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Evaluation of hastelloy N alloys after nine years exposure to both a ...

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.<br />

-<br />

19<br />

Air Oxidation<br />

Figure 22 shows 1 micrographs <strong>of</strong> the outside <strong>of</strong> the tubing which had been exposed <strong>to</strong> air. The oxide<br />

layers on the outside <strong>of</strong> the loop tubing underneath heaters are shown in Figs. 23-25, and the oxide layers<br />

on the loop tubing just exposed <strong>to</strong> air are shown in Figs. 26-28. Figures 23-25 (A, B, C, Fig. 22) include<br />

the hot leg and lower crossover, while Figs. 26-28 (D, E, F, Fig. 22) include the upper crossover and the<br />

cold leg. The salt temperatures in these areas were 560 <strong>to</strong> 660°C. The outside surfaces underneath heaters<br />

are appreciably hotter than the salt because <strong>of</strong> the temperature gradient across the salt film at the inside<br />

surface. This temperature difference mainly results from the fact that we have laminar flow. Because <strong>of</strong> the<br />

e<br />

\<br />

SURGE TANK<br />

-HASTELLOI N WELDED TO<br />

HASTELLOI N-2% ND WITH<br />

WASTELLOY N-2% Nb VELD ROO<br />

-WSlELLOVN-Z%Nb TUBING<br />

WnEUOY N-2ZND WELDfO WITH<br />

HASTELWY N-2ZWD WELD MH)<br />

i<br />

Schematic Vlcw <strong>of</strong> Thcr aI Convection Loop.<br />

Y<br />

Y-112589<br />

Pi. 22. Micrographs <strong>of</strong> the outside <strong>of</strong> tubing <strong>of</strong> loop 1255, exposed <strong>to</strong> air at 560-700°C for 9.2 ye=. As polished,<br />

W SOOX. Reduced 1690.

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