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Description  |
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BACKGROUND OF THE INVENTION
This invention relates to an improved method of pretreating aluminum sheet
for the resistance welding thereof.
The principle of resistance spot welding is based on heat generated by
electrical interfacial resistance to the flow of electric current between
two or more work pieces held together under force by a pair of electrodes
which act as electric conductors. Maximum heat is produced at the faying
surface (the mating surface of two sheets to be joined) by a short time
pulse of low-voltage high amperage current to form a fused nugget of weld
metal.
The interfacial resistance of the work pieces is both the promoter of and
the limiting factor of the process. Promoter because one requires
interfacial resistance at the faying surface to produce a weld. Limiting
factor because accumulation of heat generated by the interfacial
resistance at the electrode/work piece surface after a number of welds
leads to deterioration of the electrode tip. In resistance spot welding,
aluminum deterioration of the electrode tip is further accelerated by the
inherent physical, mechanical properties and surface condition of the work
pieces.
It is a well known and accepted fact that the resistance spot welding
weldability of aluminum in the as received mill finish condition is both
poor and erratic. The reason for this poor and inconsistent weldability
has been associated with the large variation in surface resistance which
in turn is related to the nature and non-uniformity of the oxide layer and
to the surface condition. One of the main goals of the aluminum industry
over recent years has been to improve the resistance spot welding
weldability of aluminum to a level acceptable by the automotive industry
as a prerequisite for the use of aluminum in autobody sheet.
Various methods have been suggested over the years for treating the surface
of aluminum in preparation for resistance spot welding. For instance,
Dorsey, U.S. Pat. No. 4,097,312 issued June 27, 1978 describes the
formation of an oxide coating on the aluminum surface and stabilizing this
by treatment with a hot aqueous alkaline solution containing long chain
carboxylic acids. An arc-cleaning technique is described by R. F. Ashton
and D. D. Rager in "An Arc Cleaning Approach For Resistance Welding
Aluminum", Welding Journal, September 1976, page 750. In addition, several
technical papers have been presented dealing with ways and means of
improving weldability.
SUMMARY OF THE INVENTION
The thrust of many of the surface treatments reported in the literature, in
general terms, has been to reduce the surface resistance equally on both
surfaces of the workpiece prior to welding. Although this has been shown
to be an improvement over untreated surfaces, it is now believed that
because the surface resistance of the workpieces in the as-received mill
finished state is both the promoter and the limiting factor of the
process, further improvement can be realized by purposely creating a
differential in surface resistance prior to welding. This differential
created between the two surfaces of the workpiece is such that the
interfacial resistance at the electrode/workpiece is both low in absolute
value and substantially lower than the interfacial resistance at the
faying surface.
Thus, the present invention in its broadest aspect relates to a method of
preparing an aluminum sheet for resistance welding in which both surfaces
of the sheet portion to be welded are treated, e.g. chemically cleaned, to
remove the non-uniform mill finish oxide layer. Then, a thin oxide layer
is provided on one surface and a thicker oxide layer is provided on the
other surface, thereby creating a differential in oxide thickness between
the surfaces of the sheet and hence a differential in surface resistance.
More specifically, the thinner layer which has a lower resistance is placed
next to the electrode, while the thicker layer of higher resistance
becomes one of the faying surfaces. Thus, since during welding the
surfaces with lower surface resistance are always in contact with
electrodes and the surfaces with higher surface resistance are always in
contact with each other, the high current density conditions which
normally attack the electrodes are significantly reduced in the region of
the electrodes while remaining high at the faying surface where the
welding takes place.
Further features and advantages of the invention will be apparent from the
detailed description hereinbelow set forth, together with the accompanying
drawings.
BRIEF DESCRIPTION OF THE DRAWINGS
FIG. 1 is a schematic view of an exemplary arrangement for spot welding
aluminum sheet members, in illustration of the method of the invention;
and
FIG. 2 is a graph comparing the results of Examples 1 and 2 set forth below
.
