In
January of 2000, a U.S. manufacturer faced an interesting situation. One of the
company's new parts required finishing; however, one of the finishing operations
specified was an expensive prefinish. Eliminating the prefinish operation would
save $2,000,000 a year, but could it find an appropriate substitute?
While on the surface this
seems like a fairly simple request, it meant the development of a new coating
from the ground up. So, the company approached MacDermid Inc., giving it the following
directives concerning the finish characteristics.
To begin with, the finish
had to have outstanding adhesion characteristics on aluminum, good wear, lubricity
and corrosion protection, as well as specific hardness properties. Additionally,
this new plating system had to be free of all toxic metals, such as chromium,
nickel or cadmium. The application of the finish had to lend itself to process
automation, and, most importantly, it had to be cost-effective. With these criteria
in mind, the process engineers put together a list of potential finishes.
After weighing all the
various alternatives, it was decided that a tin-cobalt alloy finish had the highest
potential. Developed in Europe, this specialized plating process, Cromvert, produces
a consistently uniform, tin-cobalt alloy finish. Its most common use is as a replacement
for hexavalent chromium in decorative applications; however, it had not been tried
before as a functional finish. The finish was selected because it combined the
lubricity characteristics of tin and the hardness of cobalt. Additionally, since
it is applied as a very thin coating, the process is cost-effective. (See Table
I)
The process produces an
intermetallic deposit consisting of 78% cobalt and 22% tin. The process can be
used in barrel applications.
Once a finish had been
selected, the project was moved to a pilot plating lab where sample parts could
be run to evaluate the coating and design the proper process cycle. Countless
parts were run, cycles modified and sample parts generated. Care was taken so
that actual plating shop conditions were duplicated, in order to uncover any pitfalls.
Once the process cycle was finalized, sample parts were generated for testing.
 |
| New line
at Techmetals sequences parts through the tin-cobalt alloy plating process. This
finish is used as a replacement for hexavalent chromium. The line produces 15,000
parts per day and has saved the customers $2 million.
|
The testing process was
extensive and rigorous. Adhesion, lubricity and wear resistance testing were performed
both here and overseas. (See Table II) With some minor process adjustments, all
test criteria were met or exceeded.
The next step was to locate
a facility to do the plating. As this was a newly developed process, there weren't
any applicators currently doing this work. This would mean that the plating shop
would have to either install a new line or modify an existing one. Either way,
it would require a significant financial commitment on the part of the plater.
A nationwide search was
made to locate a potential applicator. Audits were performed and candidates were
rated on technical ability, laboratory capabilities, quality control and assurance
programs, plant flexibility and overall plating knowledge. Of the dozens of potential
shops evaluated, Techmetals Inc. (Dayton, OH) received the highest score and was
chosen as the preferred applicator.
Now time was of the essence.
Months of evaluating different finishes had gone by, and the part manufacturer
was in danger of not meeting production demands. In a matter of weeks, Techmetals
had to put together an entire plating line capable of producing 15,000 parts per
day.
|
TABLE
I - Cromvet Process Characterists vs. Conventional Alternatives
|
| Parameters |
Cromvet
|
Hex Chrome
|
Tri Chrome
|
| Plating
Speed |
0.18 mm/min
@
0.5 Adm-2 (5 asf)
|
0.15 mm/min
@
12.0 Adm-2 (120 asf)
|
0.075 mm/min
@
5.0 Adm-2 (50 asf)
|
| Current
Density |
0.3-0.5
Adm-2
(3-5 asf)
|
10-15 Adm-2
(100-150 asf)
|
5-10 Adm-2
(50-100 asf)
|
| Voltage
|
2.5-3.0
V
|
16 V
|
12 V
|
| Temperature |
45C (113F)
|
40C (104F)
|
55C (130F)
|
| Hardness |
400-450
HV
|
850-1,100
HV
|
800-1,000
HV
|
Process
engineers from both companies met daily. The supplier provided the process cycle
and chemical know-how, while Techmetals had the expertise to take the project
from a laboratory setting to full production. Within two weeks of winning the
contract, Techmetals was up and running sample parts.
