MONITORING THE CONTENTS OF A CONTAINER BY ULTRASONIC MEANS

Abstract: The contents of the container (1) are non-intrusively monitored by probing the container with an ultrasonic signal, and measuring changes in the ultrasound signature of the received signal after the signal has passed through the contents of the container.

Description: MONITORING THE CONTENTS OF A CONTAINER BY ULTRASONIC MEANS This invention relates to apparatus and methods for monitoring, non-intrusively, the contents of a container containing fluid. The invention relates particularly, but not exclusively, to a method of non-mtrusively monitoring the gaseous contents of a container in order, for example, to confirm the composition or purity of the gas within the container. It is often important to be able to monitor and confirm the composition or purity of gas contained within a container in order to monitor possible events, such as corrosion of the container, or to detect a leakage of the gas contained within the container or the leakage of a gas into the container. This may be particularly important when the gas or other contents of the container are toxic or in some other way harmful. The invention therefore has particular application in, for example, the nuclear industry where the storage of radioactive substances requires continual or periodic monitoring of storage conditions to confirm continuous safe storage. It may also be useful to non-intrusively monitor the contents of a container holding hazardous fluid or solid m the form of, for example, flammable, biological or pharmaceutical materials . The invention may also be useful in monitoring the contents of containers in the vicinity of potentially hazardous processes such as in the operation of high voltage switch gear where gas within containers provides electrical insulation for the switchgear . Known methods and apparatus for monitoring the gaseous contents of a container in order to confirm the composition of the gas within the container reqαne penetration of the container in order to sample the gas contained within the container or m order to introduce a sensor into the container. A problem with such known methods and apparatus is that because it is necessary to penetrate the container, there is a risk that leakages from the container occur around the area where penetration has taken place. Such systems, in seeking to establish that no leakage is occurring have to generate a potential site for leakage. This is technically undesirable and a potential problem with regulatory authorities. Spent nuclear fuel is highly radioactive and it is necessary to appropriately deal with the fuel to ensure that the radioactive spent fuel does not contaminate the environment.. There is a requirement to be able to safely store spent nuclear fuel for an intermediate period known as "interim storage" which period may be prolonged if required, pending a decision as to whether reprocessing or disposal of the fuel is to be undertaken. Spent fuel is typically stored within a sealed container during such storage. Typically, a container suitable for interim storage of spent fuel comprises a canister made of pressure vessel grade steel within which the spent fuel is held. The canister incorporates radioactive shielding in its lid. Once the canister has been filled with spent fuel, it is fitted with a lid and welded. The final welding of the lid seals the fuel. The lid of the canister will typically have a double seal. Prior to final sealing of the lid, the canister is filled with helium so that the spent fuel is held in a sealed container in a helium atmosphere . To provide further radiation shielding " the canister is placed in a concrete storage cask which is also fitted with a lid. The canister may be positioned within a concrete cask such that there is a space between the canister and the cask. The cask has inlet ports at the bottom and outlet ports at the top so that air may flow within the concrete cask in order to cool the canister . The concrete outer cask provides shielding for both gamma and neutron radiation and protection against external hazards. It is desirable to be able to, from time to time, monitor the contents of the canister m order to ensure that no untoward reactions are occurring within the canister. Such checks would also indicate the continued integrity of the fuel cladding m the canister . A known method of monitoring spent fuel within a sealed canister or dual purpose metal cask involves opening the sealed canister to examine the fuel and the atmosphere surrounding the fuel known as the cover gas within the canister. A disadvantage with this known method is that there 15 a risk of contamination to the surroundings and the facilities required are extensive and expensive. In addition, it is neither easy nor practical to be able to continuously monitor the canister and contents thereof using such a method. A second known method of monitoring spent fuel within a canister is through use of an installed penetration by which it is possible to attach instrumentation to measure the pressure or quality of the cover gas over the spent fuel or the seal interspace gas. Measurement of such gases will provide information relating to the chemical composition of the cover gas m the canister. A disadvantage of this known method is that the presence of the penetration prejudices or degrades the integrity of the containment barrier of the canister thus providing a potential leak