Patent Number: 044180357
Section: description

DETAILED DESCRIPTION OF PREFERRED EMBODIMENT Referring now to the drawings in detail, FIGS. 1 and 3 illustrate a gamma sensor of the type disclosed in the aforementioned prior application, generally referred to herein by reference numeral 10. The sensor is shown in FIG. 1 within a nuclear reactor fuel core surrounded by a body of reactor coolant 12. The sensor includes an elongated heated body 14 that extends vertically through a fuel core, and is enclosed by an outer sheath 16 establishing thermal contact with coolant to form a radially outer heat sink to which radial heat flow paths extend when the body is internally heated by gamma radiation during power generation except at spaced regions in each measurement zone at which thermal resistance gaps 30 are located. In such regions, radial heat flow is inhibited to produce the varying temperature distribution. The sensor thereby measures heat flow rate which is directly related to local power generated at a plurality of vertically spaced measurement zones, one of which is shown in FIG. 1. The local heat rate measurement is effected by multiple junction thermocouples 18 at each of the measurement zones positioned within a central bore 20 of the heated body. As more clearly seen in FIG. 3, each thermocouple includes a pair of junctions 22 and 24 interconnected in series and embedded in an insulating medium 26, such as aluminum oxide enclosed within stainless steel cladding 28. The spaced junctions as shown in FIG. 1 are axially positioned adjacent to the thermal resistance gap 30 formed in the heated body at each measurement zone. Referring once again to FIG. 3, the junctions are electrically connected across a voltmeter 32 forming part of external instrumentation in order to register a differential temperature signal voltage reflecting the local heat rate or power developed at adjacent fuel rods. In accordance with the present invention, the thermocouple device 18 is positioned with its tip portion 34 and the faster responding junction 22 thereat vertically above the other junction 24. This is an inversion of the vertical thermocouple arrangement heretofore associated with gamma sensors as disclosed in the prior copending application aforementioned. Ordinarily, the reversal in location of junctions has little effect on normal operation of the thermocouple in measuring local power generation with the junction 22 acting as the cold junction while the junction 24 is the hot junction located in the hot region axially coextensive with the thermal resistance gap 30. Normal operation is based on the presence of coolant 12 continuously along the vertical length of the sensor establishing a uniform heat sink temperature for the outer sheath 16. The signal voltage exhibited at the voltmeter 32 will then be of a positive polarity. As a result of certain reactor malfunctions producing a loss of coolant, depletion in the body of coolant 12 causes a drop in coolant level 36 as shown in FIGS. 1A and 1B. When the coolant level drops below the upper faster responding junction 22 as shown in FIG. 1A, the region of the heated body 14 above the coolant level becomes hot relative to the region therebelow producing a reversal in polarity of the signal voltage exhibited at voltmeter 32. Such a reversal of signal voltage polarity would not occur if the thermocouple were inverted as in the arrangements heretofore utilized. The polarity reversal may therefore be utilized to trigger an alarm 38 or initiate an action sequence in order to cope with a reactor accident involving a loss of coolant. As shown in FIG. 3, the thermocouple cladding 28 is grounded at 40 in order to permit measurement of absolute sensor temperature during accidents, by means of a grounded voltmeter 42 electrically connected to junction 22. Further, the temperature readings of the voltmeters may be increased by electrical heating of the body 14 through a heater device 44 connected through switch 46 to an external source of heating current 48. The heater device is of the type disclosed in copending application Ser. No. 888,881, filed Sept. 28, 1978, serving an in-situ calibration purpose. As shown in FIG. 2, the heater device may be located within the bore 20 of heated body 14 amongst the thermocouples 18 for selectively providing additional electrical heating at all of the measurement zones served by the respective thermocouples 18 associated with each sensor. As will be explained further hereinafter, the heater device 44 not only enhances detection of a drop in coolant level, but also enables determination of heat transfer conditions at the external surfaces of the sensor 10. By way of example, FIG. 4 illustrates a typical nuclear reactor vessel 50 having a dome 52 at its upper end and a bottom 54 into which vessel penetration tubes 56 extend. The tubes 56 support various instruments such as sensors 10 hereinbefore described inserted through the bottom of the vessel into the fuel core 58 positioned within the vessel below the dome 52. The sensors are connected through cables 60 to a remote external instrument panel site as is well known in the art. Further, the vessel is provided with inlet or outlet nozzles 62 through which it is maintained filled with a liquid coolant such as water. The fuel core 58 is exposed to the coolant, and the coolant extends up into the dome 52. In accordance with the present invention, one or more of the sensors 10 extends vertically from the fuel core up into the dome so as to monitor heat transfer conditions of the coolant therein, including coolant level. The sensors also continue monitoring local power generation within the fuel core. Support and guidance for the vertically extended sensors may be provided by the thimble plug assembly 64 also already known