ORNL-1771 - Oak Ridge National Laboratory
ORNL-1771 - Oak Ridge National Laboratory
ORNL-1771 - Oak Ridge National Laboratory
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ANP QUARrERLY PROGRfSS REPORT<br />
3. E TAL ~~A~~~~ ~~~~~~~<br />
The emphasis in the engineering work has shifted<br />
to research and component development for the<br />
CFRE and for in-pile loops, since most of the<br />
preoperational ARE tests have been completed.<br />
Two types of pumps have been developed for in-<br />
pile loop use:. The vertical-shaft centrifugal sump<br />
pump, which would be installed outside the reactor<br />
shield and thus would require auxiliary shielding,<br />
is now being fabricated iii sufficient quantity to<br />
meet the demands of the in-pile loop program and<br />
the f orced-c i rcu lot ion corros i on testing program.<br />
The small (4-in.-OD), air-driven, horizontal-shaft<br />
sump pump being developed for insertion in a<br />
reactor beam hole was tested with NaF-ZrF, at<br />
1350'F. Some difficulfy was encountered with<br />
initial priming, but operation was otherwise satis-<br />
factory. A new, small pump that hos the required<br />
small holdup volume is being designed. This<br />
pump, which will use a turbine-type impeller, has<br />
the advantage that both the inlet and discharge<br />
can be at the bottom. HydruiJlic drive motors of<br />
suitably small dimensions have been found to be<br />
satisfactory drives for these pumps.<br />
Additional work has been done on the development<br />
of forced-c irculation corros ion-testi ng loops for<br />
obtaining information on the corrosion of lntonel<br />
in high-velocity turbulent fluoride mixtures with<br />
large temperature differentials in the system. TWO<br />
series of loops are being constructed to meet the<br />
following requirements: a Reynolds numhr of<br />
10,000 with temperature gradienfs of 100, 200, and<br />
300°F and c1 temperature gradient of 200'6 with<br />
Reynolds numbers of 800, 3,000, and 15,000. The<br />
maximum fluid temperature is to be !500°F. A<br />
forced-circulation loop is also being developed for<br />
tctting combinations of structural metals in contact<br />
with high-velocity turbulent liquid metals under<br />
high temperature differentials,<br />
Soveral exploratory tests were made of gas<br />
burners for use with the proposed gas-furnace heat<br />
source for h igh-temperature reactor mockup tests.<br />
Also, a study is under way 06 the cavitation phe-<br />
nomenon associated with operating liqiiid metal<br />
systems at elevated temperatures, high flow rates,<br />
-~<br />
ID. F. SalrnQn, ANP Quar. Prog. Rep. June 10, 1954,<br />
<strong>ORNL</strong>-1729, p 19.<br />
34<br />
H. w. Savage<br />
Aircraft Reactor Engineering Division<br />
and high pump speeds. A correlation of fluid-flow-<br />
noise intensity with pressure data noted.<br />
The number of stations available for convection<br />
loop testing has been increased from 18 to 31 so<br />
that many more long-term tests (2000 hr or longer)<br />
nnd intensive tests of special materials can be<br />
made. The basic design of the convection loops<br />
has been simplified, and various means of heating<br />
the loops and of making operation of them more<br />
automatic are being studied.<br />
IN-PILE LOOP COMPONENT DEVELOPMENT<br />
W. 8. McDonald<br />
Aircratt Reactor Engineering Division<br />
An in-pile loop for insertion in the MTR is to be<br />
designed, constrvcted, and operated as a joint<br />
<strong>ORNL</strong> and Pratt & Whitney Aircraft Division<br />
project. The loop is being developed for circu-<br />
lating proposed fuel mixtures so that the extent<br />
of radiation damage to materials of construction and<br />
the effect of radiation on the fuel can be de-<br />
termined. Preliminary QRNL work on this project<br />
is concerned with the design and development of<br />
compoiients of cr loop to operate in a horizontal<br />
beam hole. Further developmental work was also<br />
done on the vertical-shaft centrifugal puinp for use<br />
with both in-pi le and out-of-pi le forced-circu-<br />
lation loops.<br />
Horizontal-Shaft §ump Pump<br />
D. F. Salmon d. A. Conlin<br />
Aircraft Reactor Engineering Division<br />
The air-driven horizontal-shaft sump pump de-<br />
scribed previously' was operated with NaF-ZrF,<br />
at 1350OF. It produced a %psi head at 6000 rpm<br />
and n flow rate of 1.5 gpm. Initial difficulty in<br />
priming the pump was solved by momentarily<br />
flooding the impeller labyrinth. This pump, which<br />
was built as a pilot model for checking design<br />
principles, hot pump performance, and reliability,<br />
has too large o VO~~J~C;? holdup for in-pile use and<br />
will now be used as a laboratory pump.<br />
A new pump has been designed that has the<br />
required small pump holdup volume., For priming,<br />
this design incorporates a baffle in the sump tank