U.S. patent number 3,808,868 [Application Number 05/320,895] was granted by the patent office on 1974-05-07 for pilot construction for necking die assembly.
This patent grant is currently assigned to United Can Company. Invention is credited to Wayne F. Wolfe.
United States Patent |
3,808,868 |
Wolfe |
May 7, 1974 |
PILOT CONSTRUCTION FOR NECKING DIE ASSEMBLY
Abstract
An annular die member and internal pilot for forming a
reduced-diameter cylindrical neck on the end of a cylindrical can
body having a side lap, wherein no orientation of the lap relative
to the die assembly is required. The pilot is longitudinally
segmented and the segments are each resiliently biased outwardly so
that the segment or segments adjacent the lap may yield inwardly to
accommodate the lap while the other segments provide a full
circumferential support to the can body end. The pilot is axially
movable relative to the annular die member as a can body end is
inserted into the die assembly so that there is no relative
movement between the pilot segments and can body as would otherwise
cause scratching of the interior of the can body.
Inventors: |
Wolfe; Wayne F. (Belmont,
CA) |
Assignee: |
United Can Company (Haywood,
CA)
|
Family
ID: |
23248288 |
Appl.
No.: |
05/320,895 |
Filed: |
January 4, 1973 |
Current U.S.
Class: |
72/361; 413/69;
72/370.02 |
Current CPC
Class: |
B21D
41/04 (20130101); B21D 51/2615 (20130101); B21D
51/2638 (20130101) |
Current International
Class: |
B21D
41/00 (20060101); B21D 41/04 (20060101); B21D
51/26 (20060101); B21d 041/04 () |
Field of
Search: |
;113/16,12AA
;72/94,354,358,370,353,465 |
References Cited
[Referenced By]
U.S. Patent Documents
Primary Examiner: Herbst; Richard J.
Attorney, Agent or Firm: Moore; Carlisle M.
Claims
Having thus described my invention, I claim:
1. Can necking apparatus comprising:
a ring die having a die surface facing inwardly towards the axis of
said die, said die surface including an annular portion of a
diameter substantially equal to the diameter of the can body to be
necked, an inwardly tapered surface and an annular portion of
reduced diameter,
a pilot disposed within and coaxial to said ring die, said pilot
having an outwardly facing surface thereon extending longitudinally
therealong opposite to said annular portion of reduced diameter of
said ring die and having a clearance therewith to receive a can
body therebetween,
said pilot including a plurality of longitudinally extending
segments radially disposed around said pilot, the outer surfaces of
said segments together forming said outwardly facing surface of
said pilot,
means mounting said segments on said pilot for individual
translatory movement of said segments towards and away from the
axis of said pilot to enable any of said segments to be moved
towards the axis of said pilot by the lap of a can body inserted
into said clearance,
means yieldably biasing each of said segments away from the axis of
said pilot and exerting a substantially equal outward force on each
segment even though a segment has been moved towards the axis of
said pilot by the lap of a can body inserted into said
clearance.
2. Can necking apparatus comprising:
a ring die having a die surface facing inwardly towards the axis of
said die, said die surface including an annular portion of a
diameter substantially equal to the diameter of the can body to be
necked, an inwardly tapered surface and an annular portion of
reduced diameter,
a pilot disposed within and coaxial to said ring die, said pilot
having an outwardly facing surface thereon extending longitudinally
therealong opposite to said annular portion of reduced diameter of
said ring die and having a clearance therewith to receive a can
body therebetween,
said pilot including a plurality of longitudinally extending
segments radially disposed around said pilot, the outer surfaces of
said segments together forming said outwardly facing surface of
said pilot,
means mounting said segments on said pilot for individual
translatory movement of said segments towards and away from the
axis of said pilot,
a sleeve inside said pilot, said sleeve having the outer surface
thereof engaging the inner surface of all of said segments, said
sleeve being filled with a pressure-transmitting fluid.
3. Can necking apparatus as set forth in claim 2, and further
including means for pressurizing the fluid in the interior of said
sleeve and for relieving pressure from the interior of said sleeve,
and means on said pilot for positively limiting movement of said
segments away from the axis of said pilot.
4. Can necking apparatus as set forth in claim 3 and further
including means for moving said pilot axially between first and
second positions relative to said ring die, said pilot having an
outwardly extending shoulder thereon at one end of said outwardly
facing pilot surface, said shoulder being adjacent one end of said
annular portion of reduced diameter when said pilot is in its first
position and said shoulder being adjacent the other end of said
annular portion of reduced diameter when said pilot is in its
second position.
