TREA

Wind power generator equipped with a cooling system

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Information

  • Patent Grant
  • 10505419
  • Patent Number
    10,505,419
  • Date Filed
    Tuesday, April 5, 2016
    8 years ago
  • Date Issued
    Tuesday, December 10, 2019
    4 years ago
Information
Abstract
A wind power generator has a nacelle; a hub rotatable about an axis of rotation with respect to the nacelle; at least two blades fitted to the hub; an electric machine which is fitted to the nacelle, is bounded by an inner surface extending about the axis of rotation, and has a rotor and a stator; and a cooling system for airflow cooling the electric machine, and which has a deflector body for defining a gap between the deflector body and the electric machine and guiding the airflow into the gap.
Description
BACKGROUND

Known airflow cooling systems are not particularly efficient, especially in the case of generators equipped with a cylindrical electric machine.


SUMMARY

The present invention relates to a wind power generator equipped with a cooling system.


More specifically, the present invention relates to a wind power generator comprising a nacelle; a hub rotatable about an axis of rotation with respect to the nacelle; at least two blades fitted to the hub; an electric machine which is fitted to the nacelle, is bounded by an inner surface extending about the axis of rotation, and has a rotor and a stator; and a cooling system for airflow cooling the electric machine.


It is an object of the present invention to provide a wind power generator equipped with a highly efficient cooling system.


A further object of the present invention is to provide a wind power generator equipped with a straightforward, low-cost cooling system.


According to one embodiment of the present invention, there is provided a wind power generator equipped with a cooling system, the wind power generator comprising a nacelle; a hub rotatable about an axis of rotation with respect to the nacelle; at least two blades fitted to the hub; an electric machine which is fitted to the nacelle, is bounded by an inner surface extending about the axis of rotation, and has a rotor and a stator; and a cooling system for airflow cooling the electric machine, and which comprises a deflector body for defining a gap between the deflector body and the electric machine and guiding the airflow into the gap.


According to the present invention, the efficiency of the cooling system is improved by the entire airflow being forced into the gap, which runs close to the electric machine and improves thermal exchange by preventing part of the airflow from flowing too far away from the hottest parts of the electric machine.


Additional features and advantages are described in, and will be apparent from, the following Detailed Description and the figures.





BRIEF DESCRIPTION OF THE DRAWINGS

A non-limiting embodiment of the present invention will be described by way of example with reference to the accompanying drawings, in which:



FIG. 1 shows a partly sectioned side view, with parts removed for clarity, of a wind power generator in accordance with the present invention;



FIG. 2 shows a larger-scale lateral section of a detail of the FIG. 1 wind power generator;



FIG. 3 shows a larger-scale view in perspective, with parts removed for clarity, of a detail of the FIG. 1 wind power generator;



FIG. 4 shows a larger-scale lateral section of a detail of the FIG. 1 wind power generator.





DETAILED DESCRIPTION

Number 1 in FIG. 1 indicates as a whole a wind power generator, which comprises a pylon 2 extending along a vertical axis A1; a nacelle 3 fitted to the top end of pylon 2 and rotatable with respect to pylon 2 about axis A1; a hub 4 mounted to rotate with respect to nacelle 3 about an axis of rotation A2 crosswise to axis A1; and three blades 5, only two of which are shown by dash lines in FIG. 1.


Pylon 2 is substantially defined by a hollow cylinder housing stairs (not shown in the drawings) and/or lifts (not shown in the drawings).


Pylon 2 is normally secured to the ground by a foundation (not shown in the drawings). Alternatively, in off-shore systems, pylon 2 is secured to a floating platform (not shown in the drawings).


Nacelle 3 comprises a hollow body fitted to the top end of pylon 2 to rotate about axis A1, and supports an electric machine 6 having a rotor 8 and a stator 9, and bounded by an inner surface 7 extending about axis of rotation A2. In other words, electric machine 6 is a hollow cylindrical generator.


Likewise, hub 4 comprises a hollow body integral with rotor 8.


Wind power generator 1 comprises a cooling system 10 supported partly by hub 4 and partly by nacelle 3, and which serves to airflow cool electric machine 6, and in particular to conduct an airflow, predominantly in a direction D1 parallel to axis of rotation A2, from an inlet 11 in hub 4 to an outlet 12 in nacelle 3.


