CN108711966B - Rotor assembly of generator and generator - Google Patents
Rotor assembly of generator and generator Download PDFInfo
- Publication number
- CN108711966B CN108711966B CN201810668935.5A CN201810668935A CN108711966B CN 108711966 B CN108711966 B CN 108711966B CN 201810668935 A CN201810668935 A CN 201810668935A CN 108711966 B CN108711966 B CN 108711966B
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- baffle
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- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02K—DYNAMO-ELECTRIC MACHINES
- H02K1/00—Details of the magnetic circuit
- H02K1/06—Details of the magnetic circuit characterised by the shape, form or construction
- H02K1/22—Rotating parts of the magnetic circuit
-
- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02K—DYNAMO-ELECTRIC MACHINES
- H02K2213/00—Specific aspects, not otherwise provided for and not covered by codes H02K2201/00 - H02K2211/00
- H02K2213/12—Machines characterised by the modularity of some components
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- Engineering & Computer Science (AREA)
- Power Engineering (AREA)
- Permanent Field Magnets Of Synchronous Machinery (AREA)
- Iron Core Of Rotating Electric Machines (AREA)
Abstract
The embodiment of the application provides a rotor assembly of a generator and the generator, wherein the rotor assembly of the generator comprises more than two rotor sections, and any two rotor sections are connected in a sealing mode. The rotor assembly of the generator provided by the embodiment of the application successfully solves the technical problems of overlarge size and inconvenience in transportation of the permanent magnet direct-driven wind driven generator by adopting a simple and practical modular structure design.
Description
Technical Field
The application relates to the technical field of generators, in particular to a rotor assembly of a generator and the generator.
Background
With the increasing technical level in the field of wind power, the current wind driven generator is continuously developed towards high power, the physical size of the permanent magnet direct-drive wind driven generator is gradually increased, and road transportation becomes very difficult when the diameter of the permanent magnet direct-drive wind driven generator exceeds a certain limit value. Therefore, how to realize the use stage of the wind driven generator after assembly can not only ensure the high-power output capability of the wind driven generator, but also consider the feasibility and convenience of the wind driven generator in transportation before assembly, and is one of the technical problems to be solved urgently in the industry at present.
Disclosure of Invention
The application provides a rotor subassembly and generator of generator for solve the technical problem of aerogenerator portability transportation.
The technical scheme of the application is as follows:
According to a first aspect of embodiments, there is provided a rotor assembly of an electrical generator, comprising: more than two rotor sections; any two rotor sections are connected in a sealing way.
Optionally, the rotor section includes at least one rotor support section and a plurality of rotor cover sections corresponding to the number of rotor support sections, and any rotor support section is detachably connected to the corresponding rotor cover section.
optionally, the rotor support section comprises: the stiffness adjusting device is connected with the rotor housing section.
Optionally, the rotor casing section comprises an arcuate wall plate, and a baffle plate;
The baffle extends along the upper edge and/or the lower edge of the arc-shaped wall plate in the radial direction; the arc-shaped wall plate is fixedly connected with the baffle plate.
the rigidity adjusting device comprises a first bearing part and/or a second bearing part;
the first force bearing part is arranged on the outer surface of the arc-shaped wall plate;
The second force bearing part is arranged on the outer surface of the baffle plate and extends to the outer surface of the arc-shaped wall plate through the connecting position of the arc-shaped wall plate and the baffle plate and bending.
Optionally, one end of the second force bearing part extends from the edge of the baffle plate close to the rotating shaft; and the second bearing part is fixedly connected with the baffle and/or the baffle.
Optionally, a flange is fixedly connected to the inner side of the baffle, the flange is connected with the rotating shaft, and the flange is in contact with the second force bearing part.
Optionally, the rotor support sections further comprise a flange part, and two adjacent rotor support sections are fixedly connected through the flange part; and a sealing groove is arranged on the flange component, and a sealing component is arranged in the sealing groove.
optionally, the flange part extends along the rotor support section and/or the rotor end cover section and projects radially outwards.
Optionally, the rotor support section further comprises a magnetic yoke, the magnetic yoke is arranged on the inner wall of the rotor support section, and the magnetic pole is installed at the magnetic yoke of the rotor support section; the flange part is provided with a mounting plane for fixing the magnetic pole.
Optionally, the flange parts are respectively provided with a positioning part.
According to a second aspect of embodiments, there is provided an electrical generator comprising a rotor assembly of any of the above-described electrical generators.