5. Can necking apparatus comprising:
a ring die having a die surface facing inwardly towards the axis of
said die, said die surface including an annular portion of a
diameter substantially equal to the diameter of the can body to be
necked, an inwardly tapered surface and an annular portion of
reduced diameter,
a pilot disposed within and coaxial to said ring die, said pilot
having an outwardly facing surface thereon extending longitudinally
therealong opposite to said annular portion of reduced diameter of
said ring die and having a clearance therewith to receive a can
body therebetween,
said pilot including a plurality of longitudinally extending
segments radially disposed around said pilot, the outer surfaces of
said segments together forming said outwardly facing surface of
said pilot,
means mounting said segments on said pilot for individual
translatory movement of said segments towards and away from the
axis of said pilot,
means for yieldably biasing each of said segments away from the
axis of said pilot and for releasing said bias to allow a necked
can body to be stripped from said pilot.
6. Can necking apparatus as set forth in claim 5 and further
including means for moving said pilot axially between first and
second positions relative to said ring die, said pilot having an
outwardly extending shoulder thereon at one end of said outwardly
facing pilot surface, said shoulder being adjacent one end of said
annular portion of reduced diameter when said pilot is in its first
position and said shoulder being adjacent the other end of said
annular portion of reduced diameter when said pilot is in its
second position.
Description
BACKGROUND OF THE INVENTION
This invention relates to the formation of a reduced-diameter neck
on a "three-piece" metal can, i.e., cans having a can body made
from a rectangular piece of metal rolled into a cylinder with the
edges being joined at a soldered lap extending the length of the
cylinder, the two end pieces being therafter secured to the can
body by rolling operations.
It is well known that the end of a cylindrical body can be reduced
in diameter by forcing the can end into a die set comprising a ring
die having an annular inwardly facing die surface of a diameter to
produce the desired size neck, and an inner cylindrical pilot, and
an inner pilot, there being a clearance between the ring and pilot
to enable the can end to be received therebetween. It is also known
that the amount of clearance between the ring and pilot is quite
critical. Obviously, the clearance must be sufficient to allow the
can body to be inserted therebetween. However, if the clearance is
too great, then the can body end will not be properly supported
during the necking operation and undesirable wrinkling of the
necked portion will occur.
With deep drawn aluminum cans having no side laps, i.e., a uniform
wall thickness at all points around the can end, a ring die and
pilot assembly can be made easily with proper clearance. With
lapped can bodies, the problem is considerably greater. A fixed
ring die and pilot assembly could be made with a uniform spacing
therebetween equal to the wall thickness of the can and with a
large clearance at one point therebetween to accommodate the
thicker can lap. However, such a die assembly would require
orientation of the can body to the die assembly before the can body
is inserted thereinto. Such orientation is slow and expensive and
unsuitable for commercial operations.
One approach to the problem of providing a can necking die assembly
for lapped cans is that shown in U. S. Pat. No. 3,600,927 wherein a
floating pilot is disposed within the ring die, with the clearance
therebetween averaging half the combined thickness of the can wall
and the can lap. With this arrangement, no orientation of the lap
of the can body is required. This approach, however, requires that
the can bodies operated thereon by made to very close tolerances.
If the lap thickness is greater than that for which the ring and
pilot are designed, the can body cannot be inserted into the die
set. If the lap thickness is appreciably less, then the can body
end may not be suitably supported during the necking operation, and
wrinkling of the can end may result.
The floating pilot approach also has an inherent drawback resulting
from the fact that the ring and pilot members are both circular in
cross section. At the point wherein the can lap is between the
members the gap therebetween must obviously be at least equal to
the thickness of the lap. The gap between the members gradually
diminishes around the die, in either direction from the lap, with
the least amount of gap, approximately the thickness of the can
body wall, being at the point diametrically opposite to the can
lap. As a result the gap on either side of the can lap and for a
substantial distance therefrom will be only slightly less than the
thickness of the lap. If the can lap is made by a process wherein
the lap thickness is substantially less than twice the thickness of
the can wall, the gap between the ring and pilot created by the lap
will not be too detrimental. However, if the can lap is formed in a
conventional manner, wherein the edges of the can body are simply
lapped one over the other and soldered together, the finished lap
will be as much as four times the thickness of the can wall. As a
consequence, if this type can body is necked with a floating pilot,
the gap between the die members for a substantial distance on
either side of the lap will be four times the thickness of the can
wall therebetween, and the can wall will not be properly supported
so as to prevent wrinkling thereof during the necking process.
The floating pilot approach also has an inherent drawback in that
as the can body end is forced into the die assembly the can body
end will slide along the surface of the pilot. If the can body has
a protective inner coating, such relative movement of the pilot and
can body can often cause detrimental scratching of this
coating.
