U.S. patent number 3,678,727 [Application Number 05/067,476] was granted by the patent office on 1972-07-25 for stretch-draw tubing process.
Invention is credited to Robert G. Jackson.
United States Patent |
3,678,727 |
Jackson |
July 25, 1972 |
STRETCH-DRAW TUBING PROCESS
Abstract
Metallic tubing is drawn under tri-axial stress. A tube which
has the capability of cold work is used as a starting material. The
tube is stretched longitudinally under cold working conditions
without restraint against reduction in diameter and in cross
section into the plastic range but below the point of necking to
reduce its diameter. Then the tube is drawn with tools which
subject it to force inwardly on two axes at right angles to the
longitudinal axis and at right angles to one another under cold
working conditions into the plastic range. The cold worked
condition of the tube is retained during the stretching and
drawing.
Inventors: |
Jackson; Robert G. (St. Louis,
MO) |
Family
ID: |
22076246 |
Appl.
No.: |
05/067,476 |
Filed: |
August 27, 1970 |
Current U.S.
Class: |
72/274;
72/370.25; 72/378 |
Current CPC
Class: |
B21C
1/22 (20130101) |
Current International
Class: |
B21C
1/16 (20060101); B21C 1/22 (20060101); B21c
037/06 () |
Field of
Search: |
;72/274,283,367,368,378 |
References Cited
[Referenced By]
U.S. Patent Documents
|
|
|
3469425 |
September 1969 |
Spurr et al. |
|
Primary Examiner: Larson; Lowell A.
Claims
Having thus described my invention, what I claim as new and desire
to secure by Letters Patent is:
1. The process of drawing metallic tubing, starting with metallic
tubing capable of undergoing cold work, which comprises stretching
the tubing longitudinally under cold working conditions without
restraint against reduction in diameter into the plastic range but
below the point of necking to reduce the diameter and wall, and
then after relieving the tension drawing the tubing with tools
which subject it to force on two axes at right angles to the
longitudinal axis and at right angles to one another under cold
working conditions into the plastic range, the cold worked
condition of the tubing being retained between the operations.
2. The process of claim 1, in which the drawing of the tubing with
tools is accomplished by compression of the tube wall in the radial
direction, and compressive hoop stress.
3. The process of claim 1, in which the drawing of the tubing with
tools is accomplished by tension of the tube wall in the radial
direction, and compressive hoop stress.
4. The process of claim 1, in which the drawing of the tubing with
tools is accomplished by compression of the tube wall in the hoop
stress direction and compressive radial stress.
5. The process of claim 1, in which the drawing of the tubing with
tools is accomplished by tension of the tube wall in the hoop
stress direction and compressive radial stress.
Description
DISCLOSURE OF INVENTION
The invention relates to a process of making metal tubes or pipes
of any cold workable metal by stretch-drawing.
A purpose of the invention is to reduce the wall thickness and
diameter of a tube by tri-axial deformation, one axis being the
longitudinal axis and the other two axes being at right angles to
the longitudinal axis and at right angles to one another.
A further purpose is to start with a tube capable of cold work and
preferably annealed, to stretch the tube longitudinally under cold
working conditions without restraint against reduction in diameter
and in cross section into the plastic range but below the point of
necking to reduce the tube cross section, and then to draw the tube
with tools which subject it to force inwardly on two axes at right
angles to the longitudinal axis and at right angles to one another
under cold working conditions into the plastic range, the tube
retaining its condition of cold work during the stretching and
drawing.
A further purpose is to perform the two axes drawing on the tube
with tools according to the process of sinking, plug drawing, core
drawing, rod drawing, taper drawing, rock-rite drawing, or
otherwise.
Further purposes appear in the specification and claims.
In the drawings I have chosen to illustrate the invention
diagrammatically, the drawings being selected with respect to
convenience in illustration and generality of description.
FIG. 1 is a broken side elevation of a metallic tube which may
comprise the raw material of the invention.
FIG. 2 is an end elevation of the tube of FIG. 1.
FIG. 3 is a broken side elevation of the tube subjected to uniform
stretching longitudinally, showing the result of the stretching in
reducing the cross-section or diameter and wall.