which could lead to radioactive contamination. According to a first aspect of the present invention, there is provided a method for non-mtrusively monitoring the contents of a sealed container comprising steps of: transmitting an ultrasonic signal through a wall of the container into the contents of the container, receiving a signal from within the container, and analysing the received signal thereby deducing the composition of the contents of the container. This can thus be achieved without having to αnseal the container. Accordmg to a second aspect of the present invention there is provided apparatus for non-mtrusively monitoring the contents of a sealed container the apparatus comprising: transmitter means for transmitting an ultra-sonic signal through a wall of the container into the contents of the container; receiving means for receiving a signal from within the container; analysing means for analysing the received signal thereby deducing the composition of the contents of the container. By means of the present invention it is possible to measure at intermittent intervals the quality of the atmosphere within a container . The canister may be a substantially gas tight canister. The canister may be a metal canister, for instance of carbon steel or stainless steel. The canister may be formed of a body and one or more lid elements. The one or more lid elements may be sealed to the body in use. Preferably a first lid is provided , together with a second outer lid. Preferably the first lid is received within the opening to the canister. The first and/or second lid may rest on one or more internal lips provided by the canister. The one or more lid elements may be welded to the body. The welds may provide a gas tight seal between a first lid and the canister and a second lid and the canister. Preferably the canister has the general form of a right cylinder. Preferably the lids are provideα on the top end of the canister, most preferably within the profile of the side wall of the canister, such that an end wall of the side wall is exposed. Preferably the canister contains spent nuclear fuel rods or other irradiated nuclear material. The canister may be provided with an internal gas pressure of greater than ambient, a positive pressure. The positive pressure may be at least 1.1 atmospheres, more preferably at least 1.2 atmospheres. Preferably the gas in the canister _≤ substantially helium. Preferably the canister is provided within a furtr.er container m use. The outer container may be a cask, fcr instance a concrete cask. Preferably the internal configuration of the outer container generally matches the outer configuration of the canister. The outer container may be provided with a lid to seal the body of the container following insertion of the canister. Preferably the outer container is provided with a supply of cooling gas to its interior. Preferably the cooling gas directly cools the outside of the canister. The cooling gas is preferably air. An inlet to the inside of the outer container and an outlet therefrom may be provided. Preferably the inlet and outlets are dog-legged. The invention may be used to measure the fluid contents of a container and may therefore be used to monitor a gaseous or liquid content of a container. The invention may be used to measure the presence of one or more components of a gas. For instance, the presence of air in an helium atmosphere or the presence of xenon and/or krypton in an helium atmosphere may be measured. The invention may be used to measure the level of one or more components of a gas. For instance, the level of air in an helium atmosphere may be measured or the level of xenon and/or krypton m an helium atmosphere may be measured. Advantageously, the method comprises the steps of measuring the sound velocity and/or attenuation of the transmitted signal and / or the reflected signal. The sound velocity ana/ or attenuation may ϋe considered at more than one frequency of transmitted signal. By measuring velocity and attenuation at least two different frequencies of transmitted signal, unknown quantities in the calculations / algorithms required to derive information regarding a composition of the contents are eliminated from the calculations. The metnod may measure the velocity and/or attenuation using transmission measurements. The method may measure the velocity and/or attenuation using reflected measurements. Conveniently, the method comprises the step of measuring velocity and attenuation of both a transmitted signal, such as a "line of sight" received signal, and a reflected signal . The transmitted ultrasound signal may be provided by a transducer . Preferably the ultrasound source and/or receiver therefore is removed from the canister between at least some of the tests. The transmitter and/or receiver may be removed whenever the time period between tests exceeds 1 hour, or more preferably 1 day. Preferably a calibration and/or checking station is provided for the transmitter and/or receiver and/or accompanying electronics between at least some of the tests. Preferably such checks are made when tests are separated by more than 1 hour and more preferably by more than 1 day. Conveniently, the source of the transmitted signal is positioned outside the container, and a receiver is positioned outside the container. The source of the signal and/or receiver are preferably mounted on the lid of the container. The source of the signal and/or receiver may be