DETAILED DESCRIPTION
Referring first to FIG. 1, there is shown an arrangement for joining, by
spot-welding, two aluminum sheet members 10 and 11 (viewed edge-on),
utilizing a pair of welding electrodes 12 and 14. Sheet 10 has a first
major surface 16 in contact with the electrode 12, and a second major
surface 18; sheet 11 has a first major surface 20 in contact with the
electrode 14, and a second major surface 22 in contact with the major
surface 18 of sheet 10. The surfaces 18 and 22 are the faying surfaces of
the sheets; i.e. welding occurs at a locality 24, between the electrodes,
at which these latter surfaces are in contact with each other.
In an illustrative embodiment of the method of the invention, the two sheet
members 10 and 11 initially have a non-uniform mill finish oxide layer on
each of their major surfaces. The first step of the method is a treatment
of at least the portions of the sheet members to be welded, for effecting
removal of the non-uniform mill finish oxide layer from both major
surfaces of each of those sheet portions. Next follows the step of
providing a very thin oxide layer on the surfaces 16 and 20 of the two
sheet members, and a thicker oxide layer on the faying surfaces 18 and 22
of the sheet members, i.e. after the removal of the mill finish, thereby
creating a differential in oxide thickness between the two major surfaces
of each sheet member.
For welding, the sheet members 10 and 11 are now brought into
resistance-joining relationship and interposed between welding electrodes,
with the sheet member surfaces 16 and 20 bearing the very thin oxide
layers situated to contact the welding electrodes, and the faying surfaces
18 and 20 with their thicker oxide layers brought into contact with each
other, as shown. The electrodes 12 and 14 are brought into forced contact
with the sheet member thus disposed, and sufficient electric current is
passed between the electrodes to locally fuse the sheet members together
in the region 24 and provide a resistance-welded joint.
The differential in oxide thickness may be chemically produced and is
preferably created by a selective anodization treatment. According to one
technique, after the aluminum sheet surfaces have been cleaned, a natural
oxide layer is allowed to form on both cleaned surfaces. Then, one of
these surfaces with a natural oxide layer is subjected to anodization to
form a thicker oxide layer. The surface with the natural oxide layer which
is not being anodized may be protected during the anodization by means of
a protective electroplating layer, although it is also possible to
selectively anodize only one surface without using the protective layer.
The protective layer is typically in the form of a tape which serves as an
electrical insulator and also protects the surface against chemical attack
by the solution.
Alternatively, both cleaned surfaces may be subjected to anodization with
one surface being subjected to a very light anodization to form a thin
oxide layer and the other surface being subjected to a heavier anodization
to form a thicker oxide layer.
Using the above techniques, the thin oxide layer preferably has a thickness
of between about 20 and 200 .ANG. and the thicker oxide layer preferably
has a thickness of between about 110 and 1500 .ANG.. This results in a
differential in oxide thickness in the range of about 90 to 1480 .ANG.. It
is particularly preferred to have an oxide thickness differential in the
range of about 150 to 600 .ANG., with the optimum being in the range of
300 to 400 .ANG..
Typical of the aluminum sheet to which this invention applies are alloys
having the AA (Aluminum Association) designations 2036, X2038, 3004, 5052,
5182, 5454, 6009, 6010 and X6111.
The invention also relates to a welding process for the above sheets. Thus,
the sheets are brought into resistance joining relationships with the very
thin oxide layer situated to contact the welding electrodes. Then, the
electrodes are brought into forced contact with the sheets and sufficient
electric current is passed between the electrodes to locally fuse the
sheets (at the faying surface) and provide a resistance welded joint.
Certain preferred embodimemts of the present invention are illustrated by
the following examples.
EXAMPLE 1
A. Cleaning of Aluminum
A series of sample strips measuring 25 by 500 mm were prepared from 0.9 mm
thick sheeting of aluminum alloy AA-6010-T4. The strips were subjected to
vapor degreasing and then cleaned in NaOH solution at a temperature
between 65.degree. and 71.degree. C. for 25 to 35 seconds. Thereafter, the
strips were rinsed in 50% HNO.sub.3 solution at a temperature in the range
of 19.degree.-25.degree. C. for 15-25 sec. Next the strips were rinsed in
continuously flowing deionized cold water and then dried using forced air.
B. Surface Protection
One surface of each strip was covered using electroplating
pressure-sensitive tape, such as 3M No. 484 or a No. C-320 tape available
from Arno Adhesive Tapes Inc.