The technical scheme provided by the embodiment of the application has the following beneficial effects:
The embodiment of the application provides a rotor assembly of a generator, which comprises more than two rotor sections, wherein any two rotor sections are in sealing connection. The embodiment of the application takes the outer rotor component of the permanent magnet direct-drive wind driven generator as an example, and by adopting a simple and practical modular structure design, the technical problems of overlarge size and inconvenience in transportation before the permanent magnet direct-drive wind driven generator is assembled are successfully solved, and meanwhile, the high-power output capacity after the permanent magnet direct-drive wind driven generator is transported to a destination and assembled and integrated is guaranteed.
Embodiments of the present application provide a generator that includes a rotor assembly of the generator that is made up of a plurality of smaller sized rotor segments. The rotor of the generator is divided into a plurality of sections and respectively transported, so that the high-power output capacity of the wind driven generator is guaranteed, the feasibility of the wind driven generator in transportation is realized, the road transportation requirement of the current high-power generator is met, and the application area of the large-diameter permanent magnet direct-driven wind driven generator is enlarged.
Drawings
In order to more clearly illustrate the technical solutions in the embodiments of the present application, the drawings used in the description of the embodiments of the present application will be briefly described below. The outer rotor of this application embodiment is the example, through introducing the structure of the outer rotor subassembly of generator, explains and utilizes the technical scheme of modularization design mode, with the inner rotor of generator or outer rotor split into a plurality of parts to reach the transportation of being convenient for, improve the good technological effect of generating efficiency.
Fig. 1 is a schematic structural diagram of an outer rotor assembly of a generator according to an embodiment of the present disclosure;
FIG. 2 is a schematic structural diagram of a rotor support section of an outer rotor assembly constituting a generator according to an embodiment of the present disclosure;
FIG. 3 is an enlarged schematic view of the circled labeled area in FIG. 2;
FIG. 4 is a schematic structural view of a rotor end cover section;
FIG. 5 is an enlarged schematic view of the circled labeled area in FIG. 4;
FIG. 6 is another schematic view of a rotor spider section.
description of reference numerals:
10-an outer rotor assembly of a generator, 100-a rotor section, 110-a rotor spider section, 111-a first connecting flange, 112-a second connecting flange, 113-a first seal groove, 114-a flange, 115-an annular rib, 116-an L-shaped rib, 117-a first dowel hole, 118-a mounting plane, 119-a stiffening ring section,
120-a rotor end cover section, 121-a third connecting flange, 122-a fourth connecting flange, 123-a second seal groove, 124-a second dowel hole;
130-magnetic pole; 131-ring baffle, 150-baffle, 190-welding position;
20-axis.
Detailed Description
in order to solve the technical problems of overlarge size and inconvenience in transportation of the permanent magnet direct-drive wind driven generator, the inventor of the application considers that a modular structure design mode is adopted, and the permanent magnet direct-drive wind driven generator is split into a plurality of parts to be transported respectively.
The inventor of the application finds that the permanent magnet direct-drive type wind driven generator generally has two structural forms of an outer rotor and an inner rotor, the rotor of the outer rotor permanent magnet direct-drive type wind driven generator is positioned on the outer side of a stator, the diameter of an air gap of a generator is fixed, the outer diameter of the rotor of the outer rotor permanent magnet direct-drive type wind driven generator is larger than that of the rotor of the inner rotor permanent magnet direct-drive type wind driven generator, and therefore the requirement that the size of the outer rotor generator is reduced by means of. Obviously, the modularized rotor structure suitable for the inner rotor permanent magnet direct-drive type wind driven generator and the outer rotor permanent magnet direct-drive type wind driven generator is provided, the outer rotor of the generator can be conveniently split into a plurality of parts and can be transported respectively, and the modularized rotor structure is very necessary.
According to a first aspect of embodiments, there is provided a rotor assembly of an electrical generator, comprising: more than two rotor sections; any two rotor sections are connected in a sealing way. The rotor section comprises at least one rotor support section and a plurality of rotor end cover sections matched with the number of the rotor support sections, and any rotor support section is detachably connected with the corresponding rotor end cover section.
Embodiments of the present application will now be described in detail, with reference to a generator rotor assembly comprising two rotor sections, examples of which are illustrated in the accompanying drawings, wherein like or similar reference numerals refer to the same or similar elements or elements having the same or similar function throughout. The embodiments described below with reference to the drawings are exemplary only for the purpose of explaining the present application and are not to be construed as limiting the present invention.