In the example shown in the drawings, stator 9 extends about rotor 8, and rotor 8 is integral with hub 4 and extends inside stator 9. The inner surface 7 of electric machine 6 is therefore the inner surface of rotor 8.


Stator 9 is fixed or connected directly to nacelle 3 along an inner cylindrical surface of nacelle 3. Hub 4 and rotor 8 are connected to each other and supported by a bearing 13 in turn supported by nacelle 3.


In a variation not shown in the drawings, the rotor extends about the stator, the stator is located inside the rotor, and the inner surface of the electric machine is defined by the stator.


Cooling system 10 comprises, in succession from inlet 11 to outlet 12, an air intake filtration device 14; a ventilation unit 15; and a deflector body 16.


With reference to FIG. 4, filtration device 14 is fitted to hub 4, is located at inlet 11, and comprises a convex panel 17 located in front of inlet 11 and having an outward-facing convex face 18 and an oppositely-convex annular edge 19; an annular panel 20 having a concave face 21 extending about edge 19 and facing convex panel 17; and an annular panel 22 extending inside convex panel 17 and comprising a convex face 23 facing convex panel 17, and a concave face 24 facing hub 4.


Panel 17 is fitted to hub 4 by spacer arms 25, whereas panels 20 and 22 are fixed or connected directly to hub 4 about inlet 11. Panels 17, 20 and 22 are guide panels for guiding the air intake into hub 4, and are designed and positioned with respect to one another to define a labyrinth air intake path. Filtration device 14 thus prevents, or at least reduces, entry of water, snow or impurities into hub 4 and nacelle 3.


With reference to FIG. 1, ventilation unit 15 is housed inside hub 4, and comprises a powered fan 26; a guide 27 parallel to axis of rotation A2; and a slide 28 that runs along guide 27 in direction D1, and supports fan 26.


Guide 27 comprises two rails 29 located about axis of rotation A2 and extending in direction D1. Fan 26 serves to increase airflow speed in direction D1 into nacelle 3.


Deflector body 16 serves to form a gap 30 between deflector body 16 itself and electric machine 6, and to guide the airflow into gap 30.


As shown more clearly in FIG. 2, deflector body 16 is fixed or connected to electric machine 6, in particular to rotor 8, by means of brackets 31.


In the example shown in the drawings, and particularly in FIG. 1, rotor 8 comprises a sleeve 32 supported by bearing 13 and integral with hub 4; a cylindrical structure 33 integral with sleeve 32; and permanent magnets 34 fixed along the outer surface of cylindrical structure 33. Cylindrical structure 33 defines inner surface 7, which is a cylindrical surface.


Cooling system 10 also comprises fins 35 parallel to direction D1 and fixed or connected to inner surface 7 of cylindrical structure 33.


Stator 9 comprises a stator pack 36 fixed or connected to the surface of nacelle 3; and stator windings (not shown in the drawings).


With reference to FIG. 2, deflector body 16 is substantially axially symmetrical about axis of rotation A2, is fixed or connected to sleeve 32 by brackets 31, and comprises a substantially conical central portion 37 for guiding the airflow to inner surface 7 and defined by a central panel 38 and by a number of panels 39 extending about central panel 38; and a cylindrical portion 40 facing and parallel to inner surface 7, and which serves to define gap 30 and comprises a number of panels 41. Panels 38, 39 and 41 are connected removably to one another.


With reference to FIG. 3, fins 35 extend from inner surface 7 of rotor 8 towards axis of rotation A2, and are divided into groups 42 and 43, each of which, in addition to a given number of fins 35, comprises a perforated cylindrical sector 44 fixed by screws to cylindrical structure 33. As shown in FIG. 3, fins 35 and respective cylindrical sector 44 are preferably formed in one piece.


With reference to FIG. 2, panel 38 is fixed or connected to panels 39 by means of thumbscrews 45, and comprises grips 46 by which to remove panel 38 easily to allow access by maintenance personnel inside hub 4.


With reference to FIG. 1, fan 26 is movable along axis of rotation A2 to allow passage by maintenance personnel and also to set the fan to the best operating position.