The first set of test parts
performed exceptionally well. All the performance criteria were met, with one
exception. One specific application required a minimum plating thickness be applied
that exceeded what could be done with the new process. This was a major hurdle
to clear, as there simply wasn't time to evaluate new finishes in the laboratory.
A solution had to be found to this problem on a production scale before sales
demands were interrupted.
Once again, engineers from
the two companies met and considered various alternatives. Plating a higher thickness
wasn't a viable alternative, so an alternate base coating would be required. All
the same wear, corrosion and environmental considerations had to be met.
|
TABLE
II - Cromvet Wear Resistance Properties
|
| The
test methods used conform to ASTM B 117/537. The abrasion test used is a modified
version of ASTM D 968 (ASTM D 968-8) using 20 liters of sand instead of 100. The
two ASTM specifications are partial fulfillment of the requirements of SAE Aerospace
Standard AS4984. |
| AL
ID No. |
SOT
ID No.
|
Original
Weight (g)
|
End
Weight (g)
|
Weight
Loss (g)
|
Liters
of Sand
|
Comments
|
| P99-1431-1 |
47
|
28.6979
|
28.6961
|
0.0018
|
20
|
Ni/Alloy
|
| P99-1431-2 |
45
|
28.0147
|
28.0129
|
0.0018
|
20
|
Ni/Alloy
|
| P99-1431-3 |
14
|
27.0298
|
27.0288
|
0.0010
|
20
|
Ni/Cr
|
| P99-1431-4 |
11
|
27.4001
|
27.4000
|
0.0001
|
20
|
Ni/Alloy
|
| P99-1431-5 |
40
|
28.8190
|
28.8155
|
0.0005
|
20
|
Ni/Alloy
|
| P99-1431-6 |
48
|
28.3729
|
28.3726
|
0.0003
|
20
|
Ni/Alloy
|
| P99-1431-7 |
32
|
27.3022
|
27.3007
|
0.0015
|
20
|
Ni/Cr
|
| P99-1431-8 |
10
|
27.6127
|
27.6112
|
0.0015
|
20
|
Ni/Alloy
|
| P99-1431-9 |
25
|
23.5488
|
23.5485
|
0.0003
|
20
|
Ni/Alloy
|
| P99-1431-10 |
20
|
27.4368
|
27.4360
|
0.0008
|
20
|
Ni/Alloy
|
| P99-1431-11 |
22
|
22.8590
|
27.8583
|
0.0007
|
20
|
Ni/Cr
|
| P99-1431-12 |
21
|
25.5163
|
23.5160
|
0.0003
|
20
|
Ni/Alloy
|
| P99-1431-13 |
26
|
26.3119
|
26.3115
|
0.0004
|
20
|
Ni/Cr
|
| P99-1431-14 |
24
|
26.4870
|
26.4861
|
0.0009
|
20
|
Ni/Cr
|
| P99-1431-15 |
49
|
27.8553
|
27.8548
|
0.0005
|
20
|
Ni/Alloy
|
| Ni/Cr
X = 0.9 mg |
s
= 0.0004 |
|
|
|
|
| Ni/Sn/Co
X = 0.8 mg |
s
= 0.0007 |
|
|
|
|
After weighing all the
possibilities, a base coating was selected and tested. The results were positive,
and the project was back on track. This meant, however, that Techmetals faced
a new challenge; having to retrofit a new process tank into an already existing
line. This is a good example of why plant flexibility was so important in the
initial plant audits.
The companies are happy
to report that the line is now up and running full production. It is in operation
5 days per week producing 15,000 parts per day. The estimated cost savings to
the part manufacturer is in excess of $2,000,000, and the use of hazardous metals
has been entirely eliminated. This newly installed line has open capacity to process
an additional 1,000 ft2/hr of aluminum parts in bright nickel, tin and Cromvet
to meet future customer needs for either engineering or decorative applications.
Through the cooperation
of the companies, a cost-effective, environmentally friendly, wear-resistant coating
was developed and put into production to everyone's mutual satisfaction. It is
an excellent example of how teamwork and shared knowledge can be used to solve
industry problems.