SUMMARY OF THE INVENTION
The present invention utilizes an annular die member to reduce the
diameter of a can body pushed thereinto. In place of a solid
internal pilot, a segmented pilot is used, the pilot having its
cylindrical support surface formed by a plurality of longitudinally
extending segments, all of which are resiliently biased outwardly,
and each of which is capable of inward yielding relative to the
adjacent segments. Thus, as a can body is pushed into the die
assembly, the pilot segment or segments adjacent the can body lap
will yield inwardly to enable the can body end to be inserted
between the two die members. The remaining pilot segments will be
undisturbed and will provide a full circumferential support for the
can body end. With this arrangement no orientation of the can body
lap is required and considerable variation in lap thickness of the
can body can be accommodated.
In addition, the pilot is axially yieldable so that as the can body
end is inserted into the annular die member and engages the pilot,
the pilot will then move axially with the can body end during the
remainder of the necking operation. This movement together of the
pilot and can body end eliminates the scratching of the inner
surface of the can body as it is being necked.
BRIEF DESCRIPTION OF THE DRAWINGS
In the drawings forming a part of this application and in which
like parts are designated by like reference numerals throughout the
same,
FIG. 1 is a sectional view taken along the axis of the die
assembly, illustrating the position of the ring die and pilot
members prior to the insertion of a can body end thereinto;
FIG. 2 is a view similar to FIG. 1, illustrating the position of
the die members upon full insertion of a can body end
thereinto;
FIG. 3 is an enlarged sectional view, taken along the axis thereof,
of the pilot member;
FIG. 4 is a transverse sectional view of the pilot member, taken
along line 4--4 of FIG. 3;
FIG. 5 is a transverse sectional detail, on an enlarged scale,
illustrating the manner in which the pilot segments yield inwardly
to accommodate the can body lap.
DESCRIPTION OF THE PREFERRED EMBODIMENT
The can necking machine, generally indicated by the reference
numeral 10, comprises a base plate 11 to which the cup-shaped
adapter plate 12 is secured by mounting screw 13. Locking nut 14 is
threaded into the adapter plate 12, nut 14 having an inwardly
projecting flange 15 to engage ring die member 16 and hold the die
member and annular die shoe 17 securely in place against the end of
adapter plate 12.
The ring die member 16 has a die surface facing inwardly towards
the axis of the die member, the die surface comprising an annular
cylindrical portion 18 substantially equal to the normal outside
diameter of the can body to be necked, an inwardly tapered surface
19 and an annular cylindrical portion 20 of reduced diameter
substantially equal to the desired outer diameter of the neck to be
formed on the can body.
The pilot member 21, axially disposed within the ring die 16,
includes a cylindrical guide 22 disposed within adapter plate 12
for axial movement, between a first position (FIG. 1) wherein one
end of guide 22 engages shoulder 23 of die shoe 17 and a second
position (FIG. 2) wherein the other end of guide 22 engages
shoulder 24 of adapter plate 12. Compression spring 25 resiliently
biases guide 22 to its first position.
Pilot 21 further includes a cylindrical core 26 and retainer plate
27, these elements being firmly secured to guide 22 by screw 28. A
plurality of longitudinally extending support segments 30 are
radially disposed around the core, the segments 30 having outwardly
facing shoulders 31 and 32 which engage inwardly facing surfaces on
the retainer plate 27 and guide 22 to limit outward movement of the
segments.
Each pilot segment 30 has an outwardly extending shoulder 33
thereon and an outwardly facing surface 34 which extends from the
inner edge of shoulder 33 to the outer end of the segment. As seen
in FIG. 4, the individual surfaces 34 of the segments form an
outwardly facing annular cylindrical surface 34' and the individual
shoulders 33 form an annular shoulder 33' circumferentially of the
pilot. The annular shoulder 33' is adjacent the outer and inner
ends of the reduced-diameter die surface 19 when the pilot is in
its first and second positions respectively.
A flexible, fluid-impervious sleeve 35 is disposed within the pilot
21, around core 26, and with its outer surface 36 being in
engagement with the inner surfaces 37 of all of the pilot segments
30. A fluid path from the interior of the sleeve 35 to the exterior
of the assembly is provided by the lateral passages 38 through core
26, the axial passage 39 through screw 28 and the axial passage 40
through mounting screw 13 and the axial stub 41 thereof. A conduit
41 extends from passage 39 to two-way valve 43, this valve being
operable to supply fluid under pressure from a suitable source S to
the interior of sleeve 35, or to exhaust pressure therefrom. Stub
41 of mounting screw 13 is sealed to guide 22 by O-ring 44.
The outer cylindrical surface 45 of retainer plate 27 is slightly
less in diameter than the diameter of the surface 34' when the
segments 30 are in their farthest radially outward position.
Adapter plate 12 is provided with a passage 46 therethrough so that
the interior of the adapter plate is substantially at ambient
pressure regardless of the movement of guide 22 therein.
