ORNL-2106 - the Molten Salt Energy Technologies Web Site

ORNL-2106 - the Molten Salt Energy Technologies Web Site ORNL-2106 - the Molten Salt Energy Technologies Web Site

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! ANP PROJECT PROGRESS REPORT 0.020 in. To minimize backlash and to prevent instrument pinion run-off (with attendant loss of synchronization), both the synchros and the poten- tiometers will be driven by a fine-pitch rack 1 in. longer than the power-transmi tting rack. Two plunger-sealed limit switches, which will operate through the motor control circuits, will be used to prevent rod overtravel at each end of the stroke, and one limit switch will be used for giving a 1% Ak/k reserve indication for filling operations. The drive mechanism, which will be canned, will be operated under a 15psi helium pressure. The helium consumption will be limited to that lost in periodic venting of the container. INSTRUMENT DEVELOPMENT R. G. Affel Thermocouple Data Reduction J. T. DeLorenzo W. R. Miller Equipment suitable for transmitting 100 therrno- couple signals on two conductors has been as- sembled and tested. As the simplified block diagram shows (Fig. 1.3.1), the input signals are -42 1800-rpm MOTOR MERCURY JET SWITCH NO.! scanned by a high-speed mercury-jet switch. This switch is actually a centrifugal pump, driven by a motor, which directs a fine stream of mercury at adjacent pins to complete a circuit. Synchronism between the two switches is assured by driving them with synchronous motors that operate from the same power source. Such a system offers several advantages. For example, a large number of temperatures may be scanned, visually, on one large, 17-in.-screen oscilloscope; alarm or moni- toring systems that scan several hundred readings a second are possible (available systems are limited to 1 point/sec or slower); temperature gradients or profiles on- equipment may be directly displayed; essentially all time lag in the system lies in the sensor, and therefore transient studies are limited only by the sensors; commercial null- balance potentiometric recorders can be used with such a system. The equipment being tested scans data at the rate of 2500 pointdsec. Conventional, Brown, multipoint, stripchart recorders have been modified to operate on the switch output, which is 30 pulses/sec, with each pulse 200 psec in duration. 1800-rpm MOTOR i MERCURY JET SWITCH N0.2 Fig. 1.3.1. Thermocouple Data Transmitting and Recording Apparatus. UNCLASSIFI€O ORNL-LR-DWG 14951 RECORDERS IN .

hd - Thus, even with an input signal only 0.006% of the time, the available, conventional equipment may be used in an integrated alarm or monitoring system. Cell Bulkhead Penetrations J. T. DeLonnro Fittings suitable for reactor cell penetrations for heater wiring, control wiring, chamber leads, and thermocouples have been examined. Preliminary specifications and drawings have been prepared for review, and a contract is to be negotiated with a vendor. Fuel-Expansion-Tank Level Indicator R. F. Hyland Tests are under way to determine the practica- bility of using a helium bubbler to obtain a con- tinuous fuel-level indication in the ART fuel- expansion tank in the temperature- range 1100 to 1500°F with a varying pressure above the fuel. The tests were designed so that information could be obtained on whether the bubbler tubes would become clogged with fuel or ZrF, vapor deposits, to determine the minimum helium flow that would provide an accurate level measurement, to study the effect of changes in bubbling tote on the accuracy of measurement, to learn the response of the system to pressure surges, 5nd to ascertain the accuracy of measurement. The test apparatus consists of a conventional purge system that utilizes a constant-differential relay and purgemeter to obtain constant flow and a pneumatic differential-pressure transmitter. One side of the pressure transmitter is tapped off the purge line, and the other s the apparatus, was k2% in the level range being measured. However, on fuel runs, errors of as PERIOD ENDING JUNE IO, 1956 large as 0.43 in. of fuel in 5 in. (8.6%) and as small as 0.12 in. in 5 in. (2.4%) were noted. The average error appears to be of the order of f5%. This error can probably be accounted for by the fuel-density change with temperature, which is known to an accuracy of only f5%, difficulties in the precise placement of the bubbler tube and the spark plug, and the slight inaccuracy resulting from the use of a spark-plug probe to indicate the fuel level in the vessel. It was found that a purge flow rate as small as 0.2 scfh of helium would yield consistent flow measurements, but the system response to pressure surges at this purge rate was sluggish. Purge rates of the order of 1.5 scfh (“1000 liters/day) of helium gave both consistent level measurements and fairly rapid system response to pressure surges. There is no observable change in level indication for any purge flow rate between 0.2 and 1.5 scfh. On the basis of 1850 hr of operation of the appa- ratus in one run, it appears to be practical to measure fuel level at a fuel temperature of llSO°F by the helium-bubble method on a static system. There has not yet been a sufficient number of hours of a 1500°F test to evaluate the results of level indication at this higher temperature. High-Temperature Pressure Transmitierr W. R. Miller Pressure transmitters manufactured by four different vendors have been evaluated in tests in the temperature range 1000 to 14OOOF. Three of the four units tested operated similarly. They were of the force-balance type that requires an external gas supply to maintain a zero pressure differential ross a bellows or diaphragm. The fourth unit ilites a diaphragm-isolated, NaK-filled tube tern in which the NaK hydrostatically transmits applied pressure to an external, low-temperature, displacement-type transducer. The tube-system und to have 0.6% or better, average on other types of pressure transmitters, g electrically operated devices. A h igh-temperature turbine-ty pe flowmeter has been developed for measuring flow in fused-salt 43

