



DIARY DATES
6th February 2012
New ICorr Level 2 Cathodic Protection Course More Info
6th February 2012
A-Z of Coatings Application More Info
6th February 2012
CPD The New Standards More Info
9th February 2012
London Branch Meeting More Info
20th February 2012
28th February 2012
Institute of Corrosion Technical Presentation More Info
8th March 2012
London Branch AGM and Meeting More Info
12th March 2012
Wellington Swimming Pool More Info
12th April 2012
London Branch Joint Meeting with NACE More Info
17th April 2012
Joint Marine Corrosion Forum (MCF) qand Institute of Corrosion Technical Presentation More Info
18th April 2012
Corrosion of Infrastructure More Info
26th April 2012
CED Working Day and Symposium on Microbial Corrosion More Info
12th May 2012
Corrosion Fatigue Developments More Info
Before we start just let me make a plug for the Correx conference taking place in Birmingham from Oct 27th - 29th (see other publicity in this issue). One of the sessions is on coatings and the other on CP, both areas dear to the heart of many (over half) our members and both of which get some coverage within this article. The conference is very reasonably priced and the CED workgroups hope to meet there.
Anyway in this months TT, I am returning to the topic of bimetallic corrosion, a subject area that constitutes the greatest proportion of the technical queries that I receive.
We will start by reminding ourselves how devastating this can be with an example of a gantry sign sent to me eighteen months ago by Rob Poulton and which I have already published in a article on aluminium.
This picture shows aluminium bars welded to aluminium matrix frame with plastic/pvc sheet on front of the sign attached with galvanised bolts. Not nice at all! But this months’s article has really been inspired by my listening recently to a couple of papers about use of powdered magnesium as a cathodically protecting pigment for aluminium at the Advances in Corrosion Protection by Organic Coatings Conference in Cambridge.
The story in a nutshell is that for protection of their aluminium alloys the American Air Force relied heavily on the use of chromate pigment and passivation treatment. Both very effective- but no longer allowed! So the group at North Dakota State University have been working on an alternative based on magnesium pigment dispersed in an epoxy binder. This has now has reached a state where it seems to work pretty well in the lab and is going to tried out on an actual aeroplane. It is the theory behind the use of this pigment that interests me.
Both talks used the term cathodic protection to describe the action of the magnesium (at least in the early stages of its operation- the potential does rise with time - see graph) This was based on the observation that the potential taken up by the system was below the galvanic potential taken up by the bare aluminium alloy (typically 2024 or 7075) in, say, 0.1M NaCl. Thus if the latter had a potential of say -0.6V (SHE), the potential of the system (coated with the magnesium containing paint) might be -1.0