USPatent applicationPatented

Axial bolt-in cage stator frame assembly and method for assembling a stator

Granted 12 Feb 2002 · no office action yet

Assignee: General Electric

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Attorney: Attorney · Log in to unlock

Inventors: William Hunter Boardman, IV · Examiner: Nestor Ramirez · AU 2834 · TC 2800

Application· this page
9736843
filed 14 Dec 2000
Publication
Not published
not published
Patent
US 6,346,760
granted 12 Feb 2002

Life of the application

6 dated events
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Abstract

A stator cage design is provided in which the core is formed by stacking a plurality of lamination sectors each having grooves or cutouts defined at spaced locations about the outer periphery thereof. The grooves or cutouts of axially adjacent laminations are aligned to define longitudinal grooves for receiving keybars, each of which preferably has a generally circular cross section. A core flange assembly is disposed at least at each longitudinal end of the stacked laminations and includes a plurality of apertures therethrough for receiving the respective keybars. Compression bands are circumferentially disposed about the stacked lamination and keybar assembly to hold the keybars and radially lock the stacked laminations. The core is then concentrically disposed in a stator frame. The stator frame includes frame support plates for being bolted to the flanges of the stator core and radially extending frame section plates disposed at spaced locations along the length thereof between the frame support plates.

Description

5 parts
›BACKGROUND OF THE INVENTION

The present invention relates in general to dynamoelectric machines and, more particularly, to a stacked generator stator frame assembly adapted to reduce production cycle time, eliminate stacking rework and simplify the core construction. Thus, the present invention discloses an apparatus and method for mechanically coupling stator core lamination sectors to a stator frame.

To better understand the unique and advantageous features of the invention, it is helpful to have an understanding of conventional structures that provide this function. Exemplary such conventional apparatus are disclosed for example in U.S. Pat. Nos. 4,564,779 and 4,837,471, the entire disclosures of each of which are incorporated herein by this reference.

Referring to FIG. 1, a portion of a conventional stator 10 is shown and includes a generally annular stator frame formed by an outer wrapper plate 12 and a plurality of annular web plates 14 , only one of which is shown in FIG. 1 for clarity. Holes 16 are bored in the annular web plate 14 sufficiently close to the radially inner edge 18 so that part circular holes result. A plurality of keybars 20 are disposed in respective holes 16 . The keybars are used to attach the lamination sectors 22 to the web plates 14 . More specifically, the keybars 20 each have a cylindrical portion 24 which is disposed within the holes 16 of the annual web plates 14 and a dovetail portion 26 which extends radially inwardly from the cylindrical portion 24 . The dovetail portions 26 of the keybars mate with respective dovetail slots 28 in the radially outer curved edge 30 of stator core lamination sectors 22 . The portion of stator 10 shown in FIG. 1 includes several of the plurality of stator slots 32 which contain conventional current carrying conductors 34 (only one occupied slot being shown in FIG. 1 for ease of illustration). The conductors are held in the respective slot by a conventional dovetail retaining wedge (not shown). The stator core is actually built up by stacking large numbers of stator core lamination sectors 22 side by side in sandwiched-like relationship along the dovetails of the keybars. Generally, the sectors are segmental insulated laminations of silicon steel, each typically on the order of 0.3 to 0.5 mm thick. In the illustrated construction of stator 10 , the annular web plates 14 are rigidly fixed to outer wrapper plate 12 using weld beads 36 .

The above described generator stator frame design requires the frame application and machining be completed prior to cleaning and stacking. Keybars, either welded or bolted in the frame have dovetail locations which require very tight position tolerances to ensure stackablity. The frames are stacked by hand by rocking each core punching/lamination onto the keybar dovetail at axial slot positions located every 14 inches along the axial length of the keybar. The current method of producing stacked stator frames has little margin for fabrication/machining error and often results in rework and extended stacking cycle time.

›SUMMARY OF THE INVENTION

The invention is embodied in a stator cage design that allows parallel manufacturing of the stator frame and core, thereby reducing cycle time. The core is formed by stacking a plurality of laminations, each defined by a plurality of lamination sectors that each have one or more grooves or cutouts defined at spaced locations about the outer periphery thereof. The grooves or cutouts of axially adjacent laminations are aligned to define longitudinal grooves for receiving keybars, each of which preferably has a generally circular cross section. Core flanges are disposed at least at each longitudinal end of the stacked laminations and include a plurality of apertures therethrough for receiving the respective keybars. Compression bands are circumferentially disposed about the stacked lamination and keybar assembly to hold the keybars in the circumferential groves of the laminations thereby arch-binding the core, radially locking the stacked laminations. The core is then concentrically assembled into a stator frame. The stator frame includes frame support plates for being bolted to the flanges of the stator core and radially extending frame section plates disposed at spaced locations along the length thereof between the frame support plates. The radially compressed core assures that the core punchings/lamination sectors remain in position with no binding agent required. Since there is no gap between the adjacent lamination sectors, they are self locking under radial compression. Moreover, by providing round keybars with no dovetails, in accordance with a preferred embodiment, and pressing them against complimentarily circular depressions on the core outer surface, the keybars are self located. The radial fit between the keybar and core depression assures no back of core chatter which can occur with traditional keybar dovetails creating noise and excessive core to keybar dovetail clearances.

