US3919757A - Method of fabricating a vent structure containing separating particles - Google Patents

Method of fabricating a vent structure containing separating particles Download PDF

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US3919757A
US3919757A US473448A US47344874A US3919757A US 3919757 A US3919757 A US 3919757A US 473448 A US473448 A US 473448A US 47344874 A US47344874 A US 47344874A US 3919757 A US3919757 A US 3919757A
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tubing
vent
vent structure
flattening
pressing
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US473448A
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Joseph C Mcguire
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McDonnell Douglas Corp
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McDonnell Douglas Corp
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    • GPHYSICS
    • G21NUCLEAR PHYSICS; NUCLEAR ENGINEERING
    • G21CNUCLEAR REACTORS
    • G21C3/00Reactor fuel elements and their assemblies; Selection of substances for use as reactor fuel elements
    • G21C3/02Fuel elements
    • G21C3/04Constructional details
    • G21C3/041Means for removal of gases from fuel elements
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23PMETAL-WORKING NOT OTHERWISE PROVIDED FOR; COMBINED OPERATIONS; UNIVERSAL MACHINE TOOLS
    • B23P11/00Connecting or disconnecting metal parts or objects by metal-working techniques not otherwise provided for 
    • GPHYSICS
    • G21NUCLEAR PHYSICS; NUCLEAR ENGINEERING
    • G21CNUCLEAR REACTORS
    • G21C7/00Control of nuclear reaction
    • G21C7/06Control of nuclear reaction by application of neutron-absorbing material, i.e. material with absorption cross-section very much in excess of reflection cross-section
    • G21C7/08Control of nuclear reaction by application of neutron-absorbing material, i.e. material with absorption cross-section very much in excess of reflection cross-section by displacement of solid control elements, e.g. control rods
    • G21C7/10Construction of control elements
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02EREDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E30/00Energy generation of nuclear origin
    • Y02E30/30Nuclear fission reactors
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00Metal working
    • Y10T29/49Method of mechanical manufacture
    • Y10T29/496Multiperforated metal article making
    • Y10T29/49604Filter
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00Metal working
    • Y10T29/49Method of mechanical manufacture
    • Y10T29/49826Assembling or joining
    • Y10T29/49945Assembling or joining by driven force fit