in the art. Such plug assemblies are utilized to plug or close unused openings in the upper core plate 66 of the fuel core, except for a central opening 68 in the plate through which a sensor 10 extends pursuant to the present invention as more clearly seen in FIG. 5. An extension tube 70 is secured to the upper support plate 72 which ordinarily separates the dome 52 from the main vessel chamber above the fuel core. The tube 70 protectively encloses the vertically extended portion of sensor 10 within the dome and is accordingly aligned with the plug assembly. Also, the tube 70 is provided with openings 74 and an open upper end 76 in order to permit full exposure of the sensor to the coolant while protecting the sensor against deflecting forces generated by coolant movement. As hereinbefore pointed out, selective energization of the heater 44 associated with sensor 10 enhances the multiple monitoring functions of the sensor. By way of example, a sensor body 14 internally heated by gamma radiation at a heating rate of 0.075 BTU/gm. under normal reactor operation reflected in FIG. 1, will produce a differential signal temperature (TD) across the junctions 22 and 24 of approximately 2.degree. C. as measured by voltmeter 32. The absolute temperature of the sensor (TC) under such conditions without energization of heater 44 as measured by voltmeter 42, will be close to the coolant temperature (TW). With the heater 44 energized under normal operation, the heating rate of body 14 is increased to 3.075 BTU/gm. and the differential temperature (TD) increases to approximately 80.degree. C. as expected. However, the increase (.DELTA.T) in absolute sensor temperature (TC) is relatively small such as 5.degree.-10.degree. C., confirming that good cooling heat transfer exists. When the liquid coolant level 36 drops below the cold junction 22 as shown in FIG. 1A, the sensor at the level of junction 22 will be exposed to steam or a steam-hydrogen environment while the sensor at the level of junction 24 remains covered with liquid coolant. Such degraded cooling at the level of upper junction 22 disturbs the symmetrical heat flow pattern within body 14 to effect a reversal in polarity of the differential temperature (TD) of approximately -2.degree. C. without additional heating by heater 44. The absolute sensor temperature (TC) on the other hand will be elevated above coolant temperature (TW) by an amount (.DELTA.T) of approximately 2.degree. C. because of the poor heat transfer surface in the steam environment. A clearer indication of coolant loss sufficient to trigger alarm 38, for example, will be provided by energization of heater 44 resulting in a reversed polarity temperature difference (TD) of approximately -50.degree. C. while the difference (.DELTA.T) between absolute sensor and coolant temperatures rises to approximately 100.degree. C. Based on an estimated coolant temperature (TW) of 300.degree. C. from earlier measurements, and the absolute sensor temperature (TC), where .DELTA.T=TC-TW, data is available for calculating the heat transfer coefficient at the external surface of the sensor above the liquid coolant level 36 from the known expression h=Q/.DELTA.T(A), where (h) is the heat transfer coefficient, Q is the heating rate and (A) is the surface area of the sensor. FIG. 1B illustrates a further drop in coolant level below the lower junction 24. In the latter situation, the differential temperature (TD) is close to zero, whereas the difference (.DELTA.T) between sensor and coolant temperatures is the same as in the situation shown in FIG. 1A with the heat transfer coefficient (ha) above the coolant level considerably lower than the coefficient (hb) below the coolant level. The comparisons between heating modes for the different coolant conditions illustrated in FIGS. 1, 1A and 1B are summarized in the following table: __________________________________________________________________________ DIFF. SENSOR SIGNAL (.DELTA.T) Heat COOLANT ELECTRIC HEATING RATE TEMP. TC-TW Transfer LEVEL HEATER MODE BTU/gm. (TD) .degree.C. .degree.C. Coeff(h) __________________________________________________________________________ well above off 0.075 2 0 cold junction on 3.075 80 5-10 h.sub.b .apprxeq. 1000 (Normal) between cold off 0.075 -2 2 and hot on 3.075 -50 100 h.sub.b &lt; h.sub.a junctions h.sub.b .apprxeq. 100 well below off 0.075 0 2 both junctions on 3.075 0 &gt;100 h.sub.b &lt; h.sub.a h.sub.b &lt; 100 __________________________________________________________________________ The number of gamma sensors utilized in nuclear reactors for local power monitoring purposes, presently varies between 350 and 450. When such plurality of sensors are modified in accordance with the present invention, they may be allocated in various different ways for multi-function monitoring purposes. FIG. 6 schematically illustrates how such allocation may be utilized to provide a multiple function monitoring system. Variable proportions of the sensors denoted by reference numerals 78 and 80 are respectively assigned to coolant level detection and heat transfer measuring functions by selective energization of the associated electric heaters under control of heater control 82. A fixed proportion of sensors designated 84 may be utilized for temperature surveillance without any electric heating. The signal outputs of all such sensors are fed to a data processor 86 from which power distribution, absolute sensor temperature, heat transfer coefficient and coolant level readouts are obtained at 88, 90, 92 and 94. Through a feedback mode control 96, the proportion of sensors assigned to different measuring functions may be changed. All of the sensors grouped under assignments 78, 80 and 84 may also function to provide the data for the power distribution indicator 88.