As used herein, the singular forms "a", "an", "the" and "the" are intended to include the plural forms as well, unless the context clearly indicates otherwise. It will be further understood that the terms "comprises" and/or "comprising," when used in this specification, specify the presence of stated features, integers, steps, operations, elements, and/or components, but do not preclude the presence or addition of one or more other features, integers, steps, operations, elements, components, and/or groups thereof. As used herein, the term "and/or" includes all or any element and all combinations of one or more of the associated listed items.
To make the objects, technical solutions and advantages of the present application more clear, embodiments of the present application will be described in further detail below with reference to the accompanying drawings.
Fig. 1 is a schematic structural diagram of an outer rotor assembly of a generator according to an embodiment of the present application. The two rotor segments 100 of fig. 1 are two half-circle structural pairs that are assembled together to form the outer rotor assembly 10 of a generator in the shape of a hollow cylinder, and the dashed line that extends axially through the rotor segments 100 is the axis 20. Of course, a plurality of rotor segments 100 may be provided to form the outer rotor assembly 10 of a generator.
It should be noted that, for convenience of illustration, the embodiment of the present application takes two rotor segments 100 as an example, and in actual production, a rotor assembly of a corresponding generator developed according to the technical solution of the present application generally has more than two rotor segments 100. This is because, within certain limits, the greater the number of rotor segments 100 that are separated, the more convenient it is to transport and replace the damaged rotor segments with rotor segments of acceptable quality during later rotor assembly maintenance.
The term "hermetically connected" between any two rotor segments 100 means a state in which any two rotor segments 100 are fixedly connected to each other and put into operation, and during transportation, any two rotor segments 100 may be selectively hermetically connected or may be selectively non-hermetically connected.
As shown in fig. 1, the number of the selected rotor segments 100 is 2, and each rotor segment 100 corresponds to one rotor support segment 110 and one rotor cover segment 120. The rotor segments 100 are assembled into an outer rotor assembly 10 of the integrated generator and then secured to the generator shaft system to ensure a tight connection of the components inside the rotor segments 100. Any rotor support section 110 is removably connected to a corresponding rotor head section 120.
The rotor cover section 120 and the rotor support section 110 are assembled into the rotor section 100 for transportation, so as to enhance the structural strength of the outer rotor assembly 10 of the generator and reduce the deformation during transportation. Rotor support section 110 also includes a magnetic yoke disposed on an inner wall of rotor support section 110. The magnetic poles 130 are mounted at the yokes of the rotor support segments 110.
Fig. 2 is a schematic structural diagram of a rotor support section of an outer rotor assembly constituting a generator according to an embodiment of the present application. As can be seen in fig. 1 and 2, the rotor support section 110 includes: the rigidity adjusting device is fixedly connected with the rotor shell section.
Optionally, the rotor case section of the present embodiment includes an arc-shaped wall plate, and a baffle 150;
The baffle 150 extends radially along the upper and/or lower edges of the arcuate wall panel to which the baffle 150 is fixedly attached. The rigidity adjusting device comprises a first bearing part and/or a second bearing part, the first bearing part is arranged on the outer surface of the arc-shaped wall plate, for example, the annular rib plate 115 in fig. 1 can be understood as a member belonging to the first bearing part. 119 in fig. 6 also belongs to the component of the first force-bearing part.
The second force bearing part is arranged on the outer surface of the baffle plate and extends to the outer surface of the arc-shaped wall plate through the connecting position of the arc-shaped wall plate and the baffle plate 150. For example, the L-shaped rib 116 in fig. 2 can be understood as a member belonging to the second messenger.
optionally, one end of the second force bearing part extends to the edge of the baffle 150 close to the rotating shaft; and the second force bearing part is fixedly connected with the baffle 150.
optionally, a flange 114 is fixedly connected to the inner side of the baffle 150, the flange 114 is connected to the rotating shaft, and the flange 114 is in contact with the second force bearing part.
fig. 2 shows one end of the L-shaped rib 116 belonging to the second force-bearing part, extending from the outer circumferential wall of the annular baffle 131, through the inner circumferential wall of the annular baffle 131, to the edge of the baffle 150 close to the rotating shaft; and the L-shaped rib plate 116 belonging to the second force bearing part is fixedly connected with the baffle 150 and/or the annular baffle 131. The annular baffle 131 in the embodiments of the present application may be present as a structure facilitating the sealing action against the outer rotor assembly.