C. Anodization
The exposed surfaces of the strips were anodized in 13-15 wt. % H.sub.2
SO.sub.4 solution at a temperature in the range of 19.degree.-21.degree.
C. by passing a current for preset times of 2, 5, 10, 15 and 30 seconds to
a current density equivalent to 15 amps/ft.sup.2. Thereafter, the strips
were rinsed in flowing deionized cold water for a period of 30 seconds to
2 minutes and then dried by forced air.
The oxide thickness after each anodizing treatment was determined using the
ESCA technique from three randomly selected samples. In every case oxide
thickness measurements were made concurrently with surface resistance
measurements.
The surface resistance measurements were taken with a Digital Micro Ohmeter
(DMO) 6800 600. Two strips were placed at 90.degree. angle to each other
and held under a force of 3114N by a pair of 76 mm radiused electrodes.
The same squeezing force and type of electrodes were used to make the
welds. Ten readings were taken for each pair of strips for a minimum of
500 readings for a given surface treatment. Using point electric probes,
readings were taken at about 25 mm from the point of electrode contact.
D. Welding Tests
Welds were made with a 150 kVA single phase AC pedal type resistance spot
welding machine. The welding schedule used for the tests is given in Table
1. Each test was initiated by adjusting the % heat to produce a setup
average button diameter of 4.3 mm. A Current Analyzer, Duffers Associates
model 290, was used to measure the RMS current which varied between 22-25
kA depending on the surface condition of the strips being tested. The
welding was conducted using class II electrodes with a radius of 76 mm and
a diameter of 16 mm.
TABLE 1
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WELDING SCHEDULE USED
THROUGHOUT THE TESTS
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Squeeze 91 cycles
Weld: 4 cycles
Hold: 60 cycles
Off: 60 cycles
Tip force: 3114 N
Water flow: 4 1/min
Current: 22-25 kA (RMS) depending on
surface conditions.
% Heat: 62-74
Transformer Tap: Ser. 3
Set up average diameter:
4.32 mm
Strip size: 25 .times. 500 mm
Electrodes: class II radiused
16 mm dia., 75 mm radius
Weld spacing: 25 mm
Welding rate: 17/min
Strip feed: manual
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The quality of the welds was monitored by assessing the following
parameters for every 10 strips (about 170 welds). These parameters were
measured to the procedure specified by the Aluminum Association:
(a) shear strength
(b) button diameter
(c) surface indentation
(d) peel test
The electrode life was defined by the number of acceptable welds made (by
adhering to the specified failure criteria) with a given set of electrodes
without electrode dressing and with no changes in the preset welding
parameters. The test was considered concluded when any of the following
conditions were met:
(1) one or more buttons failed to peel for two consecutive peel tests (5
welds/peel test),
(2) the average button diameter was below the minimum value given in the
Aluminum Association (AA) T-10 document,
(3) the average of five single spot shear strength samples was below the
minimum value given in the AA T-10 documemt,
(4) a hole was blown in the sheet during welding;
(5) the electrodes pulled a plug out of the sheet.
Metallographic examination was also carried out on the electrodes tip
before and after welding and on the weld microstructure as the tests
progressed to assess the extent and mode of failure of the electrodes.
The overall results, as a function of the experimental conditions, are
summarized in Table 2.
TABLE 2
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SUMMARY RESULTS OF RESISTANCE SPOT WELDING TESTS
WITH ANODIZATION OF ONE SURFACE
Differential Values Electrode/
Oxide Thickness*
Resistance**
Oxide Faying Sheet
Cu/Al
Al/Al
Cu/Al
Al/Al
Thickness
Resistance
Surface Surface No. of
(.ANG.)
(.ANG.)
(.mu..OMEGA.)
(10.sup.3 .mu..OMEGA.)
(.ANG.)
(10.sup.3 .mu..OMEGA.)