FIG. 4 is a broken side elevation of a tube after the first step of
compression drawing, in this case bar drawing, illustrating the
reduction in cross-section where both the diameter and wall
thickness are reduced.
FIG. 5 is an end elevation of a fragment of the tube of FIG. 4 to
enlarged scale showing one set of arrows or axis applying radial
pressure to the tube wall to reduce its thickness and another set
of arrows or axis applying hoop stress in the tube wall at right
angles to the radial axis.
FIG. 6 is a broken side elevation of the tube of FIGS. 4 and 5
which has been subjected to a first sinking operation, according to
the invention.
FIG. 7 is an enlarged fragmentary end elevation of the tube of FIG.
6, showing the first sinking. The sinking tools are suggested by
one set of arrows or axis applying stress radial of the tube wall,
and another set of arrows or axis applying stress at right angles
to said radial axis, both of the axes of stress being at right
angles to the longitudinal stress.
FIG. 8 is a broken side elevation of the result of the second
sinking operation applied to the tube of FIGS. 6 and 7.
FIG. 9 is an enlarged fragmentary end elevation of the tube of FIG.
8 after the second sink, one set of arrows or axis being radial and
the other set of arrows or axis being at right angles to said
radial axis, both of the axes being at right angles to the
longitudinal stress.
FIG. 10 is a broken side elevation of the result of the third
sinking operation on the tube of FIGS. 8 and 9.
FIG. 11 is an enlarged fragmentary end elevation of the tube of
FIG. 10 showing two sets of arrows to suggest the action of the
third set of sinking tools, one set of arrows showing stress in the
radial direction and the other set of arrows showing stress at
right angles to the radial direction, both axes of stress being at
right angles to the longitudinal direction.
FIG. 11a is a fragmentary enlarged end elevation of a tube which is
undergoing drawing according to the second step of Example 5, one
arrow being in the radial direction and the other set of arrows in
tension at right angles to the radial direction, both of the axes
of stress being at right angles to the longitudinal direction.
FIG. 12 is a stress-strain curve useful in explaining the
invention.
FIGS. 13 to 21 are photomicrographs of the tubing at various steps
in the process, examined at 100 diameters and electrolytically
etched with oxalic acid.
All of the specimens are of type 304 or 18 percent chromium and 8
percent nickel stainless steel of commercial grade.
FIG. 13 is a transverse section of the raw material of FIG. 1.
FIG. 14 is a longitudinal section of the raw material of FIG. 1.
FIG. 15 is a transverse section of the tube of FIG. 3 after
undergoing uniform stretching.
FIG. 16 is a longitudinal section of the tube of FIG. 3.
FIG. 17 is a transverse section of the tube of FIG. 4 after the bar
drawing pass.
FIG. 18 is a longitudinal section of the bar drawn tube of FIG.
4.
FIG. 19 is a transverse section of the tube of FIG. 6 after
undergoing the first sinking.
FIG. 20 is a transverse section of the tube of FIG. 8 after the
second sinking.
FIG. 21 is a transverse section of the tube of FIG. 10 after the
third sinking.
FIGS. 22 to 24 are photomicrographs relating to an experiment on
stainless steel type 304 tubing explained in Example 4. The tubing
was examined transversely at 200 diameters and electrolytically
etched with oxalic acid.
FIG. 22 was the result of stretching annealed tubing 7 percent and
sinking it.
FIG. 23 was the result of stretching annealed tubing 15 percent and
then sinking it.
FIG. 24 was the result of sinking annealed tubing.
In reducing tubes, stretching has been used, but without
recognition of the importance of having the tube stretched as an
integral part of a cycle of tri-axial straining, and without
recognition of the importance of allowing the tube to reduce in
diameter during stretching and to retain the effect of cold work in
a subsequent operation of drawing. Inscho U.S. Pat. No. 2,051,948
stretches metallic tubes longitudinally, but heats them to
recrystallization and also prevents reduction in diameter by using
an interior mandrel. Tanomura U.S. Pat. No. 1,415,415 stretches a
tube but prevents it from reducing in diameter by a fluid content
inside.
In the present invention, a tube is stretched and reduced in
diameter and cross section only as one step of a process of
tri-axial stretch-drawing, obtained from stretching, with the tube
retaining its cold work from stretching while it is undergoing
drawing.