Cooling system 10 also extends partly outside nacelle 3, and comprises fins 47 parallel to axis of rotation A2 and fixed or connected to the outer surface of nacelle 3, at stator 9, to assist cooling stator 9.


In actual use, nacelle 3 is oriented about axis A1 so that axis of rotation A2 is positioned in the wind direction, with blades 5 into the wind, and the airflow therefore flows naturally along the labyrinth path into inlet 11, through hub 4 and nacelle 3, and out through outlet 12. At the same time, part of the air flows over the outer surface of nacelle 3 and onto fins 47, which increase the air-stator 9 heat exchange surface.


Airflow inside hub 4 and nacelle 3 is also assisted by fan 26, which serves to overcome any load losses in the airflow, and increases airflow speed inside hub 4 and nacelle 3.


The airflow is diverted by deflector body 16, and assumes first a predominantly radial and then a purely axial speed component, both with reference to axis of rotation A2. That is, portion 37 serves to guide the airflow to inner surface 7 of electric machine 6, and portion 40 of deflector body 16 to guide and keep the airflow close to inner surface 7 of electric machine 6 and fins 35, so the entire airflow inside nacelle 3 contacts the hottest parts of electric machine 6.


It should be understood that various changes and modifications to the presently preferred embodiments described herein will be apparent to those skilled in the art. Such changes and modifications can be made without departing from the spirit and scope of the present subject matter and without diminishing its intended advantages. It is therefore intended that such changes and modifications be covered by the appended claims.

Claims
  • 1. A hollow rotary electric machine cooling system comprising: a deflector wall including a tubular portion, wherein: (i) the deflector wall is housed in a hollow rotary electrical machine defining a human passageway to a hub of a wind power generator and including: (a) a stator,(b) a shaftless hollow rotor which is distinct from the tubular portion of the deflector wall, and(c) an inner tubular surface which extends about an axis of rotation,(ii) the deflector wall is removeably connected to the shaftless hollow rotor of the hollow rotary electric machine, and(iii) a cooling airflow guide gap is defined between the deflector wall and the inner tubular surface of the hollow rotary electric machine, said defined cooling airflow guide gap extending between the shaftless hollow rotor and the deflector wall.
  • 2. The hollow rotary electric machine cooling system of claim 1, wherein the deflector wall includes a portion configured to direct a cooling airflow to: (i) the inner tubular surface of the hollow rotary electric machine, and(ii) the tubular portion of the deflector wall.
  • 3. The hollow rotary electric machine of claim 1, wherein the deflector wall includes a plurality of panels assembled adjacent to one another, at least one of said panels being configured to be removed.
  • 4. The hollow rotary electric machine cooling system of claim 1, wherein the inner tubular surface of the hollow rotary electric machine is an inner tubular surface of the shaftless hollow rotor.
  • 5. A hollow rotary electric machine comprising: a stator;a shaftless hollow rotor housed within the stator and having an inner tubular surface which defines a human passageway to a hub of a wind power generator; anda deflector wall at least partly housed in the shaftless hollow rotor, said deflector wall including a tubular portion, wherein a cooling airflow guide gap is defined between the deflector wall and the inner tubular surface of the shaftless hollow rotor, the deflector wall is removeably connected to the shaftless hollow rotor, and the shaftless hollow rotor is distinct from the tubular portion of the deflector wall.
  • 6. The hollow rotary electric machine of claim 5, wherein the deflector wall includes a portion configured to guide an airflow to: (i) the inner tubular surface of the shaftless hollow rotor and (ii) the tubular portion of the deflector wall.
  • 7. The hollow rotary electric machine of claim 5, wherein the deflector wall includes a plurality of panels assembled adjacent to one another, at least one of said panels being configured to be removed.
  • 8. A hollow rotary electric machine cooling system comprising: a deflector wall including a tubular portion, wherein: (i) at least part of the deflector wall is removeably housed in a hollow rotary electrical machine defining a human passageway to a hub of a wind power generator and including: (a) a stator,(b) a shaftless hollow rotor which is distinct from the tubular portion of the deflector wall, and(c) an inner tubular surface which extends about an axis of rotation, and(ii) a cooling airflow guide gap is defined between the deflector wall and the inner tubular surface of the hollow rotary electric machine; anda plurality of cooling fins connected to the hollow rotary electric machine along the inner tubular surface.
  • 9. The hollow rotary electric machine cooling system of claim 8, wherein the deflector wall includes a portion configured to direct a cooling airflow to: (i) the inner tubular surface of the hollow rotary electric machine, and(ii) the tubular portion of the deflector wall.
  • 10. The hollow rotary electric machine of claim 8, wherein the deflector wall includes a plurality of panels assembled adjacent to one another, at least one of said panels being configured to be removed.
  • 11. The hollow rotary electric machine cooling system of claim 8, wherein the inner tubular surface of the hollow rotary electric machine is an inner tubular surface of the shaftless hollow rotor.
  • 12. A hollow rotary electric machine comprising: a stator;a shaftless hollow rotor housed within the stator and having an inner tubular surface defining a human passageway to a hub of a wind power generator;a deflector wall at least partly removeably housed in the shaftless hollow rotor, said deflector wall including a tubular portion, wherein a cooling airflow guide gap is defined between the deflector wall and the inner tubular surface of the shaftless hollow rotor and the shaftless hollow rotor is distinct from the tubular portion of the deflector wall; anda plurality of cooling fins connected to the inner tubular surface of the shaftless hollow rotor.
  • 13. The hollow rotary electric machine of claim 12, wherein the deflector wall includes a portion configured to guide an airflow to: (i) the inner tubular surface of the shaftless hollow rotor, and(ii) the tubular portion of the deflector wall.
  • 14. The hollow rotary electric machine of claim 12, wherein the deflector wall includes a plurality of panels assembled adjacent to one another, at least one of said panels being configured to be removed.
Priority Claims (1)
Number Date Country Kind
MI2008A1122 Jun 2008 IT national
PRIORITY CLAIM