›BRIEF DESCRIPTION OF THE DRAWINGS

These, as well as other objects and advantages of this invention, will be more completely understood and appreciated by careful study of the following more detailed description of the presently preferred exemplary embodiments of the invention taken in conjunction with the accompanying drawings, in which:

FIG. 1 is a perspective view of a portion of a stator of a dynamoelectric machine showing a conventional keybar construction;

FIG. 2 is an elevational view of a portion of a stator core according to an embodiment of the invention;

FIG. 3 is a schematic cross-sectional view of an axial bolt-in cage star frame with radially compressed core embodying the invention;

FIG. 4 is a schematic cross-sectional view of an axial bolt-in cage stator frame with radially compressed core and core isolation system embodying the invention;

FIG. 5 is a cross-section illustrating an isolation system according to an embodiment of the invention; and

FIG. 6 is a cross section of an isolation system according to an alternate embodiment of the invention.

›DETAILED DESCRIPTION OF THE INVENTION · 1 of 2

Referring now to FIG. 2, a portion of a stator 110 is shown according to an embodiment of the invention. In contrast to the conventional assembly shown in FIG. 1, the outer wrapper plate 12 and annular web plates 14 conventionally provided to support and position the keybars have been omitted and the keybars are self aligned bars 120 which require no welding. In the illustrated, presently preferred embodiment, the bars are generally cylindrical, having a circular cross-section. The dovetail slots 16 conventionally provided on the outer peripheral edge of the lamination sectors that make up each layer of the core have been omitted and instead grooves or cutouts 116 are defined at spaced locations on the outer peripheral edge of the lamination sectors 122 for receiving respective keybars 120 . As illustrated in FIG. 2, the shape of the cutouts 116 generally corresponds to the shape of the outer surface of the keybars 120 . Thus, to accommodate the cylindrical keybars of the illustrated embodiment, the illustrated grooves or cutouts 116 are of a part circular shape. As described in greater detail below, to hold the keybars and radially lock the lamination sectors 122 that comprise the stacked laminations, compression bands 114 , one of which is shown in FIG. 2 and a plurality of which are shown in FIGS. 3 and 4, are tightened around the keybars, similar to belly bands used on large 2-pole generators.

With reference to FIGS. 2 and 3, one of at least two core flange assemblies 138 , 144 is disposed for receiving stacked laminations thereon. For convenience, core flange 138 will be referred to as a bottom core flange assembly although it is to be understood that the stacked laminations could be received on core flange assembly 144 . To form the stator, the core defining laminations 122 are stacked with respect to a central mandrel (not shown) to define the core 140 . The laminations 122 are stacked or otherwise disposed so that cutouts 116 are aligned with each other and with keybar receiving apertures 142 defined in the bottom core flange. Keybars 120 are inserted in apertures 142 respectively and seated in the longitudinal groove defined by the aligned cutouts 116 .

Since in the illustrated embodiment the keybars 120 are round with no dovetail and are placed against circular depressions 116 on the periphery of the core 140 , the keybars are self-located with respect to the core. An upper core flange assembly 144 is then lowered to capture the keybars 120 in respective keybar receiving apertures 146 defined therein. The compression bands 114 are applied about the keybars 120 as illustrated in FIGS. 3 and 4. The core is then tightened axially and also radially by tightening the compression bands to press the core. The keybar receiving apertures 142 , 146 may be radially elongated so as to accommodate the displacement of the keybars under radial compression by means of the compression bands 114 . The radial fit between the keybars 120 and the core depressions 116 along with the radial compression assures no core chatter, which can occur with traditional keybar dovetails, creating noise and excessive core to keybar dovetail clearances in the prior art. The core cage 148 is now complete because, as described below, the core flange assemblies 138 , 144 serve the dual function of compressing the core 140 and mounting the core to the stator frame 150 . Thus, unlike the traditional cage design, a cage embodying the invention consists essentially of a core 140 , flanges 138 , 144 , keybars 120 and compression bands 114 .