The invention is operative on all ductile metals including those
which crystallize on the face centered cubic system, body centered
cubic system, hexagonical system and tetragonal system. Thus, it is
applicable to iron and its alloys, copper and its alloys, aluminum
and its alloys, zirconium and its alloys, titanium and its alloys,
nickel and its alloys, cobalt and its alloys, silver and its
alloys, gold and its alloys, platinum and its alloys, and many
other metals and alloy systems too numerous to mention.
Raw Material
The raw material must have a capability of further cold work, and
be in the form of a tube or tube blank. In many cases the raw
material will be fully annealed before stretching, but in other
cases it will have some heat treatment which does not fully
recrystallize. Thus, it may be partially annealed, stress relieved
or have an alloy solution heat treatment before stretching. If the
previous drawing of the tube blank leaves it capable of undergoing
further cold work, it may be used without a softening heat
treatment.
Stretching
The stretching is a uniform longitudinal pulling operation which in
its simplest form may be performed with a tensile testing machine
or any apparatus capable of gripping the tube blank at the ends and
producing a uniform elongation with capability of reduction in
cross section (diameter and wall thickness). Thus, a mandrel
drawing operation will not suffice.
The conditions under which the stretching is carried out must be
cold working conditions and if any heat is present, it must not be
sufficient to cause recrystallization.
By reference to FIG. 12, it will be seen what is accomplished by
the stretching. In a typical ideal stress-strain curve the point A
is the yield strength at 0.2 percent offset. Between the point of
origin and the point A the elongation is elastic and for practical
purposes the working is within the proportional limit. Between the
point A and B permanent deformation takes place. Point B is the
point of maximum stress which the metal can withstand under a
uni-axial tensile test. Between points A and B the metal undergoes
uniform strain throughout the length and cross section under test
and in this range the metal is plastically uni-axially deformed.
The effect of the elongation in this range is to reduce the
diameter of the tube undergoing stretching and to reduce the wall
thickness. Point C is the failure or fracture point. Between points
B and C the metal undergoes necking, and the deformation takes
place in a localized area. It is not proper to elongate to this
extent.
The effect of the stretching is to produce cold work and it is
important to preserve partially or wholly the effect of that cold
work in the subsequent drawing with tools.
In most cases the stretching will not extend all the way to the
point B, but will extend over a portion of the curve AB. In many
metals about 2 to 5 percent elongation is sufficient in the
stretching.
Drawing with Tools
The work is removed from the stretching, or permissibly the tube
drawing is performed in the same machine. The tube drawing applies
a force inwardly to the tube on two transverse axes at right angles
to the longitudinal axis of the stretching and at right angles to
one another. In effect it subjects the tube to compressive plastic
deformation.
In many cases the drawing with tools is accomplished in several
different operations, and they may be commercial tube reducing
operations such as sinking, plug drawing, core drawing, rod
drawing, taper drawing, rock-rite drawing or otherwise. Once again
they must be carried out under cold working conditions, that is,
below the recrystallization temperature. If any heat treatment is
used after the stretching or between the cold drawing operations,
it should not be sufficient to fully recrystallize as the effect of
the previous cold work would then be lost.
Accordingly, the tube is subjected to tri-axial stress being
stretched in the longitudinal direction by the stretching and in
the two transverse directions by the tube drawing.
Tri-axial forming of tubing produces a product which is
mechanically stronger than uni-axial or bi-axial drawing. Tri-axial
forming permits more cold deformation than uni-axial or bi-axial
forming. Also the crystallographic effect on cold worked metals is
less with tri-axial than with uni-axial or bi-axial forming. All of
these advantages of tri-axial forming and more are obtained by the
stretch-draw process on tubing. Some of these advantages will be
illustrated in the examples presented herein.
Subsequent Operations
In some cases, after longitudinally stretching and drawing with
tools, the next step will be another cycle of stretching and then
drawing with tools.
In some cases the product of the stretch-drawing may be heat
treated and then subjected to a further drawing operation which may
be stretch-drawing.
Likewise, in some cases the product of stretch-drawing may be heat
treated and then marketed. In other cases the stretch-drawn product
will be marketed without heat treatment.
EXAMPLE 1
Example 1 will be understood best by reference to FIGS. 1 to 11 and
13 to 21.