mounted on a side wall of the container, preferably on the top of the side wall. The source of the signal and/or receiver are preferably provided in a housing. The housing may be mounted on the lid of the canister, for instance the outer lid or the inner lid. The housing may be mounted en the outer surface of the outer lid, with a passage connecting the monitoring location in the housing to the body of gas within the canister, the passage being provided in a passage defining element which passes through the lid or lids, the cross-sectional profile of the passage defining element as it passes through at least a part of a lid being less than the cross-secticnal profile of the housing, parallel to the lid. Preferably the cross-sectional profile is less throughout the elements passage through the outer lid, ana if present the inner lid. The housing may be mounted on the outer surface of the inner lid, witn a passage connecting the monitoring location xr the housing to the body of gas within the canister, the passage being provided in a passage defining element which passes through the inner lid, the cross-sectional profile of the passage defining element as it passes through at least a part of the inner lid being less than the cross-sectional profile of the housing, parallel to the lid. Preferably the cross-sectional profile is less throughout the elements passage through the inner lid. Preferably the cross-sectional profile of the housing as it passes through the outer lid is substantially the same as the housings cross-sectional profile outside the outer lid. The housing may be mounted on the end wall of the side wall of the canister, most preferably wholly within the outline of the extension of that side wal'l . The housing may be welded to the canister. The housing may be formed of one or more different materials . The received signal is preferably subjected to signal processing to extract the desired information. The signal processing may involve Fast Fourier Transform and / or chromatic baseα processing. The signal processing may involve the application of one or more Gaussian processors to the signal. The processors are preferably nonorthogonal . Preferably the processors cover the range of transmitted and / or received signal frequencies. Three processors maybe applied. Preferably the processor outputs are further processed algorithmically . Preferably the algorithm results corresponding to the nominal energy content of the signal and / or the dominant frequency and / or the effective bandwidth, most preferably all three. The signal may be represented as a point on a three dimensional plot defined by the nominal energy content of the signal, the dominant frequency and tne effective bandwidth. The condition within the container may be represented as α point on a three dimensional plot. The change in conditions may be represented as a deviation in one or more dimensions relative to that point. The extent of the deviation may represent the magnitude of the change in conditions. The direction of the deviation may represent the type of change in conditions. Alternatively however the transmitter may be positioned within the container and may be activated by, for example, a signal transmitted from outside the container. A transmitter suitable for positioning within the container may comprise, for example, a tuning fork or resonant cavity. The canister will normally be filled with helium at a pressure of about m atmospheres at the time of sealing the canister. By means of the present invention, it is possible to confirm the continued presence of helium, the absence of atmospheric gases principally oxygen, the absence of fission product gases. It is also possible to discriminate between oxygen and fission product gases, so indicating the type of failure occurring. The continued presence of helium, which is a highly mobile gas, will confirm that the canister is still satisfactorily sealed. The absence of oxygen will confirm that corrosion of the external surface of the canister has been inhibited. The absence of fission product gases will confirm that no deterioration of fuel integrity has taken place since the loading of the spent fuel into the canister. By transmitting ultrasonic sound waves into the canister and receiving waves back from the canister (waves which have passed throuσh the internal gas the effects of variation m gas temperature can be allowed for, and the nature and amount of any foreign gas identified. The internal gas at a monitoring location may be investigated. The monitoring location may be within the body of the canister. The monitoring location is preferably provided outside the body of the canister, but still sealed relative to the surrounding environment. Preferably the monitoring location is provided with a housing, most preferably the housing for the transmitter and/or receiver for the ultrasound. Preferably the monitoring location is provided m proximity to the outside of the canister lid. The monitoring location is preferably connected to the internal body of gas m the canister via a bore or other passageway. The bore may be of circular cross-section. Preferably the bore includes one or more dog-legs. Preferably the bore passes from within the canister oody to outside. The bore most preferably passes through the lid or lids of the canister. The bore may alternatively pass through the side wall of the canister. The bore may pass up through the side wall of the canister, towards