U.S. patent number 3,672,142 [Application Number 05/023,432] was granted by the patent office on 1972-06-27 for winding apparatus and method.
This patent grant is currently assigned to American Chain & Cable Company, Inc.. Invention is credited to William J. Gilmore.
United States Patent |
3,672,142 |
Gilmore |
June 27, 1972 |
WINDING APPARATUS AND METHOD
Abstract
Method and apparatus are disclosed for producing a composite
multiwire structure by helically wrapping at least one wire
structure about a core element and, prior thereto, imparting
undulating longitudinal movement to the wire structure at a point
located closely to the point of wrapping to effectively control
torsion naturally induced in the wire structure during the wrapping
operation.
Inventors: |
Gilmore; William J. (Manitou
Beach, MI) |
Assignee: |
American Chain & Cable Company,
Inc. (New York, NY)
|
Family
ID: |
21815060 |
Appl.
No.: |
05/023,432 |
Filed: |
March 27, 1970 |
Current U.S.
Class: |
57/17; 57/19;
57/9 |
Current CPC
Class: |
D07B
7/14 (20130101); D07B 7/025 (20130101); B21F
7/00 (20130101); D07B 2207/209 (20130101) |
Current International
Class: |
B21F
7/00 (20060101); D07B 7/00 (20060101); D07B
7/14 (20060101); D07b 003/04 () |
Field of
Search: |
;57/17,19,3,6,9,13,15,139,144,145,156,160,161,166,137,138,18,59 |
References Cited
[Referenced By]
U.S. Patent Documents
Primary Examiner: Watkins; Donald E.
Claims
I CLAIM:
1. Apparatus for wrapping at least one wire structure about a
longitudinal axis to produce a composite multiwire structure having
an absorbed torsional stress comprising:
a. means for directing each wire structure from a supply along a
path converging at a predetermined point along said axis;
b. means for rotating each wire structure about said axis as it is
being advanced toward the point of convergence to helically wind
the wire structure at said point with an induced torsion; and
c. torsion isolation means disposed along the converging path of
travel of said wire structure for isolating torsion in said wire
structure to the portion disposed downstream thereof.
2. Apparatus according to claim 1 wherein:
a. said torsion isolation means is located in closely spaced
relationship to said point of convergence.
3. Apparatus according to claim 2 wherein said torsion isolation
means includes:
a. means for applying pressure to each wire structure in generally
opposing directions transverse to its direction of travel to
thereby impart undulating movement to each wire structure as it is
advanced toward said point of convergence, said means compressively
engaging each wire structure during said undulating movement.
4. Apparatus according to claim 3 wherein said means for applying
pressure to each wire structure comprises:
a. a plurality of spaced rollers engaging one side of each wire
structure; and
b. a plurality of spaced rollers engaging the other side of each
wire structure, the rollers engaging the one side of each wire
structure being aligned between the rollers engaging the other side
of each wire structure.
5. Apparatus according to claim 4 wherein:
a. the rollers of said torsion isolation means are in compressive
engagement with each wire structure.
6. Apparatus according to claim 5 wherein:
a. each roller of the torsion isolation means compressively engages
the wire structure against the next downstream roller.
7. Apparatus according to claim 6 further including:
a. spool means for said supply having an axis of rotation which is
coincident with the axis of the composite multiwire structure.
8. Apparatus according to claim 7 further comprising:
a. means for feeding a core wire structure along said longitudinal
axis.
9. A method for wrapping at least one wire structure about a
longitudinal axis to produce a composite multiwire structure having
an absorbed torsional stress comprising the steps of:
a. directing each wire structure from a supply along a path
converging at a predetermined point along said axis;
b. rotating each wire structure about said axis as it is being
advanced toward the point of convergence to helically wind the wire
structure at said point with an induced torsion;
c. isolating torsion in said wire structure to the portion disposed
downstream of and spaced from said supply by subjecting each wire
structure to pressure in generally opposing directions transverse
to its direction of travel along said converging path to provide
undulating movement thereto and subjecting said wire structure to
opposed compressive forces during said undulating movement.
10. The method according to claim 9 wherein:
a. each wire structure is fed from a supply coil mounted for
rotation about an axis coincident with said longitudinal axis.
11. The method according to claim 10 further including the step
of:
a. feeding a core element along said axis as each wire structure is
rotated thereabout.
Description
BACKGROUND OF THE INVENTION
Multiwire strands generally include an inner load bearing core
element and a plurality of round wires wrapped helically in one or
more layers about the core element. For mechanical application, the
round wires are usually made of high yield strength material.
Typically, a plurality of these strands are themselves wrapped
helically about a suitable core element which may itself be a
multiwire strand to produce a wire rope or cable structure.
