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Cadmium Substitution - garteur

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GARTEUR LIMITED<br />

D.3 Results and discussion<br />

D.3.1<br />

D.3.1.1<br />

Accelerated corrosion tests<br />

Daimler Benz Airbus Aerospace<br />

The results of neutral salt tests are summarised in table D1. The blocks were inspected<br />

on a weekly basis for evidence of rusting on the bolt heads. Data presented in table D1<br />

indicate that the four substitute coatings examined were less prone to rusting under<br />

these conditions than the electrodeposited cadmium control. The most promising coating<br />

was the Delta-tone/Delta coat which showed no evidence of rusting during the exposure<br />

period.<br />

D.3.1.2<br />

Fokker<br />

Metallographic examination of the aluminium alloy blocks after testing showed that<br />

corrosive attack had occurred in the countersink when cadmium plated bolts were used.<br />

No evidence of corrosion was found in the countersinks when there was contact with<br />

zinc-nickel and zinc-cobalt-iron plated bolts.<br />

D.3.2<br />

Natural exposure trials<br />

During the 10 month exposure period at the Schiphol test site no evidence of corrosion<br />

attack was observed.<br />

D.3.3<br />

Electrochemical measurements<br />

In the first part of this study, the current flow between different coatings and two<br />

aerospace aluminium alloys was monitored. In all cases, some galvanic current flow was<br />

detected indicating that the coatings were interacting galvanically with the two alloys.<br />

Curves showing the variation in galvanic corrosion current with time for each of the<br />

coatings coupled to 2014-T6 and 7075-T6 aluminium alloys are reproduced in figures D4<br />

and D5 respectively. In most cases, the current was found to flow from the coating to the<br />

aluminium alloys. The exceptions were electrodeposited zinc-nickel alloy coating and<br />

Delta-tone where current reversal effects were seen after coupling periods of over 100<br />

hours. Tables D3 and D4 give the average current densities recorded for each of the<br />

coatings. In general, higher galvanic current values were observed for the more active<br />

zinc base coatings than the less active aluminium base coatings.<br />

The coupling of a metal coating with an aluminium alloy can cause corrosion of the<br />

aluminium alloy even if the coating is a sacrificial one. This occurs as a result of the build<br />

up of alkaline conditions on the aluminium alloy surface, which unlike in the case of steel<br />

which is stable at high pHs, can lead to damaging pit attack. In the second part of the<br />

work, therefore, the effect of galvanic coupling on the corrosion rate of the aluminium<br />

alloys was determined.<br />

The galvanic corrosion rate of the aluminium alloy, R g was calculated from the following<br />

expression,<br />

R g = R a - R o --------------------- (D1)<br />

where R o is the self corrosion rate and R a is the total corrosion rate of the aluminium<br />

alloy.<br />

The corrosion rates, R g, , of the two aluminium alloys were slightly increased by coupling<br />

with cadmium plating as indicated in tables D3 and D4.<br />

Page 72<br />

GARTEUR SM/AG17 TP128

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