Method of producing a commutator of an electrical machine

Information

  • Patent Grant
  • 6643912
  • Patent Number
    6,643,912
  • Date Filed
    Monday, June 25, 2001
    23 years ago
  • Date Issued
    Tuesday, November 11, 2003
    21 years ago
Abstract
The invention relates to a method for producing a commutator ring (10) for a commutator of an electrical machine, in which the laminas (12) of the commutator ring and fastening means (18) are formed out of a band material (27), and a selectable number of laminas (12) are then closed to form the commutator ring. The fastening means are produced with a special tool (35) in the form of dovetail grooves (22) by means of a so-called furrowing operation, which is done simultaneously from both face ends of the laminas (12).
Description




BACKGROUND OF THE INVENTION




The invention is based on a method for producing a commutator ring for a commutator. It is known to produce commutator rings from a previously engraved band material for so-called roll commutators. In this process, an optionally profiled endless band, whose width is equivalent to the later axial length of the commutator, is provided transversely to the direction of motion of the band with grooves by means of a forming tool, so that laminas that are now joined together only via webs. Depending on the number of laminas in a commutator ring, a corresponding number of laminas is cut apart from the onward-moving, now shaped band and closed to form the commutator ring. To stabilize the commutator ring and to insulate the individual laminas from one another, the commutator ring is usually embedded together with a metal hub in an insulating compound.




In order to prevent axial and radial shifting of the laminas in the later intended use of the commutator ring, it is known—for instance from German Published, Examined Patent Application DE-AS 12 18 053—to cut barbs on the back side of the laminas for the sake of anchoring them in the insulating compound. This has the disadvantage that cutting the barbs reduces the usable thickness of the laminas of the commutator ring.




From U.S. Pat. No. 5,204,574, a commutator ring is also known which has dovetail profiles extending axially of the laminas, by means of which profiles securing of the laminas in the radial direction of the commutator is assured, but shifting in the axial direction of the commutator cannot be precluded.




To overcome this disadvantage, it is known from Published, Unexamined German Patent Application DE-OS 195 43 998, for the sake of axially securing the laminas, to design the dovetail profiles by means of a special process in such a way that via the axial spacing, an interruption of the dovetail profile is made. This production process is still relatively complex, however, making it more expensive.




SUMMARY OF THE INVENTION




In accordance with the present invention, dovetail grooves provided on the laminas are formed by simultaneous lateral furrowing of the laminas beginning at both face ends of the laminas by means of one tool each so that approximately in the middle of the laminas, a groove-free zone remains between the dovetail grooves.




The method of the invention for producing a commutator ring has the advantage over the prior art that its production is made still simpler and less expensive, and that even very special forms of the dovetail groove can be produced more simply, for the sake of especially good retention of the laminas.




Further advantages of the invention will become apparent from the ensuing description, the dependent claims, and the drawing.











BRIEF DESCRIPTION OF THE DRAWING




The invention will be described in further detail below in terms of two exemplary embodiments in conjunction with the drawings.





FIG. 1

is an elevation view of the face end of a profiled lamina band with furrowed dovetail grooves;





FIG. 2

is a cross section through the profile of the laminas in the direction A—A of

FIG. 1

;





FIG. 3

is an elevation view from the back side of the lamina profile band of

FIG. 1

;





FIG. 4

is a plan view of an apparatus for producing the lamina profile band;





FIG. 5

is a cross section along the line A—A of

FIG. 4

;





FIG. 6

is a cross section along the line B—B of

FIG. 4

;





FIG. 7

is a side view of a special tool for the apparatus of

FIGS. 4-6

for furrowing the laminas;





FIG. 8

shows the special tool in plan view,





FIG. 9

shows this tool in a front elevation view, and





FIG. 10

shows this tool in an enlarged detail of the face end of the furrowing knife;





FIG. 11

is a plan view on the face end of a lamina ring rolled into its finished form;





FIG. 12

shows a finished commutator in longitudinal section; and





FIG. 13

, as a further exemplary embodiment, shows a lamina profile band with double dovetail grooves.