Optionally, a flange 114 is fixedly connected to the inner side of the baffle 150 in the embodiment of the present application, the flange 114 is connected to the rotating shaft, and the flange 114 is in contact with the second force-bearing part.
The rotor support section 110 is provided with a first bearing part in the structural form of an annular rib plate 115 and a second bearing part in the structural form of an L-shaped rib plate 116, and the first bearing part and the second bearing part are integrally connected with the rotor support section 110, so that the deformation of a product in the manufacturing, transporting and assembling processes can be effectively reduced. The L-shaped rib should contact the flange 114 to ensure uniform overall stress on the rotor spider section 110. Optionally, if cooling is required, heat dissipation ribs may be designed outside the yoke of the rotor support section 110.
The rotor sections of the embodiments of the present application are described above as including at least two rotor support sections and a plurality of rotor cover sections corresponding to the number of rotor support sections, and any rotor support section is detachably connected to the corresponding rotor cover section. The implementation of the detachable connection between the rotor support section 110 and the corresponding rotor cover section 120 is described in detail below with reference to fig. 2-5.
optionally, the rotor support segments 110 further include a flange member, two adjacent rotor support segments 110 are fixedly connected by the flange member, a sealing groove 113 is formed in the flange member, and a sealing member is disposed in the sealing groove 113.
Optionally, the rotor support section 110 of the present embodiment further includes a first connecting flange 111 and a second connecting flange 112. A first connecting flange 111 and a second connecting flange 112 are arranged between two adjacent rotor segments 100, and the first connecting flange 111 and the second connecting flange 112 are used for fixedly connecting two adjacent rotor segments 100.
As shown in fig. 2, the first connecting flange 111 and the second connecting flange 112 are respectively of an L-shaped structure, two sides of the L-shape extend along the rotor support section 110 and the rotor cover section 120 respectively, the openings are opposite and separated from two ends of one rotor section 100, and the two ends are attached to and fixedly connected with end faces of the rotor section 100. And the first and second connection flanges 111, 112 each project radially outwardly from the rotor part.
The first connecting flange 111 is provided with a first sealing groove 113 with a preset shape, and the shape of the first sealing groove 113 is substantially similar to that of the first connecting flange 111, and is preferably arranged on the inner side of the first connecting flange 111. A seal is provided in the first seal groove 113. Optionally, the sealing element comprises a sealing strip or a sealing ring which extends through the plane of the connecting flange 111. The sealing ring can be a standard O-shaped sealing ring or a rectangular sealing ring or other sealing rings, and the sealing of the inner side and the outer side of the generator at the joint is realized through the extrusion deformation of the sealing ring.
Optionally, in the embodiment of the present application, a sealant may be further coated at the opening positions of the two ends of the first sealing groove 113 and the joint surface of the first connecting flange 111 and the second connecting flange 112.
Optionally, after assembly, the first connecting flange 111 and the second connecting flange 112 between adjacent rotor support sections 110 are in contact, and the rotor support sections 110 are fixed by bolts or other detachable methods.
Optionally, rotor support section 110 of the embodiments of the present application rotor support section 110 further comprises a magnetic yoke disposed on an inner wall of rotor support section 110; when a generator in the form of an inner rotor is used, the yoke is arranged on the outer wall of the rotor support section 110. When an outer rotor form of generator is used, the magnetic poles 130 are mounted at the yokes of the rotor support segments 110. The first and second connection flanges 111 and 112 are provided with mounting planes 118 for fixing the magnetic poles 130. An example of the specific location of the mounting plane 118 can be seen in fig. 3.
Optionally, the second connecting flange 112 can also be provided with a mounting surface 118 for fixing the poles of the pole 130.
FIG. 4 is a schematic structural view of a rotor end cover section. Fig. 5 is an enlarged schematic view of the circled labeled area in fig. 4.
Since the end faces of the rotor segment 100 usually have a certain thickness, the first and second connecting flanges 111, 112 described above are used. Other shapes of the connecting flange may be chosen for a smaller thickness of the contact surface of the component.
a third connecting flange 121 and a fourth connecting flange 122 are disposed between adjacent rotor cover sections 120 of the present embodiment, and the third connecting flange 121 and the fourth connecting flange 122 are used to fixedly connect two adjacent rotor cover sections 120.
