SYSTEM FOR AEROSOL SAMPLING DURING MECHANICAL LOAD

Abstract

A system for sampling aerosols, for purpose of predictive analyses, from fractured test specimens is provided. The system includes a test enclosure, a load apparatus, and an aerosol sampling pack in fluid communication with the test enclosure. The test enclosure is sized to partially or completely receive the test specimen therein, and the load apparatus is configured to impart a mechanical load (e.g., tension, bending, torsion, shear forces, or compression) on the test specimen. The aerosol sampling pack receives solid aerosols that are generated upon fracture of the test specimen.

Claims

1. A system for sampling solid aerosols, the system comprising: a test enclosure to at least partially receive a test specimen that is to release solid aerosols when fractured; a mechanical-test apparatus configured to apply a mechanical load to the test specimen while the test specimen is at least partially received within the test enclosure; and one or more sampling packs configured to detect the solid aerosols to be released by the test specimen; and a pump for drawing the aerosols to the one or more sampling packs.

2. The system of claim 1, further including a source of inert gas to provide an inert gas inside the test enclosure.

3. The system of claim 1, wherein the one or more sampling packs include a cyclone sampler pack or a cascade sampler pack.

4. The system of claim 1, wherein the pump is a vacuum pump, the system further including a power supply that is configured to provide local power to the vacuum pump.

5. The system of claim 1, further comprising an aerodynamic particle sizer configured to determine sizes of the solid aerosols released by the test specimen.

6. The system of claim 1, further comprising a means for rinsing inside walls of the test enclosure upon completion of a mechanical test and for removing solid aerosols deposited on the inside walls during the mechanical test.

7. The system of claim 1, wherein the solid aerosols are released by the specimen when the mechanical load causes fracture of the specimen.

8. The system of claim 7, wherein the mechanical load that causes the fracture of the test specimen is one or more of tension, bending, torsion, shear, or compression.

9. The system of claim 1, wherein the test specimen comprises spent nuclear fuel.

10. The system of claim 9, wherein the spent nuclear fuel comprises high burnup spent nuclear fuel.

11. The system of claim 9, wherein the spent nuclear fuel comprises uranium dioxide.

12. The system of claim 9, wherein the spent nuclear fuel is shaped as a rod.

13. The system of claim 1, wherein the specimen comprises asbestos or concrete.

14. A system comprising: a test enclosure configured to supportably receive a test specimen therein, the test enclosure including a lid portion and a base portion, the base portion including first and second side openings to receive the test specimen therethrough; a load apparatus configured to apply a mechanical load to the test specimen when the test specimen is supportably received within the test enclosure; and an aerosol sampling pack in fluid communication with the test enclosure, wherein the aerosol sampling pack is adapted to detect solid aerosols released by the test specimen if fractured when subjected to the mechanical load.

15. The system of claim 14 further including: a conduit coupling the test enclosure to the aerosol sampling pack; and a vacuum pump to draw the solid aerosols into the conduit.

16. The system of claim 14, wherein the aerosol sampling pack includes a cyclone sampler pack or a cascade sampler pack.

17. The system of claim 14, further comprising an aerodynamic particle sizer configured to determine sizes of the solid aerosols released by the test specimen.

18. The system of claim 14, wherein the load apparatus is adapted to impart tension, bending, torsion, shear forces, or compression on the test specimen.

19. The system of claim 14, wherein the sampling pack comprises a battery configured to provide local power.

20. The system of claim 14, wherein the load apparatus is adapted to impart a four-point bending load on the test specimen.

Description

BRIEF DESCRIPTION OF THE DRAWINGS

[0013] FIG. 1 is a perspective view of test enclosure to partially contain a rod-shaped test specimen therein.

[0014] FIG. 2 illustrates the test enclosure of FIG. 1 in combination with a test specimen and a load apparatus.

[0015] FIG. 3 illustrates an aerosol sampler pack, power module, and vacuum pump for use with the test enclosure of FIGS. 1-2.

[0016] FIG. 4 is a perspective view of a test enclosure in accordance with another embodiment.

[0017] FIG. 5 is a perspective view of the test enclosure of FIG. 4 in combination with a load frame, with the front frame being omitted for clarity.

[0018] FIG. 6 is a schematic diagram of a further embodiment of a system for sampling aerosols as contained within a hot cell.

[0019] FIG. 7 is a perspective view of the system for sampling aerosols of FIG. 6.

DETAILED DESCRIPTION OF THE CURRENT EMBODIMENTS

[0020] The current embodiments include a system for sampling aerosols from fractured test specimens. The system includes a test enclosure, a load apparatus, and an aerosol sampling pack. The load apparatus is configured to impart tension, bending, torsion, shear forces, or compression on the test specimen, and the aerosol sampling pack is configured to sample the aerosols that are generated upon fracture of the test specimen. The load apparatus (e.g., the portion of a load frame that secures and loads the specimen) and the aerosol sampling pack can be external to or contained within the test enclosure. Examples of each embodiment are discussed below.