In the fabrication of multiwire strands or multistrand ropes of the
type described, a twisting action is imparted to the individual
wire or strand between the point of closing and the supply spool as
it is being wrapped about the core element. This twisting action
results in the build-up of induced torsional stress in the wire or
strand; and this stress becomes additive creating the danger of
eventual breakage, snarling or other malfunction of the wire or
strand during the stranding operation. To overcome this problem
stranding equipment normally associated with the wire rope industry
presently utilize what is commonly referred to as "planetary
action" to accomplish basic stranding and closing of wire and
strand elements about a core element. With planetary action, a line
drawn radially outward from the center axis of the wire or strand
to intersect a given point on the circumference of the wire or
strand would always extend in the same direction as the wire or
strand is being wound about the core element. In other words, if a
line were scribed on the top of the wire or strand as it was being
payed out from the supply spool, that line would contact the
surface of the core element (at its lowest point) only once in
every lay length and would be spaced farthest i.e. at a distance
equal to the diameter of the wire or strand) from the surface of
the core element at 180.degree. of wrap or one half the lay length
as measured from the point at which the scribed line contacts the
core element.
Costly and complex cradles and planetary devices used in planetary
winding machines restrict their usefulness from the standpoint of
general application and render the use of such machines
economically feasible only for large production runs and large
manufacturing concerns. In addition, because conventional planetary
winders of the type described are quite large in size and mass the
speeds at which they can be operated is likewise restricted thus
making their general use and installation even more economically
unattractive.
SUMMARY OF THE INVENTION
In accordance with the teachings of the present invention, method
and apparatus are provided for making a composite multiwire
structure by continuously wrapping one or more wire structures
helically about a longitudinal axis in a simple, efficient, and
economical manner. The wrapping of each wire structure is effected
in a non-planetary fashion and in such a way that the build-up of
induced torsion in the wire structure is effectively controlled.
Each wire structure of the composite multiwire structure which is
wrapped in this manner may be a single wire or, in certain cases, a
multiwire structure.
In the presently preferred embodiment of this invention the
composite multiwire structure is formed by helically wrapping at
least one wire structure about a longitudinal axis defined by a
longitudinally moving core element as the wire structure is
advanced along a predetermined path converging with the path of
movement of the core element. Advantageously, a plurality of single
element wire structures are helically wrapped in side-by-side
relationship about the core element to form a single layer of a
composite strand structure. The actual wrapping is accomplished by
simultaneously moving the core element in a longitudinal direction
and rotating each wire structure in a non-planetary fashion about
the moving core element to effect the helical wrap at the point of
convergence of the wire structures and the core element.
For controlling the amount of torsion induced in the wire structure
due to its rotational movement about the core element, torsion
isolation means through which each wire structure is directed is
disposed in the path of travel of the wire structure between its
supply spool and the point at which it converges with the core
element. This means is located in closely spaced relationship to
the point of convergence between the wire structure and the core
element and comprises a plurality of pressure rollers engaging
either side of the wire structure. These rollers exert pressure on
the wire structure in generally opposing directions transverse to
the direction of movement of the wire structure toward the core
element. Also, the rollers engaging one side of the wire structure
are disposed alternately in relation to the rollers engaging the
other side of the wire structure in such a manner that undulating
movement is imparted to the wire structure in a zone located
upstream and relatively near to the point at which the wire
structure is wrapped about the core element.
With this arrangement, the torsion induced in the individual wire
structure is contained in the zone between the pressure rollers and
the point of convergence or closing. This forces the wire structure
to absorb the torsional stress as it is being wrapped about the
core element. Also, because of the relatively short distance
between the pressure rollers and the point of closing, the induced
torsion does not become additive and hence it is possible to
continuously wrap the wire structure about the core element without
danger of breakage of the wire structure in torsion.
BRIEF DESCRIPTION OF THE DRAWINGS
FIG. 1 is a diagrammatic illustration of apparatus constructed in
accordance with the teachings of this invention.
FIG. 2 is an enlarged elevation view, partially broken away, of the
apparatus employed to isolate torsion induced in the wire structure
as it is being wrapped about the core element.
FIG. 3 is a cross-sectional view taken along the lines 3--3 of FIG.
2.
DETAILED DESCRIPTION OF THE INVENTION
With reference to FIG. 1, there is shown apparatus for continuously
wrapping two wire structures 1 and 1' about a longitudinal axis in
helical relationship to produce a composite multiwire structure. In
the presently preferred embodiment of this invention the wire
structures 1 and 1' are wrapped about a core element 2 which is
disposed along the longitudinal axis. As is clear from FIG. 1, the
apparatus for wrapping the wire 1' is substantially identical to
that for wrapping the wire 1. Accordingly, the parts of the
apparatus for wrapping wire 1' corresponding to like parts of the
apparatus for wrapping wire 1 will be designated by the same
reference numerals with the suffix prime ('). Also, the following
description of the invention will be made primarily with respect to
wrapping of the wire 1, it being understood that such description
applies equally to the wrapping of wire 1'.
The wire structure 1 is made of high yield strength material and
may comprise a single round wire or, alternatively, a multiwire
structure comprising a plurality of helically wound single round
wires. Likewise, the core element 2 may comprise a single wire or a
multiwire construction. The wire structure 1 is made of high yield
strength material in the sense that it resists bending or will not
easily take a permanent set. An example of such material is steel.