This is a specific illustration of application of stretch-drawing
to austenitic stainless steel type 304 18 percent chromium and 8
percent nickel.
The raw material in this case is a welded tube which has been
reduced by rod drawing to a tube blank 30, which has then been
fully annealed. The tube blank 30 is then gripped as by grips at
the ends and stretched according to FIG. 3 to form the stretched
tube 31. The arrows 32 suggest the elongation by grips. The results
of elongation in this case is of the order of 25 percent reduction
in tube cross-section and is in the range AB and not beyond the
point of necking. The operation is at ambient temperature in this
case, and the metal does not become hot enough to recrystallize.
There is no internal restraint on the tube, and therefore as shown
it is able to reduce its diameter uniformly and reduce its wall
thickness uniformly. After the stretching, the tube is subjected to
drawing with tools as shown in FIGS. 3 to 11.
FIG. 4 shows the tube 32 after the bar drawing and FIG. 5 by arrows
33 suggests the action of the tools in compression reducing the
tube on one transverse axis while arrows 34 suggest the reduction
of the tube on another transverse axis at right angles to the axis
33.
FIGS. 6 and 7 show the tube 35 after the first sinking operation.
The effect of the sinking operation in compressibly reducing the
tube is suggested by arrows 36 which show one transverse axis and
by arrows 37 which show the other transverse axis at right angles
to axis 36.
FIGS. 8 and 9 show the tube 38 after the second sinking operation.
Arrows 40 suggest the compressible reduction on one transverse axis
and arrows 41 suggest the reduction on another transverse axis at
right angles to axis 40.
FIG. 10 shows the tube 42 after the third sinking operation. Arrows
43 in FIG. 11 suggest the action of the tools in reducing the tube
by compression on one transverse axis and arrows 44 suggest the
action of compressing the tube on a transverse axis to right angles
to the axis 43.
No heat treatment was applied to the tube subsequent to the
stretching and through this sequence of bar drawing and sinking and
so the properties were built-up by cold work to a tensile strength
of more than 200,000 psi. The total tri-axial cold work resulted in
about an 80 percent reduction in tube cross-sectional area.
FIG. 13 shows a transverse photomicrograph of the blank 30, and
FIG. 14 is the longitudinal section. The grain size is ASTM 6.
The results of the stretch elongation of tube 31 is shown in
transverse section in FIG. 15 and in longitudinal section in FIG.
16. Severe deformation is indicated along the slip planes. The
grain size is ASTM 6.
FIG. 17 shows the cross section of the tube 32 after the bar pass,
and FIG. 18 shows the longitudinal section after the bar pass.
The grain size in cross section is ASTM 7, and the grain size in
longitudinal section is ASTM 7. The grains are elongated in the
longitudinal specimen. FIG. 19 shows a photomicrograph of the tube
35 after the first sink pass. The grain size is ASTM 8. FIG. 20
shows a photomicrograph of tube 38 after the second sink pass. The
grain size is ASTM 9.5.
FIG. 21 shows the photomicrograph tube 42 after the third sink
pass. The grain size is ASTM 10.
Table 1 shows the mechanical properties.
TABLE 1
Mechanical Properties
After Initial After Bar After After Tube Stretch Draw 1st Sink 3rd
Sink
__________________________________________________________________________
Yield Strength 46,900 130,500 163,000 172,200 191,600 psi 0.2%
Offset Tensile Strength 96,400 142,900 188,200 198,000 227,000 psi
Elongation % 55 20 8 4 4 in 2 inch. Rockwell Hardness B72 C22 C44
C46 C48
__________________________________________________________________________
experience indicates the reductions accomplished by stretching, bar
drawing and three sinkings, without failure, and without
intermediate heat treatment, were more severe than could ordinarily
have been performed by conventional methods without intermediate
heat treatment.
An interesting effect is that the stretch tube 31 has a matte
surface which tends to hold lubricant on the surface of the tube
during the bar drawing. The other tubes have a shiny surface.
EXAMPLE 2
Example 2 demonstrates in a zirconium alloy that the hardening
produced by stretching serves to produce a more drawable material
with less tendency to gall or pick up on the tools than other
drawing operations. It is possible by stretch-drawing to produce
much more severe draws without failure of the work than would be
possible in drawing soft zirconium alloy.