DESCRIPTION OF THE PREFERRED EMBODIMENTS




In

FIGS. 1-3

, a lamina profile band is shown in fragmentary form as a lamina strand


27


, which has an L-shaped copper profile. In the engraving apparatus described in further detail hereinafter and shown in

FIGS. 4-6

, the lamina strand is machined in individual production steps. In a first step, by means of contrary dies, engraved grooves


20




a


,


20




b


are engraved in the lamina strand in a known manner, thus cutting the laminas


12


of a commutator apart from the strand. What remains between the laminas


12


is a connecting web


28


. In subsequent operating increments, dovetail grooves


22


are then made on the long sides of the laminas


12


; they serve the purpose of later anchoring of the laminas in the insulating material of the commutator.




The laminas


12


have a long leg


14


, whose outside later forms the running face of the commutator. A short, radially outward-pointing leg


16


serves to make contact of the laminas


12


with the winding terminals of the rotor of an electrical machine, not shown. The dovetail grooves


22


extend longitudinally of the back side of the laminas, or in other words axially of the commutator, and are interrupted approximately in their middle. What remains approximately in the middle of the laminas between the dovetail grooves


22


is a groove-free zone


26


.





FIGS. 4-6

show an apparatus


30


for producing a lamina strand according to

FIGS. 1-3

. In

FIG. 5

, in a longitudinal section through the apparatus


30


, the lamina strand


27


can be seen lying on its back on a support


31


, specifically with its short leg


19


downward. A feed device transports the lamina strand


27


toward the observer, and an embossed groove


20




a


is first engraved in each lamina


12


by an engraving tool, not visible here. Then by means of two toggle levers


33


that move vertically upward and downward and with the aid of one special tool each, the so-called furrowing tool


35


, as shown in

FIGS. 7-10

, one profiled dovetail groove


22


is furrowed into each long side of the laminas


12


simultaneously from both face ends of the laminas, or in other words from the right and left, in each case as far as the groove-free zone


26


of each lamina (see FIGS.


1


-


3


). The direction of motion of the tool


35


is horizontal. This involves a reciprocating motion by means of a toggle lever guide


36


. After each furrowing operating on the opposed sides of the adjacent laminas


12


, the lamina strand


27


is moved onward by one lamina


12


. During the furrowing operation, the laminas


12


are pressed against the support


31


of the apparatus


30


by means of a down-holding device


37


that can be seen in FIG.


6


. In

FIG. 5

, it can be seen that the furrowing tools


35


have dipped from the face ends of the laminas


12


into a longitudinal groove


22


a between laminas far enough that between the opposed furrowing tools


35


, the requisite spacing for creating the groove-free zone


26


still remains.




The furrowing tool


35


can be seen in

FIGS. 7-10

.

FIG. 5

shows the side view with its fastening holes


38


, with the aid of which it is fastened firmly in the apparatus


30


by screws


39


,


40


shown in FIG.


5


. The furrowing tool


35


has a double-edged furrowing knife


43


,


43




a


at the top and at the bottom, and the knife terminates at the front in a respective furrowing point


42


,


42




a


. In the plan view of

FIG. 8

, the point


42


of the furrowing tool


35


is seen. In

FIG. 9

, the front elevation view of the furrowing tool


35


is shown, and

FIG. 10

shows the lower portion of

FIG. 9

, substantially enlarged. It can be seen there that there is one furrowing edge


45


,


46


on each of the two sides of the furrowing knife


43


. With the aid of the furrowing knife


43


and the furrowing point


42


, the furrowing of the profiled dovetail grooves


22


is thus done simultaneously on both long sides of the embossed grooves


20




a


of the laminas


12


from both face ends as far as the middle remaining zone


26


, which remains free of dovetail grooves. Particularly from

FIG. 10

, it is clearly seen that as a result of the furrowing edges


45


and


46


of the lower furrowing knife


43


, one furrow each is made in the opposed long sides of the adjacent laminas


12


. As soon as the lower furrowing knives


43


have reached their serviceable lives, the furrowing tool


35


is removed from the apparatus


30


and rotated


180


about the longitudinal axis, so that the upper furrowing knife


43




a


can now be used.




Once the requisite number of laminas in the lamina strand


27


of

FIG. 1

is attained in succession in this way, this strand is cut from the profile band by the apparatus


30


,


15


and in the next station, a lamina ring


10


, as shown in

FIG. 11

, is formed from the lamina strand


27


in a known manner.