[0021] Referring first to FIGS. 1-2, a test enclosure in accordance with one embodiment is illustrated and generally designated 10. The test enclosure 10 is illustrated in connection with a four-point bending load, but can be modified for essentially any bending load (e.g., three-point bending, four-point bending), compressive load (e.g., uniaxial, biaxial, and planar), tensile load (e.g., uniaxial, biaxial, and planar), shear load, or torsion load. The illustrated test enclosure 10 includes a base portion 12 and a lid portion 14. The base portion 12 and the lid portion 14 cooperate to partially house a rod-shaped test specimen 100 therein, test specimen being shown in FIG. 2. In particular, the base portion 12 includes an enlarged base tray 16 and four sidewalls 18. The enlarged base tray 16 provides stability to the test enclosure 10, and two sidewalls define a U-shaped notch 20 for passage of the test specimen 100 therethrough. The base portion 12 also includes an access opening 22 for a sampler conduit, discussed below.

[0022] As also shown in FIGS. 1-2, the lid portion 14 includes first and second openings 24, 26 for first and second load pins 28, 30, and the base tray 16 includes first and second slots 32, 34 for first and second support pins 36, 38. The support pins 36, 38 are slightly higher than the base of each U-shaped notch 20, such that the test specimen 100 is supported by the support pins 36, 38. The support pins 36, 38 are connected to a fixed crosshead 40, and the load pins 42 are connected to a moving cross-head 42. Collectively, the support pins 36, 38, the load pins 28, 30, the fixed crosshead 40, and the moving cross-head 42 comprise the load apparatus. The test enclosure 10 helps fix the test specimen 100 in place, and the moving cross-head 42 moves down to apply a bending load to the test specimen 100. A load cell converts the measured load into an electrical signal for output to an integral controller. The fixed cross-head 40 and the moving cross-head 42 are supported across two columns, which collectively comprise the load frame. An example load frame includes the 5960 Series Load Frame by Instron of Norwood, Massachusetts, but other load frames can be used in other embodiments.

[0023] As noted above, the base portion 12 includes an access opening 22 for a sampler conduit. The sampler conduit provides a fluid flow path between the test enclosure 10 and an aerosol sampler pack 44, shown in FIG. 3. Air is drawn into the aerosol sampler pack 44 with the aid of a dedicated vacuum pump 46, the vacuum pump including an integral potentiometer for flow rate adjustment. The vacuum pump 46 is driven by an on-board power supply 48, for example a battery pack, to allow portability of the aerosol sampling pack 44, vacuum pump 46, and power supply 48, each being supported on an upright sensor bracket 50, collectively forming a sensor assembly 52. The aerosol sampler pack 44 in the illustrated embodiment is a cyclone sampler pack, but can be a cascade sampler pack in other embodiments. The cyclone sampler pack 44 samples and separates aerosols by the use of a centrifugal force. As aerosols enter the cyclone sampler pack 44 from the sampler conduit 54, the aerosols are accelerated to a speed sufficient to cause large aerosol particles outside of the sampling range to fall out of the flow, while particles within of the sampling range are deposited onto a filter within the cyclone sampler pack. By contrast, a cascade sampler pack will contain multiple collection stages arranged in series, with each collection stage having an orifice plate and a separate, removable collection surface below the orifices. With each successive stage, the orifice cross-sectional areas decrease in order to increase the velocity of the aerosol-laden air, and only particles small enough to remain within the flow pass to the next stage, while particles within the cut point range of the current stage are deposited. Example sampler packs include the Sioutas Personal Cascade Impactor and the Respirable Dust Aluminum Cyclone, each by SKC, Inc. Though not shown, the sensor assembly 52 can include an aerodynamic particle sizer (spectrometer) for independently sizing the aerosols.

[0024] As alternatively shown in FIGS. 4-5, a test enclosure in accordance with a further embodiment is illustrated and generally designated 60. The test enclosure 60 is positioned on a load frame 110 between two columns 112, 114, and the load apparatus and the aerosol sampling pack are contained within the test enclosure 60. The test enclosure 60 includes a base platform 62, a four-sided back frame 64, and a four-sided front frame 66. The front frame 66 is joined to back frame 64 along first and second hinges 68, such that the front frame 66 can open for access to the interior of the test enclosure 60. The front frame 66 includes a viewing window 70, the viewing window optionally being formed from ballistic glass. The front and rear frames 64, 66 are formed from aluminum, but can be formed from other materials in other embodiments.