hd<br />

-<br />

Thus, even with an input signal only 0.006% of<br />

<strong>the</strong> time, <strong>the</strong> available, conventional equipment<br />

may be used in an integrated alarm or monitoring<br />

system.<br />

Cell Bulkhead Penetrations<br />

J. T. DeLonnro<br />

Fittings suitable for reactor cell penetrations for<br />

heater wiring, control wiring, chamber leads, and<br />

<strong>the</strong>rmocouples have been examined. Preliminary<br />

specifications and drawings have been prepared<br />

for review, and a contract is to be negotiated with<br />

a vendor.<br />

Fuel-Expansion-Tank Level Indicator<br />

R. F. Hyland<br />

Tests are under way to determine <strong>the</strong> practica-<br />

bility of using a helium bubbler to obtain a con-<br />

tinuous fuel-level indication in <strong>the</strong> ART fuel-<br />

expansion tank in <strong>the</strong> temperature- range 1100 to<br />

1500°F with a varying pressure above <strong>the</strong> fuel.<br />

The tests were designed so that information could<br />

be obtained on whe<strong>the</strong>r <strong>the</strong> bubbler tubes would<br />

become clogged with fuel or ZrF, vapor deposits,<br />

to determine <strong>the</strong> minimum helium flow that would<br />

provide an accurate level measurement, to study<br />

<strong>the</strong> effect of changes in bubbling tote on <strong>the</strong><br />

accuracy of measurement, to learn <strong>the</strong> response of<br />

<strong>the</strong> system to pressure surges, 5nd to ascertain<br />

<strong>the</strong> accuracy of measurement.<br />

The test apparatus consists of a conventional<br />

purge system that utilizes a constant-differential<br />

relay and purgemeter to obtain constant flow and a<br />

pneumatic differential-pressure transmitter. One<br />

side of <strong>the</strong> pressure transmitter is tapped off <strong>the</strong><br />

purge line, and <strong>the</strong> o<strong>the</strong>r s<br />

<strong>the</strong> apparatus, was k2% in <strong>the</strong> level range being<br />

measured. However, on fuel runs, errors of as<br />

PERIOD ENDING JUNE IO, 1956<br />

large as 0.43 in. of fuel in 5 in. (8.6%) and as<br />

small as 0.12 in. in 5 in. (2.4%) were noted. The<br />

average error appears to be of <strong>the</strong> order of f5%.<br />

This error can probably be accounted for by <strong>the</strong><br />

fuel-density change with temperature, which is<br />

known to an accuracy of only f5%, difficulties in<br />

<strong>the</strong> precise placement of <strong>the</strong> bubbler tube and <strong>the</strong><br />

spark plug, and <strong>the</strong> slight inaccuracy resulting<br />

from <strong>the</strong> use of a spark-plug probe to indicate <strong>the</strong><br />

fuel level in <strong>the</strong> vessel.<br />

It was found that a purge flow rate as small as<br />

0.2 scfh of helium would yield consistent flow<br />

measurements, but <strong>the</strong> system response to pressure<br />

surges at this purge rate was sluggish. Purge<br />

rates of <strong>the</strong> order of 1.5 scfh (“1000 liters/day) of<br />

helium gave both consistent level measurements<br />

and fairly rapid system response to pressure<br />

surges. There is no observable change in level<br />

indication for any purge flow rate between 0.2 and<br />

1.5 scfh.<br />

On <strong>the</strong> basis of 1850 hr of operation of <strong>the</strong> appa-<br />

ratus in one run, it appears to be practical to<br />

measure fuel level at a fuel temperature of llSO°F<br />

by <strong>the</strong> helium-bubble method on a static system.<br />

There has not yet been a sufficient number of<br />

hours of a 1500°F test to evaluate <strong>the</strong> results of<br />

level indication at this higher temperature.<br />

High-Temperature Pressure Transmitierr<br />

W. R. Miller<br />

Pressure transmitters manufactured by four<br />

different vendors have been evaluated in tests in<br />

<strong>the</strong> temperature range 1000 to 14OOOF. Three of<br />

<strong>the</strong> four units tested operated similarly. They were<br />

of <strong>the</strong> force-balance type that requires an external<br />

gas supply to maintain a zero pressure differential<br />

ross a bellows or diaphragm. The fourth unit<br />

ilites a diaphragm-isolated, NaK-filled tube<br />

tern in which <strong>the</strong> NaK hydrostatically transmits<br />

applied pressure to an external, low-temperature,<br />

displacement-type transducer. The tube-system<br />

und to have 0.6% or better, average<br />

on o<strong>the</strong>r types of pressure transmitters,<br />

g electrically operated devices.<br />

A h igh-temperature turbine-ty pe flowmeter has<br />

been developed for measuring flow in fused-salt<br />

43

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