the lid end of the canister. The bore may pass through the side wall of the canister, for instance to connect to an element externally provided on the canister and leading to the monitoring location. The monitoring location is preferably m proximity to the transmitter and/or receiver. Ideally the monitoring location is provided between the transmitter and the receiver. The transmitter and receiver may be separated by a gap of between 0.5 and 20cm or more preferably 3 and 8cm. The transmitter and/or receiver are preferably separated from the monitoring location by a thickness of material. The material thickness is preferably at least 5mm and more preferably at least 10mm or even 20mm. Preferably a volume of gas is provided in the housinα on the distal side of the monitoring location relative to the body of the canister. Preferably the body of gas has a greater extent, perpendicular to the bore supplying it and/or parallel to the axis of the transmitter/receiver alignment, than the monitoring location itself. A d sc shaped gas volume ma_ be provided. In this way reduction of noise is facilitated. It has previously been thought impossible to use sound or ultrasonic waves to determine the contents of a canister due to the fact that the temperature of the gas within the canister will affect the characteristics of reflected sound waves . In addition, m order to be able to deduce the composition of the fluid within the container, the signal sound wave has to travel through a thick container wall without unacceptable signal loss. It had previously been thought that the attenuation of signals due to the thickness and nature of the canister material would be an insurmountable problem in using ultra-sonic signals to determine the contents of the container. In addition, further problems associated with the method of the present invention include attenuation of the signal due to the impedance mis-matchmg at changes of material. Further, a large amount of noise is generated by spurious internal reflections of the signal. The physical properties of helium, oxygen and krypton / xenon (the principle fission product gases) m terms of atomic weight, molecular weight and bonding characteristics are sufficiently different to one another to allow reliable discrimination at the levels which would be expected within a canister containing spent fuel. The present invention therefore provides a method where ultra-sound is transmitted through a container wall which may be metallic and may have considerable thickness, or alternatively may be a non-metallic material. The ultra-sound may traverse through the gas or fluid within the container and then be received and detected through the container wall at a different point to that of which the ultrasound was transmitted into the canister wall initially. Alternatively, it may be received and detected at the same point at which it was transmitted through the canister wall following reflection of the signal. The passage of the signal through the gas at ospnere or fluid will have modified the signal signature so by comparing the transmitted and received signals the composition of the gas or fluid may be inferred. In particular, the speed of sound, ICS attenuation and its frequency may be modified by differences m gas or fluiα composition . Alternatively, the resonance frequencies of the container and internal structures will be altered by the contained gas or fluid composition and this change may be used to infer the composition. The signal may be produced by means positioned outside the canister for example a transmitter. Alternatively, the signal may be produced from transmission means contained within the canister. Such transmission means may be m the form of, for example, a tuning fork or resonant cavity which may be activated from outside the container. The invention will now be further described, by way of example only, with reference to the accompanying drawings m which: Figure 1 is a schematic representation of canister containing spent fuel monitored by means of an embodiment of the present invention; Figure 2 is a partial cross-sectional view of the top portion of a spent fuel canister illustrating a further embodiment of the invention Figure 3 is a detailed cross-sectional view of the sensor component of Figure 2; Figure 4 is a partial cross-sectional view of the top portion of a spent fueJ canistei illustrating a still further embodiment of the invention; Figure 5 is a partial cross-sectional view of the top portion of a spent fuel canistei illustrating a yet further embodiment of the invention; Figure 6 illustrates a variation on the top portion of the canister of Figure 2; Figure 7 illustrates a further variation on the top portion of the canister of Figure 2; Figure 8 illustrates in plan view a variation on the embodiment of 4; Figure 9 displays experimental results for time difference between transmission and reception for ultrasound signals with varying gas composition; Figure 10 illustrates a typical input signal and a typical detected signal; and Figure 11a to lie illustrate the application of a signal processing technique suitable for use in the present invention. Referring to Figure 1, a container suitable for storing spent fuel is designated generally by the reference numeral 10. The container comprises a canister 12 which is loaded with spent fuel rods 13 and is then is sealed with a welded lid. Once the spent fuel 13 is sealed within the canister 12 