[0025] The load frame 110 extends into the interior of the test enclosure 60 via a lower opening in the base platform 62 and via an upper opening 72 defined between the back frame 64 and the front frame 66. The test enclosure 60 also includes a system for rinsing the inside walls of the test enclosure. The system for rinsing the inside walls can include one or more atomizing spray nozzles 80 and a rinse collection tray 82. The spray nozzles 80 are supported near the uppermost portion of the test enclosure 60 and are oriented toward the enclosure sidewalls to avoid spraying the test specimen. Each spray nozzle 80 provides a desired spray pattern, for example a solid cone spray pattern, a hollow cone spray pattern, or a tapered-edge flat spray pattern. The rinsing liquid, for example water or alcohol, can be directed into a funnel (not shown) at the base of the test enclosure and drained to a collection bottle, which may also be sampled for particulates.

[0026] As also shown in FIG. 6, the test enclosure 60 houses a load apparatus. The load apparatus includes a fixed cross-member 40 and a moving cross-member 42 for providing a four-point bending load. The load apparatus can be modified in other embodiments to provide essentially any bending load, torsion load, compressive load, shear load, or tensile load. The fixed cross-member 40 is even with the viewing window 70. To provide aerosol sampling, at least one sensor assembly 52 (shown in FIG. 3) is contained within the test enclosure 60, optionally two or more sensor assemblies, further optionally three sensor assemblies. Each sensor assembly 52 includes an aerosol sampling pack 44, a vacuum pump 46, and a power supply 48. The sensor assemblies 52 are modular, such that each sensor assembly 52 can be replaced between fracture tests. The test enclosure 60 can also include a gas inlet 84 at the base of the enclosure for providing an inert gas under positive pressure. For example, the gas inlet 84 can provide a slow inert gas flow to ensure that the gas in the test enclosure remains mixed.

[0027] As further optionally shown in FIGS. 6-7, a system for sampling aerosols from fractured fuel rods is illustrated. The system in this embodiment is intended to sample uranium dioxide or solid fission product particles in the fission and fill gases of a fractured fuel rod if released through a breach in the fuel rod cladding. The test enclosure 90 is contained within a hot cell 120 and is formed from transparent, shatterproof material, for example ballistic glass. Inert gas is forced into the test enclosure 90 (from gas source 88) under positive pressure to agitate the aerosols, which are drawn into the aerosol sampler 44 via the sampler conduit 54. Though not shown, a vacuum pump can be positioned within the hot cell 120 to draw aerosols into the aerosol sampler 44 in the manner set forth above in connection with FIGS. 1-5. The load mechanism in this embodiment includes first and second rotary motors 92, 94 that provide flexure to the test specimen 100. The load mechanism further optionally imparts vibrations on the test specimen 100, also leading to fracture and the generation of aerosols for collection and analysis by the aerosol sampler 44.

[0028] These and other embodiments are configured to sample any solid phase aerosols released from a test specimen as it is fractured. As noted above in connection with FIGS. 6-7, the present invention can be used to sample aerosols that are released from fractured fuel rods to estimate the quantity of radioactive aerosol material that would be released if a spent commercial power rod were fractured in a transportation accident. The present invention is also well suited for applications where it is desirable to define the respirable fraction of aerosols resulting from particular actions, such as the manufacture of a part by impact (e.g., by forging), housing industry tasks (e.g., remediation or replacement of insulation or piping components), or breaking down cardboard for recycling. The present invention is also well suited for use by industrial laboratories specializing in aerosol collection and characterization, for example, the characterization of aerosols produced by medical inhalers.

[0029] The above description is that of current embodiments of the invention. Various alterations and changes can be made without departing from the spirit and broader aspects of the invention as defined in the appended claims, which are to be interpreted in accordance with the principles of patent law including the doctrine of equivalents. This disclosure is presented for illustrative purposes and should not be interpreted as an exhaustive description of all embodiments of the invention or to limit the scope of the claims to the specific elements illustrated or described in connection with these embodiments. For example, and without limitation, any individual element(s) of the described invention may be replaced by alternative elements that provide substantially similar functionality or otherwise provide adequate operation. This includes, for example, presently known alternative elements, such as those that might be currently known to one skilled in the art, and alternative elements that may be developed in the future, such as those that one skilled in the art might, upon development, recognize as an alternative. Further, the disclosed embodiments include a plurality of features that are described in concert and that might cooperatively provide a collection of benefits. The present invention is not limited to only those embodiments that include all of these features or that provide all of the stated benefits, except to the extent otherwise expressly set forth in the issued claims. Any reference to claim elements in the singular, for example, using the articles a, an, the or said, is not to be construed as limiting the element to the singular.