This ring comprises a plurality of annularly disposed laminas


12


, which seen in longitudinal section have an L-shaped profile. The laminas are then embedded with their dovetail grooves


22


for anchoring purposes in an insulating molding composition


11


, which can optionally also receive a metal hub at its hub bore


13


. After the lamina ring has been embedded, the connecting webs


28


between the laminas are twisted off in a the region of the running face of the collector, so that the laminas are now anchored in the collector hub in such a way that they are insulated from one another.





FIG. 13

shows a second exemplary embodiment of the invention, namely a lamina strand


27




a


with double dovetail grooves


22


and


22




a


. Once again, after the engraving of the longitudinal grooves


20




a


and


20




b


, the dovetail groove


22


is first furrowed into the lamina sides—as described above.




This is done in a first station of the apparatus


30


. In a succeeding station of the same apparatus, the upper dovetail grooves


22




a


are then furrowed into the sides of the laminas with a similar knife, as shown and described in

FIGS. 7-10

. Depending on the design of the furrowing knife profile, various forms of embodiment are possible. With such double furrows, the anchoring of the laminas


12


in the insulating material of the commutator hub is strengthened further, so that with such laminas, higher rotary speeds and larger commutator diameters can be achieved. Optimization with regard to the tear strength of the insulating material on the one hand and the lamina material on the other is expediently achieved by providing that the last furrows


22




a


made are embodied as relatively long.



Claims
  • 1. A method of producing a commutator of an electrical machine, comprising the steps of forming a commutator ring which has laminas; disposing the laminas side by side over a circumference of the commutator ring and shaping the laminas from a band material by engraved grooves; anchoring the laminas in an insulator body by dovetail grooves provided on inner sides and extending axially of the laminas so as to act as fastening means; and forming the dovetail grooves by simultaneous lateral furrowing of the laminas parallel to surfaces of the laminas, beginning at both face ends of the laminas by means of one tool each, so that approximately in a middle of the laminas, a groove-free zone remains between the dovetail grooves.
  • 2. A method as defined in claim 1, and further comprising using the tools for furrowing which are formed as knives; and moving the knives back and forth in opposite motion along sides of the laminas.
  • 3. A method as defined in claim 1, and further comprising forming the dovetail grooves by furrowing out with a further tool, in form of double dovetail grooves located one above the other on the sides of the laminas.
  • 4. A method as defined in claim 1, and further comprising using for the furrowing of the laminas an apparatus in which a strand of the laminas is placed in such a way that long legs of the laminas are oriented with their face ends toward the tool; and performing engraving of the engraved grooves between the laminas beforehand in the same apparatus.
  • 5. A method as defined in claim 1, and further comprising furrowing out lower grooves of the dovetail grooves in a first station on an apparatus; and furrowing out upper grooves of the dovetail grooves in a subsequent station in sides of the laminas. grooves.
  • 6. A method of producing a commutator of an electrical machine, comprising the steps of forming a commutator ring which has laminas; disposing the laminas side by side over a circumference of the commutator ring and shaping the laminas from a band material by engraved grooves; anchoring the laminas in an insulator body by dovetail grooves provided on inner sides and extending axially of the laminas so as to act as fastening means; and forming the dovetail grooves by simultaneous lateral furrowing of the laminas parallel to surfaces of the laminas, beginning at both face ends of the laminas by means of one tool each, so that approximately in a middle of the laminas, a groove-free zone remains between the dovetail grooves; and performing the farrowing simultaneously in two laminas located side-by-side on opposed sides of the laminas.
Priority Claims (1)
Number Date Country Kind
197 43 086 Sep 1997 DE
PCT Information
Filing Document Filing Date Country Kind
PCT/DE98/00941 WO 00
Publishing Document Publishing Date Country Kind
WO99/17409 4/8/1999 WO A
US Referenced Citations (3)
Number Name Date Kind
4358319 Yoshida et al. Nov 1982 A
5204574 Kanno et al. Apr 1993 A
5584115 Takahashi Dec 1996 A
Foreign Referenced Citations (5)
Number Date Country
12 18 053 Jun 1966 DE
195 43 998 May 1997 DE
0 019 472 Nov 1980 EP
899393 Mar 1961 GB
2 307 599 May 1997 GB