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A
erospacecoatingsare the first formof protectionagainst
the extreme environments an aircraft is subjected to.
Therefore, a coating must maintain high performance
properties throughout its lifetime. A great deal of research is
taking place into the replacement of hexavalent chromium—
Cr(VI)—a carcinogen currently used within primers and as part
of the pretreatment for a coating substrate due to its highly
effective anticorrosive and adhesive properties. To minimize
exposure to Cr(VI), preventing topcoat degradation should
also be a priority. Measures taken to prolong topcoat lifetime
or identify when the topcoat is failing will aid in reducing the
risks imposed by Cr(VI). However, two main issues must first
be resolved. One is determining the degradation mechanism
at themolecular scale. This is essential in order to establish the
topcoat’s failure point. The other is monitoring the topcoat in
order to establish where the coating is in its functional lifetime
and whether measures should be put in place to aid function-
ality. This kindof large-scalemonitoring requires a simple, cost
effective, and nondestructive technique.
First, inorder tounderstand thedegradationphenomena,
it is essential to examine the interface between the topcoat
and the environment. Themain causes of degradation include
high humidity, extreme temperatures, and UV radiation, which
is an acute cause. Many well established testing methods exist
within the coatings industry as ameans of comparing coatings
and meeting application requirements. These include natural
exposure and accelerated testing methods such as exposure
within a QUV chamber, prohesion chamber, and temperature
cycling. However, thesemethods often requiremonths or even
years of exposure to observe degradative effects. Further, as an
aircraft crosses the tropopause the level of ozone it is exposed
to rises significantly, an issue seldom addressed in the liter-
ature but that could play a vital role in determining an aero-
space coating’s failure mechanism. With this in mind, a novel
coating test method called HyperTest was developed, which
combines UV and ozone—a technique traditionally used for
secondary electronmicroscopy sample preparation.
The device requires the sample to be placed within a vac-
uum chamber and then uses a UV lamp light source at wave-
lengths (λ) of 185 and 254 nm to irradiate the topcoat surface.
The long wavelength is also able to photodissociatemolecular
oxygen into atomic oxygen, which is then able to form ozone.
The short wavelength penetrates the coating surface creating
HYPERACCELERATED DEGRADATION OF AN
AEROSPACE COATING
A promising method of testing aerospace coatings could help minimize exposure
to hexavalent chromium by understanding coating lifecycles.
Taraneh Bozorgzad Moghim, Marie-Laure Abel, and John F. Watts
University of Surrey, UK
excited molecules or free radicals, which are able to react with
ozone to form simple volatile molecules that are released by
the vacuum (Fig. 1). Through analysis of the topcoat of the
UV/ozone exposed samples, as detailed here, the HyperTest
method proves to be hyperaccelerating when compared to
samples treated with UV within a QUV chamber.
ANALYZING COATING FAILURES
Surface sensitive analytical techniques are imperative for
understandingdegradationphenomena.Determiningchanges
occurring to the topcoat surface, particularly during initial deg-
radation, can aid development of a degradation mechanism
and subsequently allow identification of the coating’s failure
point. The main analytical techniques applied in this research
include time of flight secondary ion mass spectrometry (ToF-
SIMS) and x-ray photoelectron spectroscopy (XPS), recorded
using a Theta Probe spectrometer (Fig. 2). ToF-SIMS provides a
significant level of elemental andmolecular detail of the upper
monolayer of the surface, enabling identification of degrada-
tion products. XPS is also a highly surface-sensitive technique,
offering chemical state information and enabling quantita-
tive analysis. XPS helps facilitate monitoring of degradative
changes, which occur as a function of UV and UV/ozone
exposure.
Fig. 1 —
Schematic detailing the functionality of the HyperTest
method using UV/ozone.