Materials Science Forum
Vols. 532-533
Vols. 532-533
Materials Science Forum
Vols. 530-531
Vols. 530-531
Materials Science Forum
Vols. 527-529
Vols. 527-529
Materials Science Forum
Vol. 526
Vol. 526
Materials Science Forum
Vols. 524-525
Vols. 524-525
Materials Science Forum
Vols. 522-523
Vols. 522-523
Materials Science Forum
Vols. 519-521
Vols. 519-521
Materials Science Forum
Vol. 518
Vol. 518
Materials Science Forum
Vol. 517
Vol. 517
Materials Science Forum
Vols. 514-516
Vols. 514-516
Materials Science Forum
Vol. 513
Vol. 513
Materials Science Forum
Vol. 512
Vol. 512
Materials Science Forum
Vols. 510-511
Vols. 510-511
Materials Science Forum Vols. 519-521
Paper Title Page
Abstract: AA5182 (Al-4.5 wt% Mg) can become susceptible to intergranular corrosion (IGC) with
time at moderately elevated service temperatures owing to precipitation of Mg-rich β-phase at grain
boundaries, which can lead to stress corrosion cracking (SCC). The IGC and SCC susceptibility of
AA5182 was found to depend strongly on sensitisation heat treatments. AFM and TEM studies
demonstrated that the degree of precipitation and thus susceptibility to attack for a boundary can be
related to its crystallographic misorientation. Low angle boundaries (<20°) are most resistant to
attack as they do not show β-phase precipitation. However, higher angle boundaries show highly
variable precipitation and corrosion susceptibility: critical factors are the grain boundary plane and
precipitate/matrix crystallographic relationship.
641
Abstract: Over the past ten years a detailed understanding of the dominant factors controlling the corrosion
susceptibility of painted aluminium alloy sheet used for architectural and automotive applications has been
developed. Work carried out in this field will be reviewed and the different modes of cosmetic corrosion that
can occur-, the mechanisms of surface activation, and the role of different thermo-mechanical processing
steps on controlling corrosion susceptibility for different alloy systems, including Al-Mn, Al-Mg and Al-Mg-
Si-(Cu) will be discussed. The critical role of chemical or electro-chemical cleaning prior to pre-treatment
and coating will be highlighted and prospects for meaningful accelerated testing will be discussed.
647
Abstract: Applicability of the wedge test and the accompanying fracture mechanical data analysis,
commonly used for testing of adhesively bonded joints, was inestigated in an attempt to
develop a quantitative laboratory test for evaluating paint adhesion on aluminium. The test
was further used, along with a relatively better accepted laboratory test for filiform corrosion
of painted aluminium to study the mutual effects of corrosion and adhesion of various pretreatments
and paint systems on extruded AA 6082 T6 aluminium alloy. Pretreatments used
were commercial processes for deoxidising, chromating, hot AC anodising and Ti/Zr
conversion coating. The paints were polyester TGIC and epoxy DICY, both pigmented
commercial products. In particular, the compatibility of pretreatment-paint combinations were
investigated The wedge test methodology and sample preparation developed proved to be a
satisfactory approach for quantitative evaluation of pretreatment-paint combinations for
aluminium. Ti/Zr treatment gave exceptionally good adhesion and corrosion results when
coated with polyester. Epoxy coated Ti/Zr bars failed completely. However, hot AC
anodising, although in general significantly more robust than Ti/Zr, was more compatible
with the polyester than polyester coating. With the advent of chromate-free pre-treatments,
the need to establish the compatibility of the modified aluminium surface and applied organic
coating was demonstrated.
655
Abstract: Several heterocyclic organic corrosion inhibitors that contain ionazible functional group
were encapsulated into nano-structural hybrid organo-silicate coating to improve its corrosion
protection performance on aluminum alloy 2024-T3 substrate. When the coating is formed on the
substrate surface, it serves simultaneously as protective barrier and as a reservoir for leachable
corrosion inhibitor that is stored and released through the mechanism of reversible ionic interaction
with the matrix material. The efficiency of active corrosion protection for these coating systems
was examined by electrochemical methods including potentiodynamic polarization (PDS) and
electrochemical impedance spectroscopy (EIS). The effects of chemical structure and the loading
concentration of the inhibitor within the coating were determined.
661
Abstract: Intergranular corrosion (IGC) of model alloys in the 6000-series, with and without 0.2 wt% Cu,
was studied using an accelerated corrosion test (BS ISO 11846 B), FE-SEM and FE-TEM. Low Cu
alloys (0.02wt%) did not exhibit IGC even though they contained excess Si. The high-Cu, naturally
aged material (T4) was susceptible to severe superficial etching. In the underaged state (below
peak strength), the Cu-containing material was highly susceptible to IGC. Materials aged to peak
strength (T6) or overaged were only slightly susceptible to IGC, with localized, shallow attacks.