The raw material is welded tube lengths of Zircaloy 2 which has the
following analysis:
Tin 1.4% Iron 0.13% Chromium 0.11% Nickel 0.06% Zirconium
remainder
The raw material is a nuclear circular canning tube having the
following properties:
Size .567" .times. .038" wall Condition The raw material was
annealed at 914.degree.F. This is not a full anneal since
crystallization takes place at 1250.degree.F. However, it permits
the tube to undergo subsequent cold work with a significantly
uniform stress pattern. Mechanical 70,000 psi yield strength
Properties with 0.2% set 90,000 psi ultimate tensile strength 36%
elongation in 2"
Three tubes 36 inches long were used for the test. All tubes
behaved the same, and the data presented are for the third
tube.
The tubes were engaged in the grip of a long throat tensile machine
and stretched without any lateral restraint. The tubes could be
stretched uniformly to approximately 14 percent but in order not to
produce any problem regarding the ultimate tensile strength or to
generate any necking the stretching was stopped at 11 percent. Each
tube was measured at two inch intervals before and after stretching
over the original middle 24 inches of the tube. The data were as
follows:
Percent Elongation After Stretch Diameter Location in 2" Max. Min.
Average Ovality
__________________________________________________________________________
1 10.9 .5370" .5365" .5367" .0005" 2 10.9 .5325 .5325 .5325 .0000 3
11.0 .5315 .5315 .5315 .0000 4 11.1 .5285 .5285 .5285 .0000 5 11.3
.5295 .5295 .5295 .0000 6 11.3 .5225 .5220 .5222 .0005 7 11.4 .5210
.5210 .5210 .0000 8 11.3 .5210 .5200 .5205 .0005 9 11.4 .5190 .5180
.5185 .0010 10 11.3 .5200 .5195 .5197 .0005 11 11.2 .5270 .5270
.5270 .0000 12 11.0 .5310 .5310 .5310 .0000
__________________________________________________________________________
The diameter was 0.567 inch before stretching with ovality of
0.0010 inch.
The tube was stretched to a load of 90,500 psi on the original tube
cross section or 97,200 psi on the cross section of the tube as
stretched.
After stretching, the tubes were drawn by conventional methods
without any intermediate heat treatment.
The maximum draw on fully annealed Zircaloy 2 tubing in
conventional practice is 30-35 percent of the cross sectional area
which must be followed by an anneal. Also, the tube must be coated
in normal practice with an ultra high plastic lubricant to prevent
galling and tearing. The specimens of the invention were drawn 32
percent of the cross sectional area by standard rod drawing without
special lubricant. The drawn surface was better than the usual
surface on such tubing. The tubing was then rod drawn for an
additional 24 percent and sunk for an additional 17 percent
reduction in cross section area. The total drawn tube reduction in
cross section area was 62 percent of the original area. This was
done without special lubricant and without any intermediate heat
treatment.
The operators performing the stretching and drawing operations were
familiar with drawing Zircaloy 2 by commercial methods, but they
did not know the composition of the tubes under test. When asked,
they stated that the tubes under test drew much easier than
Zircaloy 2 as they knew it. They also stated that the complete
drawing schedule could never have been performed with Zircaloy 2
regardless of what lubricant was used or what technique was used.
These operators also did not know that the blank which was their
starting material had already had 11 percent reduction, or that it
was not in its softened condition when they received it. A full
anneal of the starting material would permit more stretch in the
tube before drawing. This would indicate that Zircaloy 2 could be
drawn further by using the tri-axial stress method of the present
invention. The operators also were of the opinion that they could
have drawn the test pieces further without damage.
The final tubes were inspected visually and found to be acceptable.
A dye penetrant inspection was also performed, and the tubes were
found to be of high quality. The following Table 2 analyzes the
results obtained in the various steps:
Size Increment Resulting Reduction of Total Reduction Deformation
Inches Area in % in Area % of 2 In.