In operation, the interior of the flexible sleeve 35 is pressurized
from source S, which may be a source of compressed air. Merely for
purposes of illustration, the pressure may be in the order of
300-425 p.s.i.g. As a cylindrical can body 50 is forced axially
into the ring die 16, the can body end 51 first slides along the
die surface portion 18 without deformation. As the end of the can
is forced into engagement with and moves along the tapered die
surface 19, the diameter of the can body end will be reduced
thereby. Further movement of the can body end will then cause the
extreme leading edge of the can to be guided by surface 19 into
engagement with shoulder 33' on the pilot. Continued movement of
the can body will then force the pilot to move axially against the
bias of spring 25. The air pressure within the sleeve acts radially
outwardly on all of the pilot segments 30, causing these segments
to press outwardly on the can end to form a constant diameter neck
on the end of the can as the can end passes along the die surface
20 of the ring die 16.
At the same time, since the pilot segments 30 are each capable of
inward translatory movement against the bias of the pressurized
sleeve 35, those segments contacted by the thicker lap portion 52
of the can body will yield inwardly so that the lap can be received
between the pilot and the die surface portion 20 of the ring die
member 16, as seen in FIG. 5. Although the pilot segments 30 are
wider at their outer surface than at their inner surface, very
little total radial clearance is necessary between the segments to
provide for the relatively small amount of inward movement of the
segment or segments engaged by the can body lap. All of the
segments are capable of inward radial movement relative to the
segments on either side thereof, and thus no orientation of the can
body lap to the die assembly is required. Since the segments are
mounted on the pilot for individual translatory movement towards
the axis of the pilot, the outer surface 34 of the segment or
segments engaged by the can lap will remain parallel to the axis of
the pilot and parallel to the die surface 20 of the ring die to
provide proper support of the can body.
Many can bodies are provided with a very thin protective coating on
the inner surface thereof to prevent contact of the subsequent can
contents with the can body wall. It will be noted that as the can
body end is pushed into the ring die and as it engages and moves
the pilot axially, there is no relative movement of the pilot
segments 30 longitudinally or circumferentially relative to the
interior of the can body end. As a consequence, with no such
relative movement, there is an elimination of the scratching of the
internal coating on the can body as would otherwise occur if the
can body end were forced onto a fixed pilot.
The necking operation will be completed when the can body end has
pushed the pilot to its second position, i.e., when guide 22
bottoms against surface 24 of the adapter plate 12, FIG. 2.
The can body is now pulled axially from the die assembly. During
initial withdrawal, spring 25 forces the pilot to return with the
can body end until the pilot reaches its first position, again with
no relative movement between the pilot and can body taking place
during such travel. Shortly in advance of the pilot reaching its
initial position, valve 43 is operated to release the pressure from
the interior of sleeve 35. With the pressure relieved, there is
little outward force on the pilot segments and the can body end may
then be pulled therefrom without scratching of the inner protective
coating of the can body.
After the can body has been stripped from the die assembly, valve
43 is actuated to repressure the sleeve 35 in readiness for the
next can body.
As may be seen from the foregoing, the described pilot construction
has three significant advantages. First, no orientation of the can
body lap is required. Second, the outer surfaces 34 of all of the
pilot segments are in contact with the can body so that a full
circumferential support is provided to the interior of the can body
end as the cylindrical neck is formed thereon. Third, during the
necking operation scratching of the inner surface of the can body
is eliminated since there is no relative movement between the pilot
segments and the can body.
For a typical can body formed from tin plate having a thickness of
.006 inch the pilot segments should be formed to provide a
clearance of .007 between the outer cylindrical pilot surface 34'
and the reduced-diameter die surface 19 on the ring die. The
thickness of the can body at the lap 52 will be twice the thickness
of the tin plate plus the thickness of the solder 53 between the
lapped surfaces. The solder thickness may vary between minimum and
maximum acceptable limits of .004 to .013 inch. Thus, with a wall
thickness of .006 inch, the lap may vary from .016 to .025 inch in
thickness. However, the segmented pilot described herein can easily
accommodate such variations and still provide a firm
circumferential support to the entire periphery of the can body,
including the lap and the portions of the can body immediately on
either side of the lap. The outer surface 45 of the retainer plate
27 on the end of the pilot should have a diameter sufficiently less
than the expanded diameter of the pilot surface 34' so that the
necked-in lap of the can body can be easily stripped off the
pilot.
Although a spring 25 is shown to provide a bias force for the
pilot, it is to be appreciated that the guide 22 has a surface
equal to the cross-sectional area sealed by the stub O-ring 44 upon
which the pressure fluid acts in a direction to return the pilot to
its first position of FIG. 1. As a consequence, with a proper
sizing of this area, the fluid pressure alone may provide
sufficient bias force so that spring 25 can be eliminated if
desired.
In the apparatus described above, the necking operation has been
performed by moving a can body axially into and out of a stationary
annular die member. If desired, the very same results would be
obtained by holding a can body against axial movement and by
forcing the die assembly axially onto and off the can body end.
* * * * *