the canister 12 is vacuum dried then back filled with an inert gas, such as helium, which surrounds the spent fuel rods 13. Thermal conduction from the fuel rods 13 within the canister 12 is enhanced through the use of the helium atmosphere at a pressure slightly above atmospheric . Once loaded with spent fuel the canister 12 is positioned within a concrete cask 14 such that the outer surface 15 of the canister 12 and the inner surface 16 of the cask 14 are spaced apart from one another. This allows air flow from an air inlet 17 to an air outlet 18 formed in the outer wall 9 of the cask 14. It is necessary to have air flow passing over the canister 12 to maintain fuel temperature below regulatory limits. It is envisaged that the spent fuel rods 13 may be stored within container 10 for many decades. This means that it may be prudent to be able to provide for monitoring the contents or tne canister regularly and reliably over these time scales to assist m demonstrating and confirming safe confined storage conditions to government regulatory officials. By means of the present invention it is possible to detect the leakage of oxygen from the surrounding air into the helium atmosphere with a sealed canister m a non-mtrusive manner. By means of the present invention, the atmosphere of the canister is probed with ultrasonic signals. An ultrasonic signal transmitted into the canister will emerge from the canister, and by measuring changes m the ultrasound signature of the received signal produced by any oxygen influx, presence of oxygen may be detected. In particular, changes m sound velocity, attenuation, resonant frequencies and structures may indicate oxygen leakage into the canister. Additionally or alternatively variations in pressure within the canister may be monitored by detecting similar variations with pressure. Additionally or alternatively, as xenon and krypton gases may also be released during storage of spent fuel within the sealed canister m the event of failure of fuel rod cladding it, it is desirable to be able to monitor relatively small variations in the levels of such gases within the helium atmosphere. These Eaffects can also be monitored by suitable consideration of their effect on the ultrasound investigation. For an ideal gas the sound velocity is given by:- v = yrT ' P where γ = ratio of specific heats; r = gas constant; T = temperature; o = molecular weight. For a binary mixture y, are proportionally modified. As can be seen from equation ( 1 ) a variation in o results from a variation in the relative He, C_ composition. Thus at 30°C a complete change of atmosphere from He (p = 4, v = 1024.7 ms " 'ι, to oxygen ιp = 16, v = 332ms "1 ) leads to v c /v Hβ = ^ (or δ v = 660 s " ' . Calculations indicate that for a 10:90, 0 ^ =He mixture the sound velocity would be 764.4ms " i.e. d change of 260.3ms * '= 25%) from pure He. This variation is easily detectable experimentally and is particularly suiteα to mono-atomic gases, as is the case in the surrounding gas for spent fuel rod storage. Equation (1) also indicates that the velocity scales with T as it does with p so that a temperature change from 30 to 300 " Z would approximately lead to a velocity increase of x(3 - 4) . As a consequence of this variation t is of the upmost importance m many applications to provide for an accurate compensation for any temperature variation between measurements. This can be achieved by direct measurement of temperature conditions, with appropriate compensation for changes. However, it is a particularly significant advantage of the present invention that investigation at a number of frequencies can also determine temperature and thus account for it. Pressure variations are, however, sufficiently small to have no meaningful effect. As well as allowing consideration of z levels m the He atmosphere, any Xe, Kr released from the fuel would also affect p (for Xe, p = 131; Kr, p = 84) . Proportionately smaller amounts of Xe, Kr could produce significant sound velocity changes of the cask atmosphere due to further variation m p and hence v. The sonic velocity will vary with both frequency and gas pressure. The variation is due to visco thermal, and in the case of diatomic gases, vibrational and rotational relaxation effects. As well as variations in the speed of the ultrasound travel, variations m the attentuation of the sound wave can be expected. The attenuation, α, <^f a soundwave in a gas is usually quoted in terms of the parameter :- « P where ( = absorption coefficient; p gas pressure; J frequency) . The total absorption in a binary gas mixture in which one component is polyatomic is the sum of tnree terms: p = F : , (viscosity, thermal conduction) + F , f" (diffusion) + F, (vibration / rotation energy relaxation) . As a variation m the components present changes the attenuation effects can also, therefore, be used for also detecting differences m concentration of two binary components and for distinguishing between different contaminants and temperature effects. Thus, for example, (α p / j " ) for He and a 10:90 0-, : He mixture are 0.525 and 1.546 respectively so that a 10% oxygen contamination would produce a factor of 3x change. The above mentioned theoretical techniques can be deployed according to the present invention in a variety of different manners. In the following examples particular emphasis is placed on the monitoring of canisters for spent nuclear fuel. The embodiment illustrated in Figure 