Optionally, the third connecting flange 121 and the fourth connecting flange 122 are respectively in a "straight" structure, are separated from two ends of one rotor cover section 120, and are attached and fixedly connected to the end face of the rotor cover section 120. The flange with the straight-line structure can play a role in fixedly connecting two adjacent rotor end cover sections 120 and can also reduce the weight of the finished product of the rotor end cover sections 120 as much as possible.
The third connecting flange 121 is provided with a second sealing groove 123, the shape of the second sealing groove 123 is substantially similar to the third connecting flange 121, and the second sealing groove 123 is preferably arranged inside the third connecting flange 121, and a sealing strip or a sealing ring is arranged in the second sealing groove 123.
Optionally, the first connecting flange 111 and the second connecting flange 112 of the rotor support section 110 of the embodiment of the present application are provided with positioning members.
for example, fig. 2 shows that the positioning member provided on the first connecting flange 111 is embodied as a first positioning pin hole 117. Fig. 3 is an enlarged schematic view of the circled labeled area in fig. 2.
The rotor bracket 110 is assembled and positioned by using positioning pins, and the number of the first positioning pin holes 117 provided in the first connecting flange 111 may be one or more. The first positioning pin hole 117 can be replaced by a hinged hole, and the hinged hole bolt has the characteristics of having the functions of a positioning pin and a bolt simultaneously and bearing transverse load. The unthreaded part of the positioning pin is equivalent to a positioning pin and is required to be contacted with positioning holes of two connecting pieces, and the outer diameter of the threaded part is smaller than that of the unthreaded part. Optionally, the rotor support 110 may be assembled by using keys.
Alternatively, the third connecting flange and the fourth connecting flange are respectively provided with a positioning component, and the positioning component may be the same positioning component as the positioning component described in the above embodiments, for example, fig. 5 shows that the positioning component provided on the third connecting flange is the second positioning pin hole 124.
FIG. 6 is another schematic view of a rotor spider section.
the force-bearing structure of the rotor support section 110 shown in fig. 6 is not realized by adding the L-shaped rib plate 116 and the annular rib plate 115, but the structural rigidity is enhanced by adopting a detachable reinforcing ring which is assembled by a plurality of reinforcing ring sections 119. Compared with the lattice shape of the L-shaped rib plate 116 and the annular rib plate 115, the peripheral wall of the reinforcing ring section 119 is plate-shaped, so that when the reinforcing form of the reinforcing ring section 119 is adopted within a possible adjustment area and adjustment thickness range, the same or similar reinforcing effect as that of the reinforcing form of the L-shaped rib plate 116 and the annular rib plate 115 of the previous embodiment can be achieved by structurally ensuring the reinforcing mode through the combined action of the L-shaped rib plate 116 and the annular rib plate 115. The stiffening ring segments 119 are fixed by welding (the amount of welding may not be too large for subsequent disassembly) at the locations where the amount of yoke deformation of the spider segments 110 is large, and 1 spider segment 110 may correspond to one or more stiffening ring segments 119. After the rotor support sections 110 are joined, the adjacent reinforcement ring sections 119 at the rotor support joint are spot-welded together at the welding point 190, while ensuring that the adjacent reinforcement ring sections 119 do not contact at the welding point 190, so that the rotor support sections 110 are connected only by the first and second connection flanges 111, 112, or the rotor support sections 110 are connected only by the third and fourth connection flanges 121, 122.
it should be noted that the sealing grooves on the first connecting flange 111 of the rotor support section 110 and the third connecting flange 121 of the rotor cover section 110 may be designed as needed, and only the sealing requirements of the modular rotor may be satisfied without completely penetrating the entire contact surface.
After the rotor assembly is assembled with the stator and shafting as a single unit, the stiffener ring section 190 can be removed and the stiffener ring section 190 can be retained as desired.
based on the same inventive concept, according to a second aspect of the embodiments, the present application provides a generator, which includes the outer rotor assembly of the generator provided in the embodiments of the present application.
