This application claims the benefit of priority of U.S. Provisional Patent Application Ser. No. 61/422,486, filed Dec. 13, 2010, and titled “Apparatus for Maintaining Air-Gap Spacing in Large Diameter, Low-Speed Motors and Generators,” which is incorporated by reference herein in its entirety.
The present invention generally relates to the field of wind power units. In particular, the present invention is directed to an apparatus for maintaining the air gap in large diameter, low speed motors or generators and similar electromechanical machines.
Embodiments of the present invention comprise a rotor-stator structure including plural bumper elements that may employ synthetic sliding bearing surfaces, mounted to the stator, and designed to contact a machined surface on the rotor if generator structural deflection occurs during operation. During normal operation, the bearing surface is not in contact with the machine rotor. If extreme loads imposed on the rotor or stator structures, or other issue like bearing failure, causes the air gap to close, the bumper elements will “touch down” on a machined surface on the rotor to maintain a minimum air gap. In one exemplary embodiment, the machined surface on the rotor may be the rotor brake disc.
Maintaining a consistent air gap between the rotor and stator in electromechanical machines such as permanent magnet motors and generators is a critical aspect of efficient operation. On small diameter conventional motors and generators it is not difficult to design a machine structure that can maintain air gap clearance using conventional design methods. Maintaining a consistent air gap becomes more difficult for high torque, low speed machine designs, such as for the design of direct drive, gearless wind turbines, where the generator rotational speed is dictated by the wind turbine aerodynamic rotor. As one illustrative example, in a multi-MW class wind turbine the generator for a direct drive configuration may be required to produce its rated output power and torque at speeds in a general range of 14-16 rpm. A generator or motor in this general power and speed range must have a large air gap diameter, typically in the range of 3-5 meters. At these sizes under the experienced loads for such turbines, it becomes a design challenge to build a generator structure stiff enough to maintain the air gap integrity under all load conditions while maintaining the weight of the structural elements at a reasonable level.
Attempts have been made to add various bearing structures in order to address this problem. However, such proposed solutions generally involve relatively conventional bearing structures located at or close to the air gap to stabilize the air gap. But these conventional bearing-type solutions involve continuous load bearing structures with continuous contact that increase the weight and complexity of the design and add an additional maintenance item to the turbine design. As such, conventional solutions to this problem to date have been less than satisfactory.
For the purpose of illustrating the invention, the drawings show aspects of one or more embodiments of the invention. However, it should be understood that the present invention is not limited to the precise arrangements and instrumentalities shown in the drawings, wherein:
Embodiments of the present invention provide an apparatus for a rotating device with an air gap between rotating and stationary structures that needs to be maintained at all times, with no possible load case or scenario where the air gap entirely closes and impact or interference occurs between the rotating and stationary parts. In order to maintain a consistent air gap between the rotating and stationary components, exemplary embodiments of the present invention utilize bumper elements that are non-contact in normal operation and only pick up contact as sliding elements in the event of excessive generator structure deflection in cases of extreme loads or when problems in the main bearings cause a change in the air gap. Such bumper elements can be conveniently disposed to contact existing wear structures such as a rotor brake disc thus avoiding the need to provide additional, high strength or reinforced bearing surfaces.
Turning to the partial section views of
Stator 14 includes structural members such as spokes 24 that support the outer annular core support structure 26. Rotor brakes 28 are mounted on the stator structure to cooperate with rotor brake disc 20 for use as a rotor brake under necessary circumstances as are understood by persons skilled in the art. Also mounted on the stator structure are bumper elements 30 according to one exemplary embodiment of the present invention.
