comprises a piston for engaging with one of the plurality of recesses.
9. The brake system as claimed in claim 8, wherein the lock system comprises an automatic actuator for pushing the piston into one of the plurality of recesses.
10. The wind turbine generator as claimed in claim 8, wherein each of the plurality of recesses extend radially into the brake disc and the piston engages in a radial direction with one of the plurality of recesses.
11. The wind turbine generator as claimed in claim 8, wherein each of the plurality of recesses are spaced symmetrically around the brake disc.
12. A wind turbine comprising: a hub; and a wind turbine generator as claimed in claim 1, the wind turbine generator having a near side facing the hub and having a far side opposite to the hub, the generator includes a front endplate at the near side, wherein the brake disc and the brake caliper system are located at the far side.
13. The wind turbine generator as claimed in claim 1, wherein the radial distance between the brake disc and the frictional member is between 1 mm and 5 mm.
14. The wind turbine generator as claimed in claim 1, wherein the radial distance between the brake disc and the frictional member is between 2 mm and 4 mm.
15. The wind turbine generator as claimed in claim 1, wherein the air gap formed between the rotor and the stator is between 4 mm and 10 mm.
16. The wind turbine generator as claimed in claim 1, wherein the air gap formed between the rotor and the stator is between 5 mm and 7 mm.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
(1) Further features, properties and advantageous of the present invention will become clear from the following description of an embodiment in conjunction with the accompanying drawings. All features are advantageous alone or in combination with each other.
(2)
(3)
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(5)
(6)
(7)
(8)
DETAILED DESCRIPTION OF INVENTION
(9) An embodiment of the present invention will now be described with reference to
(10)
(11) The stator assembly 7 further comprises a frictional member, in the present embodiment a brake calliper system 13. The brake calliper system 13 is operatively configured for frictionally engaging at least a portion of the brake disc 12. The brake calliper system 13 extends radially outward from the stationary shaft 10 to the brake disc 12. The brake calliper system 13 comprises at least one brake calliper on each side of the brake disc 12 in order to enclose the brake disc 12.
(12) The radial distance 22 between the brake disc 12 and the brake calliper system 13 is less than the radial distance 23 (air gap) between the outer rotor portion 11 and the stator assembly 7. Advantageously, radial distance 22 is between 1 mm and 5 mm, preferably between 2 mm and 4 mm. Preferably, the air gap 23 has a width between 4 mm and 10 mm, advantageously between 5 mm and 7 mm.
(13)
(14) Generally, the brake disc 12 can be divided into radial segments 12a, 12b and 12c. The brake disc 12 can also be divided into any other number of radial segments. This makes it possible to exchange a large brake disc 12 easily.
(15) The brake system further comprises a number of central mounted flanges 14, in the present embodiment three central mounted flanges 14. The flanges 14 are mounted to the stationary shaft 10. The flanges 14 are staggered about an angle of 120 regarding the circumference of the stationary shaft 10. Alternatively any other number of the flanges 14 is possible. Preferably the flanges 14 are arranged around the circumference of the stationary shaft 10 such that adjacent flanges have an equal distance to each other.
(16) The brake system comprises at least one rotor lock system 17. The rotor lock system 17 comprises at least one piston 16. The piston is located inside the flange 14 or is located inside of a lock casing. The lock casing can be connected to the flange 14. Alternatively, the brake system can comprise separate flanges for housing the pistons or for being connected with at least one lock casing of the rotor lock system 17 and separate flanges 14 being connected with the brake system, especially the brake calliper system 13.
(17) The pistons 16 are located such that they are prepared to engage with the recesses 15 in the inner surface 21 of the brake disc 12. Preferably, the rotor lock system 17 comprises an automatic actuator. The automatic actuator may be configured for actuating the rotor lock. Especially, the rotor lock system 17 may comprise an automatic actuator for pushing the pistons 16 into the corresponding recesses 15. Preferably the actuator comprises hydraulic or electrical means, for instance a hydraulic cylinder. Instead of recesses also holes can be present in the brake disc 12 and instead of pistons also pins may be used.
(18) Instead of the described rotor lock system 17 comprising a number of pistons 16 also a lock system comprising an interlock, a snap-in lock, a block, an arrest, a barricade or a similar means may be used.
(19)
(20) The actuation force for actuating the brake callipers 13A and 13B is designated by an error 18. When the brake callipers 13A and 13B are actuated, they frictionally engage a portion of the brake disc 12.
(21) The wind turbine 1 may comprise a bed frame or a support structure of the stator. In this case the brake calliper system 13 can be mounted directly to the bed frame of the wind turbine 1 or to the support structure of the stator.
(22)
(23) Preferably the inventive brake system is located at the far side 20 of the generator 6 opposite to the hub 4. This allows for an easy access to the brake system and the integrated rotor lock system, especially for maintenance and service. Alternatively, the inventive brake system may be located at the hub. For example, the inventive brake system may directly be connected to the hub.
(24)
(25) A tower flange 304 is arranged on the top of the tower 303. A bedplate 305 is attached to the tower flange 304. The wind turbine 401 comprises a yaw systemnot shown herewhich is used to turn the bedplate 305 of the wind turbine 301 around the axis 300.
(26) The wind turbine 301 comprises a stationary shaft 306, while the shaft 306 has a centre axis 200. The rear side of the stationary shaft 306 is attached to a retaining arrangement 307. On the front side of the stationary shaft 306 a stator arrangement 308 of the direct drive generator 302 is arranged. The stator arrangement 308 comprises a stator support structure 309 and a lamination stack 310. The lamination stack 310 supports windings 311.
(27) The stator support structure 309 comprises two support elements 312 for a two side support of the lamination stack 310. The support elements 312 are ring-shaped. They are attached to the outside of the stationary shaft 306. A hollow cylindrical support element 313 is attached to the outer ends of the ring-shaped support elements 312. The hollow cylindrical support element 313 carries the ring-shaped lamination stack 310 and the windings 311.
(28) A rotor arrangement 314 is arranged around the stator arrangement 308. The rotor arrangement 314 comprises a front endplate 315 and a cylinder element 317. The front endplate 315 is ring-shaped, while the cylinder element 317 is hollow.
(29) The cylinder element 317 comprises a plurality of permanent magnets 318, which are mounted on the inside of the hollow cylinder element 317. The permanent magnets 318 are arranged opposite to the lamination stack 310 and the supported windings. An air gap 319 with a width of approximately 6 mm is located between the permanent magnets 318 and the lamination stack 310. Preferably, the air gap 319 has a width between 4 mm and 10 mm, advantageously between 5 mm and 7 mm. A brake disc 12 is connected to the cylinder element 317 of the rotor. A brake calliper system 13 is connected to the stationary shaft 306. The radial distance 22 between the brake calliper system 13 and the brake disc 12 is less than the air gap 319. Advantageously, radial distance 22 is between 1 mm and 5 mm, preferably between 2 mm and 4 mm.
(30) The front endplate 315 is arranged on the stationary shaft 306 via a bearing 320. The bearing 320 is capable to transform axial loads in both directions of the centre axis A. An appropriate bearing is disclosed in DE 201 16 649 U1 for example.
(31) The stationary part 321 of the bearing 320 is attached to the stationary shaft 306. The rotating part 322 of the bearing 320 is connected to a mounting ring 323. The front endplate 315 as well as the hub 324 are attached to the mounting ring 323. The hub 324 comprises mounting devices 325 for wind turbine rotor bladesnot shown here.
(32) The air gap 319 shown here is uniform to achieve a constant distance between the elements of the rotor and the elements of the stator. The one bearing design is very attractive due to its easy design.