This application is a continuation of, claims the benefit of and priority to U.S. patent application Ser. No. 13/943,435, filed on Jul. 16, 2013, which is a continuation of, claims the benefit of and priority to U.S. patent application Ser. No. 12/485,645, filed on Jun. 16, 2009, now U.S. Pat. No. 8,492,919, which claims the benefit of and priority to Italian Patent Application No. MI2008A 001122, filed on Jun. 19, 2008, the entire contents of which are each incorporated by reference herein.

US Referenced Citations (288)
Number Name Date Kind
765078 Jigouzo Jul 1904 A
1362753 Sperry Dec 1920 A
1894357 Manikowske et al. Jan 1933 A
1948854 Heath Feb 1934 A
1979813 Reis Nov 1934 A
2006172 Klappauf Jun 1935 A
2040218 Soderberg May 1936 A
2177801 Erren Oct 1939 A
2469734 Ledwith May 1949 A
2496897 Strickland Feb 1950 A
2655611 Sherman Oct 1953 A
2739253 Plumb Mar 1956 A
2806160 Brainard Sep 1957 A
2842214 Prewitt Jul 1958 A
2903610 Bessiere Sep 1959 A
3004782 Meermans Oct 1961 A
3072813 Reijnst et al. Jan 1963 A
3083311 Krasnow Mar 1963 A
3131942 Ertaud May 1964 A
3168686 King et al. Feb 1965 A
3221195 Hoffmann Nov 1965 A
3250926 O'Reilly May 1966 A
3363910 Toronchuk Jan 1968 A
3364523 Schippers Jan 1968 A
3392910 Tanzberger Jul 1968 A
3468548 Webb Sep 1969 A
3643119 Lukens Feb 1972 A
3700247 Butler et al. Oct 1972 A
3724861 Lesiecki Apr 1973 A
3735174 Bosch May 1973 A
3746349 Smale et al. Jul 1973 A
3748089 Boyer et al. Jul 1973 A
3749953 Baumann Jul 1973 A
3751699 Gleichman Aug 1973 A
3789252 Abegg Jan 1974 A
3841643 McLean Oct 1974 A
3860843 Kawasaki et al. Jan 1975 A
3942026 Carter Mar 1976 A
3963247 Nommensen Jun 1976 A
3968969 Mayer et al. Jul 1976 A
4022479 Orlowski May 1977 A
4061926 Peed Dec 1977 A
4087698 Myers May 1978 A
4273343 Visser Jun 1981 A
4289970 Deibert Sep 1981 A
4291235 Bergey, Jr. et al. Sep 1981 A
4292532 Leroux Sep 1981 A
4336649 Glaser Jun 1982 A
4339874 Mc'Carty et al. Jul 1982 A
4350897 Benoit Sep 1982 A
4354126 Yates Oct 1982 A
4368895 Okamoto et al. Jan 1983 A
4398773 Boden et al. Aug 1983 A
4452046 Valentin Jun 1984 A
4482831 Notaras et al. Nov 1984 A
4490093 Chertok et al. Dec 1984 A
4517483 Hucker et al. May 1985 A
4517484 Dacier May 1985 A
4521026 Eide Jun 1985 A
4585950 Lund Apr 1986 A
4613779 Meyer Sep 1986 A
4638200 Le Corre et al. Jan 1987 A
4648801 Wilson Mar 1987 A
4694654 Kawamura Sep 1987 A
4700096 Epars Oct 1987 A
4714852 Kawada et al. Dec 1987 A
4720640 Anderson et al. Jan 1988 A
4722661 Mizuno Feb 1988 A