Bumper elements 30 are spaced from the rotor brake disc 20 by an amount calculated to control rotor deflection and thus air gap distance so as not to exceed predetermined amounts under extreme and eccentric loading conditions. Persons of ordinary skill in the art will be able to determine the appropriate spacing between bumper elements 30 and disc 20 for specific rotor and stator design parameters and operating conditions based on the teachings contained herein. Bumper elements 30 thus serve as secondary bearings that come into play only under extreme load and deflection cases during operation, thus acting as a safety system to back up the main bearing and structural arrangement in cases of high load and deflection at the air gap. By using such bumper elements with a slow speed motor or generator, the basic structural elements of the machine can be made lighter and more flexible while still maintaining a minimum air gap.
One exemplary embodiment of bumper elements 30 is illustrated in
In the exemplary embodiment described above, bumper elements 32 help maintain the air gap by providing a radially-oriented sliding bearing surface. In other embodiments it may be desirable to further provide an axially-oriented sliding bearing surface.
As will be appreciated by persons of ordinary skill in the art, the components of exemplary embodiments described herein may be fabricated by conventional means and from conventional materials. For example, parts can be machined fabrications or castings; could be manufactured by a variety of qualified vendors. Bearing material can be a variety of materials, and can be machined or extruded to shape. Embodiments of the present invention thus allow the use of a lighter stator structure while still safely maintaining the machine air gap under all operating conditions without requiring any special fabrication or construction needs.
In the exemplary embodiments described above, the bumper elements utilize the existing safety brake disc surface designed into the rotor structure, thus dual purposing this generator design feature. However, persons of ordinary skill in the art will appreciate that other annular machined rotor surfaces including specially provided surfaces may be used as an alternative to the brake disc. The present invention has also been illustrated above by reference to exemplary embodiments wherein the rotor is positioned inside of the stator. Persons of ordinary skill in the art will appreciate based on the teachings herein that embodiments of the present invention are also equally applicable to electromechanical machine configurations where the stator is positioned on the inside with stator poles facing out and surrounded by the rotor.
Exemplary embodiments have been disclosed above and illustrated in the accompanying drawings. It will be understood by those skilled in the art that various changes, omissions and additions may be made to that which is specifically disclosed herein without departing from the spirit and scope of the present invention.
Number | Name | Date | Kind |
---|---|---|---|
5021697 | Kralick | Jun 1991 | A |
6326710 | Guenther et al. | Dec 2001 | B1 |
7122923 | Lafontaine et al. | Oct 2006 | B2 |
7180204 | Grant et al. | Feb 2007 | B2 |
7528497 | Bertolotti | May 2009 | B2 |
7709971 | Sane et al. | May 2010 | B2 |
20060152014 | Grant et al. | Jul 2006 | A1 |
20070102934 | Pescarmona et al. | May 2007 | A1 |
20080012346 | Bertolotti | Jan 2008 | A1 |
20080050235 | Wobben | Feb 2008 | A1 |
20090045634 | Sane et al. | Feb 2009 | A1 |
20090174277 | Mueller et al. | Jul 2009 | A1 |
20090206684 | Jajtic et al. | Aug 2009 | A1 |
20100045047 | Stiesdal | Feb 2010 | A1 |
20100072835 | Klatt | Mar 2010 | A1 |
20110085752 | Tecza et al. | Apr 2011 | A1 |
Number | Date | Country |
---|---|---|
1657437 | May 2006 | EP |
1783363 | May 2007 | EP |
2143944 | Jan 2010 | EP |
2157314 | Feb 2010 | EP |
2333933 | Jun 2011 | EP |
2333934 | Jun 2011 | EP |
0106623 | Jan 2001 | WO |
2005019642 | Mar 2005 | WO |
2007008884 | Jan 2007 | WO |
2007104976 | Sep 2007 | WO |
2007113498 | Oct 2007 | WO |
2008076147 | Jun 2008 | WO |
2008120257 | Oct 2008 | WO |
2009105011 | Aug 2009 | WO |
2009122428 | Oct 2009 | WO |
2009156712 | Dec 2009 | WO |
2010003868 | Jan 2010 | WO |
2010081568 | Jul 2010 | WO |
Number | Date | Country | |
---|---|---|---|
61422486 | Dec 2010 | US |