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Cadmium Substitution - garteur

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GARTEUR LIMITED<br />

compared with cadmium plating. Specimens with a configuration shown in figure F1 were<br />

stress corrosion tested to ASTM G44-75. In this test, the specimens were subjected to<br />

alternate immersion in 3.5% sodium chloride solution. One cycle in this standard<br />

includes 10 minutes in salt solution and fifty minutes drying in air. The total exposure<br />

time was 30 days.<br />

The notched tensile strength was determined on three specimens. Values of 2700, 2705<br />

and 2690 M Pa were achieved. For one set of stress corrosion specimens the notch was<br />

covered to 180 o by an aluminium casing. The reason for using this casing is to initiate<br />

galvanic corrosion and crevice corrosion. The specimens were then loaded to and held<br />

at 75% of the notched tensile strength. Each treatment was represented by three<br />

individual specimens The treatments tested were:-<br />

F.3 Results and discussion<br />

• Reference without protective coating<br />

• Porous cadmium plating<br />

• Zinc-nickel plating<br />

• Zinc-cobalt-iron plating<br />

• Sermetel<br />

• Electrodeposited aluminium<br />

• Delta-tone<br />

F.3.1<br />

Susceptibility to hydrogen embrittlement<br />

The results of slow bend tests conducted on a 35 NCD 16 steel (1800 MPa) are<br />

presented in figure F1. The results indicate that for the SermeTel coatings, there is<br />

minimal embrittlement due to plating. In the case of the electrodeposited aluminium<br />

some reduction is observed but this may be recovered by heat treating at 190 o C.<br />

One of the three electroplated zinc-nickel notched tensile specimens tested, failed within<br />

the 200 hours test period. In the second series of specimens tested, no failures occurred<br />

and it is considered that the electrodeposited zinc-nickel coating is non-embrittling.<br />

F.3.2<br />

Susceptibility to stress corrosion cracking<br />

In the sustained load tests, two specimens of three of those protected with zinc-cobaltiron<br />

and those protected with Delta-tone coating in the test set using the aluminium<br />

casings, failed within two days. Sacrificial coatings may add to the risk of post plating<br />

embrittlement. SAAB uses ZnCoFe plating to 1250 M Pa, a strength level considered to<br />

be safe. The specimens used in this investigation were hardened to 1400 M Pa.<br />

In the second test set, where no casing was used , two specimens of three with Deltatone<br />

coating failed within two days. All other specimens remained unbroken after 30<br />

days.<br />

Previous research undertaken by SAAB [F2] compared the performance of IVD<br />

aluminium and electrodeposited cadmum coatings applied to notched tensile specimens<br />

machined from either a 1366 Ni-Cr-Mo steel or a 1745 precipitation hardening stainless<br />

steel. As in the current research programme, the specimens were loaded to 75% of the<br />

notched tensile strength. From the tests undertaken, there was no indication that<br />

aluminium-coated specimens have a higher tendency to delayed fracture in a corrosive<br />

environment than cadmium coated ones.<br />

F.4 Conclusions<br />

Page 86<br />

GARTEUR SM/AG17 TP128

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