4724348 Stokes Feb 1988 A
4740711 Sato Apr 1988 A
4761590 Kaszman Aug 1988 A
4792712 Stokes Dec 1988 A
4801244 Stahl Jan 1989 A
4866321 Blanchard et al. Sep 1989 A
4900965 Fisher Feb 1990 A
4906060 Claude Mar 1990 A
4973868 Wust Nov 1990 A
4976587 Johnston et al. Dec 1990 A
5004944 Fisher Apr 1991 A
5063318 Anderson Nov 1991 A
5090711 Becker Feb 1992 A
5091668 Cuenot et al. Feb 1992 A
5177388 Hotta et al. Jan 1993 A
5191255 Kloosterhouse et al. Mar 1993 A
5275139 Rosenquist Jan 1994 A
5280209 Leupold et al. Jan 1994 A
5281094 McCarty et al. Jan 1994 A
5298827 Sugiyama Mar 1994 A
5302876 Iwamatsu et al. Apr 1994 A
5311092 Fisher May 1994 A
5315159 Gribnau May 1994 A
5410997 Rosenquist May 1995 A
5419683 Peace May 1995 A
5456579 Olson Oct 1995 A
5483116 Kusase et al. Jan 1996 A
5506453 McCombs Apr 1996 A
5579800 Walker Dec 1996 A
5609184 Apel et al. Mar 1997 A
5663600 Baek et al. Sep 1997 A
5670838 Everton Sep 1997 A
5696419 Rakestraw et al. Dec 1997 A
5704567 Maglieri Jan 1998 A
5746576 Bayly May 1998 A
5777952 Nishimura et al. Jul 1998 A
5783894 Wither Jul 1998 A
5793144 Kusase et al. Aug 1998 A
5798632 Muljadi Aug 1998 A
5801470 Johnson et al. Sep 1998 A
5811908 Iwata et al. Sep 1998 A
5814914 Caamaño Sep 1998 A
5844341 Spooner et al. Dec 1998 A
5857762 Schwaller Jan 1999 A
5886441 Uchida et al. Mar 1999 A
5889346 Uchida et al. Mar 1999 A
5894183 Borchert Apr 1999 A
5925964 Kusase et al. Jul 1999 A
5952755 Lubas Sep 1999 A
5961124 Muller Oct 1999 A
5973435 Irie et al. Oct 1999 A
5986374 Kawakami Nov 1999 A
5986378 Caamaño Nov 1999 A
6013968 Lechner et al. Jan 2000 A
6037692 Miekka et al. Mar 2000 A
6064123 Gislason May 2000 A
6089536 Watanabe et al. Jul 2000 A
6093984 Shiga et al. Jul 2000 A
6127739 Appa Oct 2000 A
6172429 Russell Jan 2001 B1
6177746 Tupper et al. Jan 2001 B1
6193211 Watanabe et al. Feb 2001 B1
6194799 Miekka et al. Feb 2001 B1
6215199 Lysenko et al. Apr 2001 B1
6215212 Grennan Apr 2001 B1
6232673 Schoo et al. May 2001 B1
6246126 Van Der Veken et al. Jun 2001 B1
6278197 Appa Aug 2001 B1
6285090 Brutsaert et al. Sep 2001 B1
6326711 Yamaguchi et al. Dec 2001 B1
6365994 Watanabe et al. Apr 2002 B1
6373160 Schrödl Apr 2002 B1
6376956 Hosoya Apr 2002 B1
6378839 Watanabe et al. Apr 2002 B2
6384504 Elrhart et al. May 2002 B1
6417578 Chapman et al. Jul 2002 B1
6428011 Oskouei Aug 2002 B1
6452287 Looker Sep 2002 B1
6452301 Van Dine et al. Sep 2002 B1
6455976 Nakano Sep 2002 B1
6472784 Miekka et al. Oct 2002 B2
6474653 Hintenlang et al. Nov 2002 B1