__________________________________________________________________________
Starting .567 OD .times. 0 0 Material .038 wall Uni-axial .522 OD
.times. 11 11 Stretch .0365 wall 1st Bi-axial .463 OD .times. 32 40
Rod Draw .0280 wall 2nd Bi-axial .394 OD .times. 24 54 Rod Draw
.0250 wall Bi-axial .356 OD .times. 17 62 Sink Draw .0238 wall
__________________________________________________________________________
EXAMPLE 3
Solution heat treatment alloys such as aluminum alloys will respond
better to subsequent aging or resolution and aging due to more
uniform dispersion of elements by tri-axial forming.
Aluminum alloy 6061 has the following analysis:
Silicon 0.40-0.80% Iron 0.70% max. Copper 0.15 to 0.40% Manganese
0.15% max. Magnesium 0.8 to 1.2% Chromium 0.15 to 0.35% Zinc 0.25%
max. Titanium 0.50% max. Other 0.05% each and 0.15% total Aluminum
Balance
This alloy is solution heat treated and then stretch-drawn after
which it is aged. The tri-axial deformation also produces a three
dimensionally more uniform metal lattice distortion which responds
more uniformly and efficiently in the solution and subsequent
coherent precipitation. The more uniform dispersion of age
hardening particles is evident in superior properties.
EXAMPLE 4
In Example 4 type 304 stainless steel tubing is stretch-drawn, less
than the maximum amount in order to preserve ductility while
improving strength by cold work.
The purpose is to produce a stretch-drawn tube with properties
superior to existing tubing. The commercial application is
especially in tubing for hydrolyics and for a fast breeder reactor
in which work-hardened tubing 304 stainless steel has applications
in heat exchangers and condensers.
All of the tubes were produced from the same heat of type 304
stainless steel. All sinking was done with the same bench,
lubricant, die and operator starting with two blanks of previously
welded, drawn, and annealed tubing 16 feet in length before
stretching. Table 3 gives pertinent information concerned with the
operation. ##SPC1##
The results in the Table show that there was a significant
improvement in yield strength by tubes B and C as compared with
Tube D which is the control and also current practice. The
percentage reduction in area has been maintained at a high level.
The stretch-drawn tube is ten full points in hardness lower than
the straight sunk tube.
The microstructure of similar tubes shows that the stretch-drawn
tubes have less evidence of residual cold work. Thus, tube B of
FIG. 22 and tube C of FIG. 23 have less evidence of residual cold
work than the control of FIG. 24.
The appearance of the outside and inside of the stretch-drawn
samples was brighter and smoother than that of the straight sunk
sample.
The stretch-drawn tubes had a greater uniformity of tube size of
the entire 16 foot length.
A similar series of experiments performed on copper base alloys,
zirconium base alloys, other stainless steels and nickel alloys is
planned to prove that similar results are obtained in other alloy
systems. These alloys are recommended for tubing in desalination
equipment.
EXAMPLE 5
A further application of stretch drawing is to perform the two axes
drawing subsequent to the elongation by expanding the tube diameter
with tools according to the process of internal diameter expanding
with the mandrel, a plug or otherwise. This procedure is tri-axial
the same as that obtained from stretch followed by inward force
drawing except that the direction of the inward forces is reversed.
This process is suggested by FIG. 11a, where arrow 33' is radial
and arrows 34' indicate hoop stress in tension, rather than any
compression as in other forms. This process has the advantage of
working tubes with large outside diameter and light walls in which
stretching is performed first and is an easy operation, but inward
two axes drawing is a difficult operation due to wrinkling of the
wall, tearing, and the like. For an outside diameter of two inches,
type 304 stainless steel tubing with a wall thickness of 0.0050
inch, the wall can be stretched and then an internal plug expanded
to bring the outside diameter to two inches again, with a net
reduction in wall thickness to 0.0040 inch. Note that this wall
reduction can be accomplished without touching the tube outside
diameter.
It will be evident that when it is indicated that the tension
stretching of the tube is a separate step applied first and the
compression or tension in the radial direction plus the compressive
hoop stress or the compression and tension in hoop stress plus the
compressive radial stress are separate steps, it is intended to
indicate that after the stretching the tension is relieved before
the subsequent operation is performed.
In view of my invention and disclosure, variations and
modifications to meet individual whim or particular need will
doubtless become evident to others skilled in the art, to obtain
all or part of the benefits of my invention without copying the
process shown, and I therefore claim all such insofar as they fall
within the reasonable spirit and scope of my claims.
* * * * *