As illustrated and described above, the compression bands 114 serve a dual purpose in the assembly of the invention. In the illustrated embodiment, back of core (BOC) baffles 113 are disposed on certain compression bands to isolate different ventilation passages. The bands may be axially aligned with the frame section plates 152 to form ventilation sealing surfaces between inlet and outlet sections of the stator to facilitate BOC sealing.

To assemble the stator, the assembled core 148 is lowered vertically into the stator frame 150 which is comprised of a generally cylindrical outer housing wall 112 , frame section plates 152 , and frame support plates 154 , 156 . As shown in FIGS. 3 and 4 and the flange assemblies 138 , 144 are bolted to frame support plates 154 , 156 . In the illustrated embodiment, the bottom flange 138 is an assembly of a bottom flange component 137 that has a diameter smaller than the top support plate 154 , so that it may pass through the frame, clearing the section plates. Once inserted, a segmented L-shaped bolting ring or brackets 139 secure the bottom flange component to the frame support plate 156 .

The core vibration transmitted to the frame is minimized by supporting at the stator flanges as shown, taking advantage of the radial stiffness of the core flanges 138 , 144 as opposed to traditional spring loaded systems which attach to keybars. Additional vibration isolation can be provided at the bolted joints 158 as required. Indeed, as shown in FIGS. 4, 5 and 6 , by providing rubber washers 160 , grommets 162 , and spacers 164 or a cantilevered spring 166 such additional vibration isolation can be provided. More specifically, FIG. 4 schematically illustrates, by way of example, the provision of isolation coupling, generally shown at 168 , between the frame support plates 154 , 156 and the stator flange assemblies 138 , 144 . FIGS. 5 and 6 show two non-limiting examples of suitable core isolation structures. In FIG. 5, it can be seen that intermediate the flange assembly 138 , 144 and frame support plate 154 , 156 , a rubber spacer 164 is provided. Moreover, a rubber grommet 162 is provided to surround each of the bolt shafts 170 extending through the bolt holes of the flange assembly 138 , 144 . Finally, a rubber washer 160 is interposed between e.g. a metallic washer 172 and/or the bolt head 174 and flange assembly 138 , 144 . Providing a rubber spacer 164 , grommet 162 and washer 160 as illustrated in FIG. 5 ensures core isolation. Although not illustrated, a nut may be provided for receiving the bolt 170 on the far, right hand side of the support plate 154 , 156 .

›DETAILED DESCRIPTION OF THE INVENTION · 2 of 2

FIG. 6 illustrates an alternate assembly for providing core isolation with a cantilevered spring. In this illustration, a generally U-shaped cantilevered spring 166 is provided having a spring portion 176 oriented generally parallel to the axis of the core 140 and first and second depending legs 178 , 180 oriented at an angle of about 90° with respect to the spring portion 176 . Depending leg 178 is bolted via bolt 182 and nut 184 to the core flange assembly 138 , 144 and the other depending leg 180 is bolted to the support plate 154 , 156 , e.g. with a bolt 186 . Again, if deemed necessary or desirable, a nut (not shown) may be provided for the free end of the bolt 186 .

Although core flange assemblies 138 , 144 are shown in the illustrated embodiment only at longitudinal ends of the core 140 , intermediate core support plates can be added to accommodate longer machines.

Using the stator frame flange to support the core is a unique feature which makes the simplified design of the invention particularly cost effective.

The vertical bolted joint offers an advantage that each attachment shares the weight of the core equally, as opposed to a radially bolted joint in which load would vary as a sinusoidal distribution with the top and bottom bolts carrying most of the core weight. Another unique design feature of the invention which significantly reduces the cost of the core assembly is the use of core radial compression bands 114 with self positioning core lamination sectors 116 and keybars 120 which do not require dovetails. This aspect of the design greatly simplifies core stacking and lends itself nicely to an automated stacking process. As will be noted from FIG. 2, in particular the clearance between adjacent lamination sectors has been eliminated so that they become self locking and radial compression does not close the stator bar slots and cut into the bar insulation.

While the invention has been described in connection with what is presently considered to be the most practical and preferred embodiment, it is to be understood that the invention is not to be limited to the disclosed embodiment, but on the contrary, is intended to cover various modifications and equivalent arrangements included within the spirit and scope of the appended claims.

Claims as granted

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Classifications

5 codes
IPC · International Patent Classification
Section H — Electricity
  • H02K1/16
  • H02K1/18
USPC · US Patent Classification
310/259310/258310/91

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File wrapper

⤢ drag to zoomJan 2001Apr 2001Jul 2001Oct 2001Jan 2002Apr 2002USPTOApplicantNotice of allowance
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Pendency
1.2 y
425 days filing → grant
Office actions
0
none on record
Examiner
Nestor Ramirez
art unit 2834 · TC 2800
Citations: 9 back · 37 forward

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