2 shows the top portion of a canister of the general type designated 12 in Figure 1. The canister 200 comprises a cylindrical side wall 202 and lid structure 204. The lid structure 204 is formed of an inner shield lid 206, which rests on lip 208, and an outer structural lid 210, which rests on lip 212. Both the shield l d 206 and structural lid 210 are welded in position with gas tight wields. The spent fuel rods are contained in the volume 214 below the shield lid 206. Mounted on the structural lid 210 is the monitor housing 216. The housing 216 provides a structural wall thickness 218 around the monitoring location 220. The structural wall thicknesses required to met regulatory standards vary for materials (for instance 25mm thickness for carbon steel, 19mm thickness for stainless steel). The monitoring location 220 consists of a cylindrical bore 222 leading from the cavity volume 214 to the monitoring location 220 and beyond to a "top hat" configuration 224. The bore 222 is fully enclosed by the housing 216 to manitam the isolation of the cavity volume 214 and its helium atmosphere from the surrounding cooling air volume 226. The bore 222 is dog leg for shielding purposes. On either side of the monitoring location are two bores 228 m the housing 216, the bores receiving the transmission transducer 230 and receiver 232. Ultrasound is passed through the monitoring location 220 and the appropriate characteristics of its passage are measured to g ve the desired information. Although physically remote from the cavity volume 214 measurements at the monitoring location 220 are accurate representations of the cavity volume due to the extreme mobility of helium. Additionally the time period between measurements is likely to be days or more with very gradual or no change expected between tests, as a consequence this gas volume is fully representative . As illustrated in more detail in Figure 3, the bore 222 consists of a main bore 234 and subsidiary bore 236 connected by a cross-bore 238. The housing 216 is mounted on the structural lid 210 by plate 240 which is wielded thereto by wields 242 and 244. To ensure good ultrasound contact between the transducers 230, 232, gel is provided on the end faces of the bores 228. As alternatives to flat ends for the bores, concave or convex faces can be used to focus the ultasound. The top hat shape to the upper section 246 of the bore 222 is so shaped for the purposes of damping noise signals spreading from the source to reciever transducer. The transducers 230, 232 face each other across a gap of 5 to 6cm m the case of a 40kHz ultrasound system. As an alternative to direct contact between the end of the bore and the transducer, the transducers may be provided with plates connected to the end surfaces of the transducers by spigots . Whilst Figure 2 and 3 imply the use of a unitary element to form the housing 216 acoustic filtering advantages can be obtamed by forming the housing of different materials. The different materials may filter the noise signal anα/or give enhancing directional effects. Acoustic filtering of the signals arising m the system, through appropriate structural configurations, is important m ensuring that the quicker signal transmission of the ultrasound through the housing does not give a noise signal which swamps th slower transmission of the ultrasound through the gas oemg monitored. The frequency of the ultrasound, the gap between the teansducers, the relative thicknesses of the intervening walls, side walls and surrounding walls all, individually and together, effect the system and can be used to effect its operation accordingly. The transducers 230, 232 are only introduced once the fuel has been loaded, as part of the loading procedure will involve the complete emersion of the canister 200 including the housing 216 in the cooling pond where the fuel is stored. The transducers 230, 232 and accompanying electronics to which they are attached (not shown) are removed from the housing 216 between tests to reduce the potential for radiation damage of the transducers and their surrounding electronics and also to reduce the number of measuring equipment sets that are needed. As tests on the gas content may be days, months or even years apart, it is wasteful to leave that part of the equipment m-situ during that time. In general, the measurement system is checked against a known standard or other claibration technique, before and/or after being used, to ensure correct operation. True verification of the systems correct operation can therefore be provided, away from the canister if desired. To give accurate measurements the temperature of the monitoring location is measured. The temperature monitoring can be effected by a thermal couple attached to the housing at a consistent position between tests. A pair of thermocouple, one at substantially the same location as the transmitting transducer, one at substantiall th« same position as the receiver are preferred m this regarα. There is no need for the temperature monitoring apparatus to intrude into the internal cavity (thereby avoiding leakage site generation) provided a consistent correction is applied. The output from the thermocouples are fed to the processing electronics to provide a correction signal. This signal can be used to correct the gas monitoring result to ensure that variations m temperature, for instance cooling of the cannister over the years, does not give a false reading of gas