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FIFTH CANADIAN CONFERENCE ON NONDESTRUCTIVE ... - IAEA

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2.2 Primary Factors<br />

- 209 -<br />

Computer simulation results verified that vectorial addition was valid for<br />

signals due to gap and wall thickness changes, thus allowing these effects to<br />

be studied independently. A number of sets of data were collected, each at a<br />

different fixed wall thickness and containing the response of the eddy current<br />

probe to a range of gap values. One such set is shown in Figure 4 where the<br />

non-linear response of the probe is evident. In order to relate these<br />

independent data sets and determine the effect of wall thickness changes, it<br />

is only necessary to determine the response of the probe to wall thickness at<br />

one fixed gap. This was done by performing a rotational scan on a pressure<br />

tube sample with a large wall thickness variation around the circumference and<br />

no calandria tube (infinite gap). The result, shown in Figure 5, was a good<br />

linear fit with a regression coefficient of 0.9887. The slope of this line<br />

was used to shift the sets of previously collected data so that they all<br />

referenced a common balance point at infinite gap and 5.0 mm wall thickness.<br />

Straight lines were fitted to the points of common gap with a great deal of<br />

success, the smallest regression coefficient being 0.9960. This overview,<br />

shown in Figure 6, formed the data base of the probe's response which was to<br />

be used during field inspections.<br />

2.3 Pressure Tube Resistivity<br />

The calculated complex plane response of the probe indicated that pressure<br />

tube resistivity could significantly influence the eddy current signal if<br />

large enough variations were encountered during the inspections. This<br />

possibility was explored by measuring the resistivity and wall thickness<br />

around the circumference of a pressure tube sample and then scanning the same<br />

section with the gap probe in order to compare both influences.<br />

The resistivity scan in Figure 7c shows a well defined change of about 1<br />

just after the 180° mark. Using Figure 3, it was calculated that a<br />

resistivity change of this magnitude should cause approximately the same<br />

effect in the Y component of the probe response as a 0.17 mm wall thickness<br />

change. Figure 7a shows that this is about half of the total wall thickness<br />

variation measured in the pressure tube sample. However, the response of the<br />

gap probe shown in Figure 7b does not agree with this prediction as the wall<br />

thickness influence was followed very closely with almost no sign of the<br />

resistivity influence.<br />

The apparent insensitivity of the probe to resistivity variations was<br />

encouraging for the immediate goal of the Pickering 1 and 2 inspections,<br />

however, further investigations are required for the long term development of<br />

the gap measurement system.<br />

2.4 Temperature<br />

The temperature sensitivity of the probe in its operating environment and in<br />

isolation are shown in Figures 8 and 9 respectively. The response in Figure 9<br />

is somewhat unexpected since send-receive probes are generally expected to be<br />

insensitive to temperature variations due to the small effect that variations<br />

in coil resistance have on the output signal. In this case the response is<br />

thought to be caused by a physical deformation of the probe and is currently<br />

under investigation. The linear response of -0.036V/°C obtained from the

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