6476513 Gueorguiev Nov 2002 B1
6492743 Appa Dec 2002 B1
6492754 Weiglhofer et al. Dec 2002 B1
6504260 Debleser Jan 2003 B1
6515390 Lopatinsky et al. Feb 2003 B1
6548932 Weiglhofer et al. Apr 2003 B1
6590312 Seguchi et al. Jul 2003 B1
6603232 Van Dine et al. Aug 2003 B2
6617747 Petersen Sep 2003 B1
6629358 Setiabudi et al. Oct 2003 B2
6664692 Kristoffersen Dec 2003 B1
6683397 Gauthier et al. Jan 2004 B2
6700260 Hsu et al. Mar 2004 B2
6700288 Smith Mar 2004 B2
6707224 Petersen Mar 2004 B1
6720688 Schiller Apr 2004 B1
6727624 Morita et al. Apr 2004 B2
6746217 Kim et al. Jun 2004 B2
6759758 Martinez Jul 2004 B2
6762525 Maslov et al. Jul 2004 B1
6781276 Stiesdal et al. Aug 2004 B1
6784564 Wobben Aug 2004 B1
6794781 Razzell et al. Sep 2004 B2
6828710 Gabrys Dec 2004 B1
6856042 Kubota Feb 2005 B1
6879075 Calfo et al. Apr 2005 B2
6888262 Blakemore May 2005 B2
6891299 Coupart et al. May 2005 B2
6903466 Mercier et al. Jun 2005 B1
6903475 Ortt et al. Jun 2005 B2
6906444 Hattori et al. Jun 2005 B2
6911741 Petteersen et al. Jun 2005 B2
6921243 Canini et al. Jul 2005 B2
6931834 Jones Aug 2005 B2
6933645 Watson Aug 2005 B1
6933646 Kinoshita Aug 2005 B2
6942454 Ohlmann Sep 2005 B2
6945747 Miller Sep 2005 B1
6949860 Hama et al. Sep 2005 B2
6951443 Blakemore Oct 2005 B1
6972498 Jamieson et al. Dec 2005 B2
6983529 Ortt et al. Jan 2006 B2
6984908 Rinholm et al. Jan 2006 B2
6987342 Hans Jan 2006 B2
6998729 Wobben Feb 2006 B1
7004724 Pierce et al. Feb 2006 B2
7008172 Selsam Mar 2006 B2
7008348 LaBath Mar 2006 B2
7016006 Song Mar 2006 B2
7021905 Torrey et al. Apr 2006 B2
7028386 Kato et al. Apr 2006 B2
7038343 Agnes et al. May 2006 B2
7042109 Gabrys May 2006 B2
7075192 Bywaters et al. Jul 2006 B2
7081696 Ritchey Jul 2006 B2
7088024 Agnes et al. Aug 2006 B2
7091642 Agnes et al. Aug 2006 B2
7095128 Canini et al. Aug 2006 B2
7098552 McCoin Aug 2006 B2
7109600 Bywaters et al. Sep 2006 B1
7116006 McCoin Oct 2006 B2
7119469 Ortt et al. Oct 2006 B2
7154191 Jansen et al. Dec 2006 B2
7161260 Krügen-Gotzmann et al. Jan 2007 B2
7166942 Yokota Jan 2007 B2
7168248 Sakamoto et al. Jan 2007 B2
7179056 Sieffriedsen Feb 2007 B2
7180204 Grant et al. Feb 2007 B2
7183665 Bywaters et al. Feb 2007 B2
7196446 Hans Mar 2007 B2
7259472 Miyake et al. Aug 2007 B2
7281501 Leufen et al. Oct 2007 B2
7285890 Jones et al. Oct 2007 B2
7323792 Sohn Jan 2008 B2
7358637 Tapper Apr 2008 B2
7377163 Miyagawa May 2008 B2
7392988 Moldt et al. Jul 2008 B2
7427814 Bagepalli et al. Sep 2008 B2
7431567 Bevington et al. Oct 2008 B1