change. Measurement of pressure within the cavity may also be desirable to remove the effect of any pressure variation from the signal analysis m a similar manner to that discussed above for temperature . In Figure 4 an alternative positioning of the housing 216 is provided on the top wall 400 of the cylindrical wall 402 of the canister 200. This provides the necessary clearance for the introduction of the shield lid 204 and structural lid 210 following introduction of the spent fuel. The conection between the monitoring location 404 and the cavity volume 406, m this case, is provided by a bore 408 in the cylindrical side wall 402. The monitoring operates in a similar manner to that outlined above . In Figure 5 the housing 216 is provided on the end of a bore carrying element 500 fixed to the side wall 502 of the canister. The bore 504 in this element 500 conects the measuring location 506 to the cavity volume 508. In the alternative form of mounting for the housing 216 of Figure 2, illustrated m Figure 6, the housing base 600 penetrates the structural lid 210 and rests on the shield lid 204. In this way only the, relatively narrow, bore carrying element 602 needs to penetrate the shield lid 204, thereby reducing the variation between the existing canister and a canister 200 embodying the present invention. In the still further alternative form of mounting for the housing 216 shown m Figure 7, the housing 216 rests on the top surface 700 of the structural liα 210. In this way the structural lid 210 and the shield lid 204 are both only penetrated by the relatively narrow, bore carrying element 702. In certain instances the housing must have quite deep bores for the transducers to give sufficient signal introduction and sufficent signal collection capability for the best results to be achieved. Transducers of 6 to 8 inches in length and 3 inches m diameter are suitable for many applications. In general the longer the transducer the better the filtering that is achieved. The Figure 4 and Figure 5 type embodiment positioning of the housing can be a problem m this regard. Figure 8 illustrates an embodiment of the invention which provides the necessary clearance for the lids 800, but provides the necessary bore length 802 by extending the housing 804 around and within the profile of the cylindrical wall 806. This form of housing 804 also avoids intrusion of the housing 806 outside the cylindrical profile, an important consideration given the very limited clearances which exist between the outside 810 of the cylindrical wall 806 and other parts of the apparatus during transfer of the canister from the cooling pond, where it recieves the spent fuel, and the concrete cask. The Figure 8 and other embodiments of the invention illustrate a transmission system for determining the ultrasonic effects. This and the other embodiments of the invention can, however, use reflective measurements. In such cases a substantially coincident transmission and reception location may be provided or the transmission ana reception locations may be provided close to one another, but separated by a small angle. The opposing side of the core containing the gas may be shaped to promote ultrasound rerlection. To illustrate the techniques effectiveness reference is made to Figure 9 which displays the time difference between signal emission and reception against different gas compositions for air to helium mixtures. In Figure 10 a typical input signal (solid line 1000 i and a typical detected signal (solid line 1002) are illustrated. The detected form includes both that part of the signal which crosses the gas gap to the detector and also a significant noise signal which travels around through the housing itself to reach the detector . To achieve the necessary accuracy in the results using the techniques of the present invention it is desirable to apply certain signal processing techniques. Preferred embodiments of the invention use Fast Fourier Transform method or the new technique of chromatic filtering to extract the desired information from the detected signal. The technique of chromatic processing is illustrated in Figure 11a to lie. Chromatic filtering of a signal (figure 11(a)) involves the use of n nonorthogonal Gaussian processors (figure 11(b)) which cover the range of frequencies covered by the signal. In one embodiment n = 3 the outputs of the Gaussian processors are manipulated algorithmically to provide at each instant m time a signal detection m terms of three parameters namely the nominal energy content of the signal, the dominant frequency and the effective bandwidth. The signal is effectively represented by a single point in a three dimensional chromatic space defined m terms of these parameters (figure 11(c)). In this embodiment the conditions within the fluid containing canister are defined by the position of the signal defining point n cnromatic space. Deviation of this point from its nominal equilibrium position is indicative of chang e d conditions m the canister. Experience with other measurements mαicate tnat : • The type of fault producing a change is characterised by the direction of the deviation from equilibrium. • The extent of fault development is characterised by the magnitude of the change. Fault types and their characteristics are determined empirically from a prior calibration. From the above mentioned three parameters the time of flight of the ultrasound through the gas gap can be determineα m the