Condition
Condition
Welds***
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N/A N/A 160 20 0 19.84 Mill Finish
Mill Finish
519
20 20 40 0.6 0 0.56 Caustic Cleaned
Caustic Cleaned
1286
20 165 40 29 145 28.96 Anodized-2 sec
Caustic Cleaned
2020
20 352 40 49 332 48.96 Anodized-5 sec
Caustic Cleaned
2722
20 557 40 149 537 148.96
Anodized-10 sec
Caustic Cleaned
2527
20 656 40 171 636 170.96
Anodized-15 sec
Caustic Cleaned
1947
20 1300 40 336 1280 335.96
Anodized-30 sec
Caustic Cleaned
1509
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Cu/Al = electrode/sheet interface.
Al/Al = faying interface.
*Mean thickness is based on 3 readings
**Mean resistance is based on 500 readings
***Number of welds is based on one test.
For mill finish surfaces, the resistance at the electrode/sheet interface
varied from 50 .mu..OMEGA. to 3,400 .mu..OMEGA. the mean value being 276
.mu..OMEGA.. Following caustic cleaning, the variation was reduced to
between 10 and 200 .mu..OMEGA. and the mean lowered to 31 .mu..OMEGA..
For mill finish surfaces, the resistance at the faying interface varied
from 500 .mu..OMEGA. to 100,000 .mu..OMEGA. with a mean value of 20,000
.mu..OMEGA.. After caustic cleaning, the resistance was reduced to between
10 and 1,300 .mu..OMEGA. and the mean was lowered to 600 .mu..OMEGA..
EXAMPLE 2
In order to demonstrate the advantages of anodizing to create a
differential in oxide thickness, a comparative study was made.
Using the same procedures as in Example 1, samples of AA2036-T4 having a
thickness of 0.036" were anodized equally on both surfaces for time
periods ranging up to about 16 seconds. The anodized samples were then
welded by the same technique as in Example 1 and the number of welds was
determined. The results for Example 1 and Example 2 are compared in FIG.
1. It will be seen that in welding samples anodized equally on both sides,
the number of welds peaked at about 1400 and then dropped off very
quickly. On the other hand, in welding the samples of this invention with
the differential in oxide thickness, the number of welds rose to a peak of
2722 welds and then decreased quite gradually. Thus, it will be seen that
the pretreating method of this invention is almost twice as effective as
anodizing equally on both sides in increasing the number of welds per
electrode.
EXAMPLE 3
The same aluminum alloy strips used in Example 1 were caustic cleaned and
prepared in the same manner as that described in part A of Example 1.
These prepared surfaces were then anodized in the same manner as Example 1
with both sides of the sample being anodized equally for one second and
then rinsed and dried as described hereinbefore.
Thereafter, one surface was protected by an electroplating tape and the
exposed surface was again anodized for preset times of 3, 6, 9, 14, 19 and
29 seconds, then rinsed and dried as described hereinbefore.
The samples thus prepared were subjected to welding tests using the same
procedure as part D of Example 1. However, rather than continuing the
welds to failure, 60-66 welds were made with each sample. The welds thus
obtained were subjected to the peel test to obtain a determination of
defective welds. The results obtained are shown in Table 3 below:
TABLE 3
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SUMMARY RESULTS OF RESISTANCE SPOT WELDING TESTS
WITH ANODIZATION OF BOTH SURFACES
Anodization
Differential Values Percentage
Total
Time Oxide Surface
Button
Shear
of Number
(seconds)
Thickness
Resistance
Diameter
Strength
Defective
of
Cu/Al
Al/Al.sup.(1)
(.ANG.)
(10.sup.3 .mu..OMEGA.)
(inches)
(lbs/spot)
Welds Welds
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1 4 98 11 0.191
423 13 66
1 7 258 27 0.185
396 3 60
1 10 333 34 0.194
451 8 62
1 15 567 52 0.193
456 14 63
1 20 868 48 0.205
459 32 62
1 25 1123 47 0.201
478 33 66
1 30 1463 145 0.204
448 39 63
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.sup.(1) This time includes the initial 1second anodization given to both
surfaces.
It will be seen from the above table that optimum results were obtained in
terms of strong welded joints with oxide thickness differentials of 258
and 333 .ANG.. Thus, it will be seen that at the preferred thickness
differentials for maximum electrode life, there is also an optimization in
terms of quality of the welded joints.
It will be obvious that various modifications and improvements can be made
to the invention without departing from the spirit thereof and the scope
of the appended claims.
* * * * *
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Description  |
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