FE-TEM investigation of the underaged material revealed scattered, small AlMgSiCu-type
precipitates, as well as a Cu-enriched film along the grain boundaries. The overaged material
showed more extensive, coarse grain boundary precipitation. However, the Cu-enriched film was
still present at localized sites. The reduced susceptibility to IGC upon artificial ageing was
attributed to breaking of the continuity of the grain boundary film. The possible role of matrix
precipitation is also discussed.
667
Abstract: High temperature heat treatment of aluminium alloys causes surface enrichment of the trace
elements in Group IIIA - VA, specifically the low melting point elements Pb, Bi, In and Sn.
The phenomenon has practical significance in promoting certain types of localised corrosion,
such as galvanic and filiform corrosion, while mitigating other types, such as pitting
corrosion of the bare surface. The purpose of this paper is to investigate the surface
enrichment and microstructure of indium relative to the available data for Pb. Model binary
AlIn alloys, containing 20-1000 ppm of In, were used after heat treatment at various
temperatures. In addition to electrochemical investigations, the microstructures were
characterised by field emission scanning electron microscopy (FEG SEM) and field emission
transmission electron microscopy (FEG TEM). Heat treatment at temperatures as low as
300°C gave significant segregation of In as opposed to 600°C for Pb. As a result of this and
yet unresolved oxide film breakdown mechanism on aluminium, In was significantly more
effective than Pb in anodically activating aluminium. These results suggest the possibility
that significant activation earlier observed on certain commercial alloys as a result of low
temperature heat treatment may be due to the trace elements In.
673
Abstract: Scanning Kelvin Probe (SKP) potentiometry is used to systematically investigate the
effect of surface abrasion and subsequent heat-treatment on the open-circuit potential in humid air
of the AA6016 surface. SKP is also used to follow the kinetics of filiform corrosion and to
determine characteristic potentials associated with the electrolyte-filled filiform head and dry
filiform tail. It is shown that simply abrading with 180 grit SiC produces a surface potential up to
0.5V lower than the bulk. When the abraded sample is overcoated with a 30 micron layer of PVB
(polyvinyl butyral) and exposed to HCl a fast, superficial filiform corrosion (FFC) is observed in
which metal loss is limited to the thickness of the surface layer. Filiform head OCP values are
similar to that of the surface layer, whereas filiform tail OCP values are similar to the bulk. A
mechanism is proposed in which the ultra-fine grain structure of the surface layer produces an
anodic activation and the potential difference between the surface layer and the bulk provides and
increased thermodynamic driving force for corrosion. For post-abrasion heat treatment temperatures
up to 350°C the fast filiform process is followed by a slower, deeper form of FFC.
679
Abstract: The presence of a heavily deformed and corrosion susceptible surface/near-surface region
on rolled aluminium alloy has been amongst the most important problems which the aluminium
manufacturers are dealing with. While primarily the composition of the alloying elements and the
thermo-mechanical treatment play an important role in determining surface activation, the
importance of several other secondary parameters cannot be ignored. This paper tries to identify the
impact of several factors, associated with sheet metal production, on the corrosion behaviour e.g. (a)
type of the cast bar fed into the hot rolling mill, whether scalped or not scalped, (b) importance of
homogenisation and in-line heat treatment, in relation to pre-existing understanding of surface
activation on AA3005, (c) effect of hot and cold rolling (d) effect of surface finish, etc. The alloy
under investigation was recycled AA5050, containing high Fe and Si as impurities, and used
commercially for architectural purpose, eg. window facades.
687
Abstract: It is generally considered that exfoliation corrosion is due to the build-up of corrosion products that
create a wedging stress that lifts up the surface grains. However, the exfoliation mechanism is still
under discussion: possible operating mechanisms include intergranular corrosion of in plane grain
boundaries accelerated by the wedging effect, or crack propagation by a “purely” stress corrosion
mechanism. The sensitivity to exfoliation corrosion of AA7449 in relation to the intergranular and
stress corrosion cracking sensitivity has been addressed in a program of controlled quenches
followed by thermal treatments. Our observations demonstrate that the quench rate has a strong
effect on intergranular corrosion and exfoliation corrosion sensitivity and in a lesser extent on stress
corrosion cracking. In the first moments of the EXCO test, the initiation of corrosion follows the
same trends as those revealed by the ASTM G110 test. We observe intergranular initiation for the
slow quench rate (~5°C/s) and pitting initiation for samples quenched between 50 to 500°C/s.
On the contrary, the final EXCO corrosion quotations do not seem to correlate with the
intergranular resistance but rather with SCC resistance.
693