desired manner. The process alsc reveals significant other information on differential attenuation and propagation which can be used. It is likely that some resonant frequencies of the gas containment facility will depenα upon the mass density of the gas within the structure. There is, therefore, the possibility of exploring whether such an approach could yield further information about the composition of the gas atmosphere. At one extreme such an approach might give a better "integrated atmosphere" indication since ma or parts of the casket volume would have an effect (rather than simply a "line of sight", local indication) . At the other extreme, a "line of sight" approach may well, in any case, excite resonances which will need to be taken into account m the analysis of test results . Sound velocity and attenuation co-efflcients may be evaluated m detail for the gaseous components He, 0 , N , Xe and Kr separately m various combinations for a range of acoustical frequencies . The purpose of these calculations is to determine the extent to which the different atmospheric combinations within the fuel storage canister might be distinguished. Differences m acoustical velocities will indicate the presence of different species. Differences m attenuation coefficient will indicate temperature effects, whilst the frequency dependence of the velocity and attenuation coefficient may enable different contaminants to oe distinguished. Calculations used to determine the composition of a gas content within a canister will take into account tne structural considerations of the canister. Some of the resonances will depend on the mass density of the gaseous atmosphere. When putting the invention into practice it is necessary to define a range of sonic frequencies to oe used m order to maximise trends and variations between different contaminants. For example, it may be possible to discriminate between oxygen and Xe/Kr on the basis of the rotational energy and relaxation of the oxygen molecule if sufficiently high frequencies are employed. In addition, for "line of sight" measurements sonic attenuation will have to be minimised for appropriate choice of frequency when taking into account the structure. The acoustic transducer could be either electromagnetic, a capacitance, or any other type of transducer. Depending on the choice of source and detector, it may be advantageous to use optical fibres in order to detect the received signal. Although the present invention has been described primarily with reference to use in connection with monitoring of spent nuclear fuel contained within fuel canisters, the invention would also be applicable m areas where materials which are harmful to human beings are being handled or transported, for example, toxins, biological materials and medical materials.

Claims: CLAIMS : 1. A method for non-mtrusively monitoring the contents of a sealed container comprising the steps of: transmitting an ultrasonic signal through a wall of the container into the contents of the container, receiving a signal from within the container, and analysing the received signal that, therefore deducing the composition of the contents of the container without having to unseal the container. 2. A method according to claim 1, comprising the steps of measuring the sound velocity and attenuation of the transmitter signal and the received signal at more than one frequency of transmitted signal. 3. A method according to claim 1 or claim 2, comprising the step of measuring velocity and attenuation of both a "line of sight" received signal and a reflected signal. 4. An apparatus for non-mtrusively monitoring the contents of a sealed container, the apparatus comprising: transmitter means for transmitting an ultrasonic signal through a wall of the container into the contents of the container; receiving means for receiving a signal from within the container; analysing means for analysing received signal thereby deducing the composition of the contents of the container. 5. An apparatus accordmσ to claim 4, wherein the source of the transmitter means is positioned outside the container, and tne receiving means is positioneu outside tne container. 6. An apparatus according to claim 4, wherein the transmitter means is positioned within the container. 7. An apparatus according to claim 6, wherein the transmitting means is activated by a signal transmitted from outside the container. 8. An apparatus according to claim 6 or claim 7, wherein the transmitter means comprises a tuning fork or resonant cavity. 9. A method substantially as hereinbefore described with reference to the accompanying drawings. 10. An apparatus substantially as hereinbefore described with reference to the accompanying drawings.

Inventors: DICKSON ROBERT MCALPINE, GIBSON JOHN RAYMOND, JONES GARY ANTHONY, JONES GORDON REES, SINGH PERMINDER TONY, SPENCER JOSEPH WILLIAM, WOOLLEY KEITH, DICKSON, ROBERT, MCALPINE, GIBSON, JOHN, RAYMOND, JONES, GARY, ANTHONY, JONES, GORDON, REES, SINGH, PERMINDER, TONY, SPENCER, JOSEPH, WILLIAM, WOOLLEY, KEITH
Applicants: BRITISH NUCLEAR FUELS PLC, DICKSON ROBERT MCALPINE, GIBSON JOHN RAYMOND, JONES GARY ANTHONY, JONES GORDON REES, SINGH PERMINDER TONY, SPENCER JOSEPH WILLIAM, WOOLLEY KEITH, DICKSON, ROBERT, MCALPINE, GIBSON, JOHN, RAYMOND, JONES, GARY, ANTHONY, JONES, GORDON, REES, SINGH, PERMINDER, TONY, SPENCER, JOSEPH, WILLIAM, WOOLLEY, KEITH
Application year: 1998
Main classification: G01M3
IPC codes: G01M3, G01N29