Where the wire structure 1 is multiwired, as for example with a
strand, wrapping about the core will, depending on the direction of
wrap of the individual wires of the strand, tend to either tighten
the wires of the strand or unwrap them. Accordingly, this should be
taken into account when wrapping strands about the core so that the
strands chosen will have the proper characteristics permitting such
wrapping.
The core element 2 is moved longitudinally in the direction
indicated by arrow 3 by suitable drive means (not shown). The wire
structure 1 is fed from supply spool 4 and trained around guide
sheave 5 and then directed through torsion isolation means,
comprising a plurality of rollers 6, in a path converging toward a
predetermined point along the path of movement of the core element.
At the point of convergence, the wire structure 1 is helically
wrapped about the core element as shown in FIG. 1.
The supply spool 4 is advantageously mounted for rotation about an
axis coincident with the axis of the core element 2. The guide
sheave 5 and rollers 6 are rotatably mounted on a support member 7
disposed in radically spaced relation to the core element and
extending generally parallel to the direction of movement of the
core element. The support member 7 is mounted for rotation about
the moving core element by a bearing support 8 disposed
concentrically about the core element. Drive motor 9 is operatively
connected by suitable gearing 10, 10a to the support member 7 to
rotate it about the core element. Advantageously driven gear 10a,
bearing support 8, and spool 4 are hollow through their central
portion to permit free passage of the core element 2.
With the construction described above, the rotating wire structure
1 is payed out from the supply spool 4 and helically wrapped about
the core element at the point at which it converges with the core
element (point of convergence or closing). However, the supply
spool 4 has no planetary motion about the core element; and only
the wire structure after being directed radially away from the
spool, is rotated about the core element to effect the
wrapping.
As the wire structure 1 is rotated about the cored element 2 in the
manner described to effect the helical wrap, it has a tendency to
become twisted. This twist is initially confined to a vicinity near
the point of closing. However, upon continued rotation of the wire
structure about the core element, this twist gradually tends to
work itself back to the supply spool 4 and cause a build-up of
resulting torsional stress over the entire length of the wire
structure between the supply spool 4 and its point of convergence
with the core element. If this torsional stress is not effectively
controlled, the wire structure will eventually be caused to break
at some point along its length, become unalterably snarled, or
otherwise interrupt proper operation of the stranding
apparatus.
With the present invention, torsion isolation means comprising the
plurality of grooved pressure rollers 6 effectively controls the
torsion induced in the wire structure during the wrapping operation
and prevents undesirable torsional feedback through the apparatus.
As shown in the drawings, the pressure rollers engage either side
of the wire structure 1 at a closely spaced location relative to
the point of convergence or closing of the wire structure 1 with
the moving core element 2. The rollers engaging one side of the
wire structure are disposed in relation to the rollers engaging in
opposite side of the wire structure in such a manner as to produce
an undulating movement to the wire structure 1. Due to the location
of the rollers, this undulation is produced in a zone located
upstream and relatively near the point at which the wire structure
is wrapped about the core element. As shown, the rollers engaging
one side of the wire structure are also arranged alternately with
respect to the rollers engaging the other side of the wire
structure so that each portion of the wire 1 passing through the
rollers 6 is in contact with at least one of the rollers. The
rollers 6 act to apply pressure to the wire structure in generally
opposing directions transverse to its path of travel toward the
core element. The wire structure 1 is therefore subjected to
increased tension in that portion of its length passing between the
rollers, with compressive forces being exerted on the wire
structure at the pressure points between opposing pairs of
rollers.
Due to the undulating action imparted to the wire structure 1 by
its undulated path and due to the pressure exerted on the wire
structure between opposing pairs of rollers, induced torsion is
effectively contained in the zone A extending between the pressure
rollers 6 and the point of convergence of the wire structure 1 with
the core element 2. Feedback of resultant torsion into the region
upstream of the pressure rollers 6 is thereby effectively inhibited
in a controlled manner. As a result, the wire structure 1 is forced
to absorb torsional stress existing in zone A as it is wrapped
about the core element 2. Accordingly, any torsion existing in zone
A does not become additive and it is, therefore, possible to
continuously wrap the wire about the core element without danger of
breakage of the wire structure in torsion or other malfunction of
the wire structure in other areas of the apparatus.
With the apparatus of the present invention the supply spool 4 is
able to be mounted with its axis coinciding with the center axis of
the core element. This relieves the support member 7 of weight
which it would otherwise carry were the supply spool to be cradled
on the support member as is generally the case with conventional
planetary winding equipment. Furthermore, because of the separate
operating positions of the supply spool and support member, the
rotating support member 7 is of considerably less size and
complexity thereby permitting it to be rotated at higher and more
economical speeds than existing planetary winding equipment.
Moreover, the use of costly spool cradles and other planetary
devices required with conventional planetary winding equipment is
advantageously eliminated.
* * * * *