The outer rotor assembly of the generator provided by the embodiment of the application comprises more than two rotor sections, and any two rotor sections are in sealing connection. The outer rotor assembly of the generator in the embodiment of the application is an outer rotor assembly of an existing integrated generator, and the outer rotor assembly of the generator is split into a plurality of rotor sections by adopting a simple and practical modular structure design, so that the technical problems that a permanent magnet direct-drive wind driven generator is too large in size and inconvenient to transport are successfully solved. The high-power wind driven generator can smoothly reach the designated work site through the processes of splitting, transporting and assembling.
embodiments of the present application provide a generator that includes an outer rotor assembly of a generator made up of a plurality of smaller sized rotor segments. The outer rotor of the generator is divided into a plurality of sections and respectively transported, so that the high-power output capacity of the wind driven generator is guaranteed, the feasibility of the wind driven generator in transportation is realized, the road transportation requirement of the current high-power generator is met, and the application area of the large-diameter permanent magnet direct-driven wind driven generator is enlarged.
in the description of the present application, it is to be understood that the terms "center", "upper", "lower", "front", "rear", "left", "right", "vertical", "horizontal", "top", "bottom", "inner", "outer", and the like indicate orientations or positional relationships based on those shown in the drawings, and are only for convenience in describing the present invention and simplifying the description, but do not indicate or imply that the device or element being referred to must have a particular orientation, be constructed in a particular orientation, and be operated, and thus, should not be construed as limiting the present invention.
the terms "first", "second" and "first" are used for descriptive purposes only and are not to be construed as indicating or implying relative importance or implicitly indicating the number of technical features indicated. Thus, a feature defined as "first" or "second" may explicitly or implicitly include one or more of that feature. In the description of the present invention, "a plurality" means two or more unless otherwise specified.
In the description of the present application, it is to be noted that, unless otherwise explicitly specified or limited, the terms "mounted," "connected," and "connected" are to be construed broadly, e.g., as meaning either a fixed connection, a removable connection, or an integral connection; they may be connected directly or indirectly through intervening media, or they may be interconnected between two elements. The specific meanings of the above terms in the present invention can be understood in specific cases to those skilled in the art.
In the description herein, particular features, structures, materials, or characteristics may be combined in any suitable manner in any one or more embodiments or examples.
The foregoing is only a partial embodiment of the present invention, and it should be noted that, for those skilled in the art, various modifications and decorations can be made without departing from the principle of the present invention, and these modifications and decorations should also be regarded as the protection scope of the present invention.
Claims (9)
1. a rotor assembly for an electrical generator, comprising: more than two rotor sections (100); a sealed connection between any two of the rotor sections (100);
The rotor section (100) comprises at least one rotor support section (110);
Each of said rotor support sections (110) comprising a rotor housing section, and a stiffness adjustment device; the rotor casing section comprises an arcuate wall plate, and a baffle (150);
The baffle (150) extends along the upper edge and/or the lower edge of the arc-shaped wall plate in the radial direction; the arc-shaped wall plate is fixedly connected with the baffle plate (150);
The stiffness adjustment device is connected with the rotor housing section; the rigidity adjusting device comprises a first bearing part and a second bearing part;
The first force bearing part is arranged on the outer surface of the arc-shaped wall plate;
The second force bearing part is arranged on the outer surface of the baffle plate and extends to the outer surface of the arc-shaped wall plate through the connection position of the arc-shaped wall plate and the baffle plate (150) in a bending mode.
2. the rotor assembly of the generator of claim 1, wherein the rotor segments (100) further comprise a number of rotor end cover segments (120) adapted to the number of rotor support segments (110), any rotor support segment (110) being detachably connected to the corresponding rotor end cover segment (120).
3. The rotor assembly of the generator as claimed in claim 2, wherein one end of the second messenger extends to an edge of the baffle (150) near the rotation axis; and the second bearing part is fixedly connected with the baffle (150).
4. The rotor assembly of the generator as claimed in claim 3, wherein a flange (114) is fixedly connected to the inner side of the baffle (150), the flange (114) is connected with the rotating shaft, and the flange (114) is in contact with the second bearing part.
5. The rotor assembly of the generator as claimed in claim 2, wherein the rotor support sections (110) further comprise flange members, and adjacent two rotor support sections (110) are fixedly connected by the flange members;
And a sealing groove (113) is arranged on the flange component, and a sealing component is arranged in the sealing groove (113).
6. Rotor assembly of an electrical generator according to claim 5, wherein the flange part extends along the rotor frame section (110) and/or the rotor end cover section (120) and projects radially outwards.
7. The rotor assembly of a generator according to claim 5, wherein the rotor support section (110) further comprises a magnetic yoke arranged on an inner wall of the rotor support section (110); and the rotor support section (110) is provided with a magnetic pole (130) at a magnetic yoke; the flange part is provided with a mounting plane (118) for fixing the magnetic pole (130).