7458261 Miyagawa Dec 2008 B2
7482720 Gordon et al. Jan 2009 B2
7548008 Jansen et al. Jun 2009 B2
7687932 Casazza et al. Mar 2010 B2
8053918 Wobben Nov 2011 B2
9312741 Pabst Apr 2016 B2
20010035651 Umemoto et al. Nov 2001 A1
20020047418 Seguchi et al. Apr 2002 A1
20020047425 Coupart et al. Apr 2002 A1
20020056822 Watanabe et al. May 2002 A1
20020063485 Lee et al. May 2002 A1
20020089251 Tajima et al. Jul 2002 A1
20020148453 Watanabe et al. Oct 2002 A1
20030011266 Morita et al. Jan 2003 A1
20030102677 Becker et al. Jun 2003 A1
20030137149 Northrup et al. Jul 2003 A1
20030230899 Martinez Dec 2003 A1
20040086373 Page, Jr. May 2004 A1
20040094965 Kirkegaard et al. May 2004 A1
20040119292 Datta et al. Jun 2004 A1
20040150283 Calfo et al. Aug 2004 A1
20040151575 Pierce et al. Aug 2004 A1
20040151577 Pierce et al. Aug 2004 A1
20040179934 Wobben Sep 2004 A1
20040189136 Kolomeitsev et al. Sep 2004 A1
20050002783 Hiel et al. Jan 2005 A1
20050082839 McCoin Apr 2005 A1
20050230979 Bywaters et al. Oct 2005 A1
20050280264 Nagy Dec 2005 A1
20060000269 LeMieux et al. Jan 2006 A1
20060001269 Jansen et al. Jan 2006 A1
20060006658 McCoin Jan 2006 A1
20060012182 McCoin Jan 2006 A1
20060028025 Kikuchi et al. Feb 2006 A1
20060066110 Jansen et al. Mar 2006 A1
20060071575 Jansen et al. Apr 2006 A1
20060091735 Song et al. May 2006 A1
20060125243 Miller Jun 2006 A1
20060131985 Qu et al. Jun 2006 A1
20060152012 Wiegel et al. Jul 2006 A1
20060152015 Bywaters et al. Jul 2006 A1
20060152016 Bywaters et al. Jul 2006 A1
20070012026 Dev Jan 2007 A1
20070024132 Salamah et al. Feb 2007 A1
20070187954 Struve et al. Aug 2007 A1
20070187956 Wobben Aug 2007 A1
20070222226 Casazza et al. Sep 2007 A1
20070222227 Casazza et al. Sep 2007 A1
20080061559 Hirshberg Mar 2008 A1
20080107526 Wobben May 2008 A1
20080118342 Seidel et al. May 2008 A1
20080290664 Kruger Nov 2008 A1
20080303281 Krueger Dec 2008 A1
20080315594 Casazza et al. Dec 2008 A1
20090302702 Pabst et al. Dec 2009 A1
20100019502 Pabst et al. Jan 2010 A1
20100026010 Pabst Feb 2010 A1
20100117362 Vihriala et al. May 2010 A1
20100123318 Casazza et al. May 2010 A1
Foreign Referenced Citations (1)
Number Date Country
19636591 Mar 1998 DE
Non-Patent Literature Citations (1)
Entry
India Office Action for Application No. 1455/MUM/2009 dated Oct. 6, 2017.
Related Publications (1)
Number Date Country
20160218575 A1 Jul 2016 US
Continuations (2)
Number Date Country
Parent 13943435 Jul 2013 US
Child 15091354 US
Parent 12485645 Jun 2009 US
Child 13943435 US