8. A rotor assembly for an electrical generator, as claimed in any one of claims 5 to 7, wherein the flange member is provided with locating features thereon.
9. An electrical generator, characterized in that the electrical generator comprises a rotor assembly of an electrical generator according to any one of claims 1-8.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810668935.5A CN108711966B (en) | 2018-06-26 | 2018-06-26 | Rotor assembly of generator and generator |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810668935.5A CN108711966B (en) | 2018-06-26 | 2018-06-26 | Rotor assembly of generator and generator |
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| Publication Number | Publication Date |
|---|---|
| CN108711966A CN108711966A (en) | 2018-10-26 |
| CN108711966B true CN108711966B (en) | 2019-12-06 |
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| Application Number | Title | Priority Date | Filing Date |
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| CN201810668935.5A Active CN108711966B (en) | 2018-06-26 | 2018-06-26 | Rotor assembly of generator and generator |
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Families Citing this family (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109950991B (en) * | 2019-05-05 | 2023-07-04 | 新疆金风科技股份有限公司 | Magnet yoke assembly, motor, wind generating set and sleeving method of motor |
| CN111987870B (en) * | 2019-05-23 | 2023-03-24 | 北京金风科创风电设备有限公司 | Assembly method of large-diameter motor |
| CN110798007A (en) * | 2019-11-18 | 2020-02-14 | 沈阳工业大学 | Outer rotor structure of permanent magnet direct-drive wind driven generator |
| CN112953053B (en) * | 2019-12-11 | 2022-11-11 | 新疆金风科技股份有限公司 | Rotor reinforcing device and rotor sleeving method |
| CN113086383B (en) | 2019-12-23 | 2022-11-11 | 新疆金风科技股份有限公司 | Transportation tool structure, split motor module with transportation tool and transportation method |
| CN113098173B (en) * | 2019-12-23 | 2023-03-31 | 新疆金风科技股份有限公司 | Supporting tool structure, split rotor with tool and assembling method of motor rotor |
| CN113746236B (en) * | 2020-05-27 | 2023-04-07 | 北京金风科创风电设备有限公司 | Rotor support, motor rotor and motor |
| CN112018968B (en) * | 2020-07-31 | 2022-12-20 | 西安中车永电捷力风能有限公司 | Anti-magnetic structure |
| CN114079338B (en) * | 2020-08-10 | 2023-10-20 | 北京金风科创风电设备有限公司 | Rotor support module and reinforcing assembly |
| CN113964986B (en) * | 2021-12-21 | 2022-03-15 | 常州神力电机股份有限公司 | Super-large-specification wind power rotor workpiece and intelligent assembling system and method thereof |
Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102347651A (en) * | 2010-07-28 | 2012-02-08 | 通用电气公司 | Segmented rotor |
| CN102386694A (en) * | 2010-08-30 | 2012-03-21 | 通用电气公司 | Segmented stator assembly |
| CN108964301A (en) * | 2018-06-06 | 2018-12-07 | 新疆金风科技股份有限公司 | Rotor, motor and wind power generating set |
Family Cites Families (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE102011088660A1 (en) * | 2011-12-15 | 2013-06-20 | Siemens Aktiengesellschaft | Electric machine with housing and stator segments |
| DK2843810T3 (en) * | 2013-09-03 | 2019-09-23 | Siemens Gamesa Renewable Energy As | Generator for a wind turbine |
-
2018
- 2018-06-26 CN CN201810668935.5A patent/CN108711966B/en active Active
Patent Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102347651A (en) * | 2010-07-28 | 2012-02-08 | 通用电气公司 | Segmented rotor |
| CN102386694A (en) * | 2010-08-30 | 2012-03-21 | 通用电气公司 | Segmented stator assembly |
| CN108964301A (en) * | 2018-06-06 | 2018-12-07 | 新疆金风科技股份有限公司 | Rotor, motor and wind power generating set |
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| CN108711966A (en) | 2018-10-26 |
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Address after: No.107 Shanghai Road, Urumqi Economic and Technological Development Zone, Urumqi City, Xinjiang Uygur Autonomous Region Patentee after: Jinfeng Technology Co.,Ltd. Address before: No.107 Shanghai Road, Urumqi Economic and Technological Development Zone, Urumqi City, Xinjiang Uygur Autonomous Region Patentee before: XINJIANG GOLDWIND SCIENCE & TECHNOLOGY Co.,Ltd. |