Definitions

  • a vent assembly including the vent structure UNITED STATES PATENTS and providing an air lock between the outer molten 7 815 889 UN) St I I 38/47 UX sodium and the vent is affixed to the upper end of 1., e 2 B a 3,274,066 9/1966 Zumwalt 176/68 each Comm 3.315.336 4/1967 Parker et al .1 29/1635 F 7 Claims, 11 Drawing Figures ⁇ 5 R A 46- 7% g US Patent Nov. 18, 1975 Sheet 1 of4 3,919,757
  • My present invention pertains generally to venting devices. More particularly, the invention relates to a very effective and practical vent structure for use in the control pins of a liquid metal fast breeder reactor (LMFBR), for example, and to a novel method of fabricating the vent structure.
  • LMFBR liquid metal fast breeder reactor
  • helium is generated in the LMFBR control pins as the result of a neutron, alpha (n, a) reaction on boron (B).
  • This helium is generated in each pin up to the rate of 3 cc/hr or 72 cc/day volume at standard temperature and pressure (STP). If all of this generated gas is released from the boron carbide (B C) matrix of a control pin, the resulting 26 liters per year poses a serious containment and pressure problem using closed control pins, especially since sudden onsets of extreme pressure could develop during the reactor power cycles.
  • the use of open control pins allows the boron carbide to come into direct contact with the high temperature sodium (Na) liquid metal coolant with the resulting attack thereon and likelihood of boron contamination of the coolant.
  • my invention is prefera bly accomplished by providing a vent structure, including a ductile and relatively thin wall tubing having an undeforrned normally lower portion and a flattened and folded (double coiled and pressed) normally upper portion, in a molten sodium coolant reactor gas generating control pin, for example, to release its generated gas normally at a relatively low flow rate such that the control pin (gas container) is maintained in a slightly pressurized state to prevent backflovv of molten sodium or vapor and consequential contamination thereof.
  • a vent structure including a ductile and relatively thin wall tubing having an undeforrned normally lower portion and a flattened and folded (double coiled and pressed) normally upper portion, in a molten sodium coolant reactor gas generating control pin, for example, to release its generated gas normally at a relatively low flow rate such that the control pin (gas container) is maintained in a slightly pressurized state to prevent backflovv of molten sodium or vapor and consequential contamination thereof.
  • the formed (flattened and folded) upper portion of the vent structure preferably includes a thin film or layer of fine alumina particles between the flattened opposing faces inside the tubing, to prevent the vent from sintering together due to grain growth across the faces occurring at high temperatures and long term operation.
  • the vent structure preferably further includes a particulate filter in the undeformed lower portion of the vent tub-
  • the method of fabricating the vent structure includes the steps, among others, of annealing a metal tubing of predetermined length and size at a predetermined temperature for a predetermined period, uniformly filling the tubing with fine alumina particles, flattening an upper portion of the tubing and then coiling and pressing such upper portion at predetermined pressures, and again annealing the tubing at a predetermined temperature for a predetermined period. Finally, a porous metal particulate filter can be press-fitted into the undeformed lower portion of the tubing.
  • the resultant vent structure is structurally stable and can operate reliably in a high temperature environment over a long term, and gas flow thereof is substantially a linear function of the applied gas pressure differential up to the point where the elastic limit of the metal tubing is reached.
  • a vent assembly including the vent structure and providing an air lock between the outer molten sodium and vent structure is attached to each pin to ensure that liquid sodium does not directly contact the vent.
  • the vent assembly includes an adapter plug mounting the lower end of the vent structure, cover structure attached to the plug and forming an air lock chamber housing the part of the vent structure above the plug, and a baffle made of porous metal provided in the chamber space between the upper portion of the vent structure and a number of small bleed holes in the cover structure.
  • the adapter plug is shaped to be suitably attached to the upper end of a control pin, and the baffle allows free passage of gas while preventing the passage of particulate matter and impeding the passage of molten sodium.
  • the possibility of sodium backflow is virtually eliminated by use of the air lock and the anti-splash porous metal baffle.
  • FIG. I is an elevational view, shown in section, of a vent assembly which is to be affixed to the normally upper end of a reactor control pin;
  • FIG. 2 is a fragmentary elevational view, shown in section and enlarged, of a vent structure constructed according to this invention
  • FIG. 3 is a graph showing a plot of helium pressure versus helium flow rate of the vent structure
  • FIG. 4 is a graph showing plots of vent temperature versus helium flow rate of two vent structures having nominally different helium release rates
  • FIG. 5 is a graph showing plots of thermal cycles versus helium flow rate at the low and high temperature limits of the thermal cycles
  • FIGS. 6A, 6B, 6C, 6D and 6E illustrate certain main steps in a method of fabricating the vent structure
  • FIG. 7 is a flow chart illustrating a process of producing the vent assembly.
  • FIG. I is an elevational view, shown in section, of the upper vent assembly 10 of a control pin I2 which is used, for example, in a liquid metal (sodium) cooled fast breeder nuclear reactor (not shown).
  • the control pin 12 and its upper vent assembly 10 are normally fully immersed deeply in (under approximately 8 feet of) the molten sodium reactor coolant operating at temperatures of about 900 to ll00F.
  • Each control pin 12 contains a series of boron carbide pellets (not shown) and is a source of generated helium.
  • the vent assembly 10 is, of course, hermetically attached to the upper end of the control pin 12 and generally includes a vent adapter plug 14, baffle l6, air lock tube 18, air lock cap 20, and vent structure 22.
  • the vent plug 14, air lock tube 18, and air lock cap are preferably made of a material similar to that of the control pin 12 structural material such as Type 316 stainless steel, which is compatible with a hot sodium (liquid and vapor) environment.
  • Baffle 16 is made of a porous metal which is resistant to attack by hot sodium.
  • a felt or foam metal can be used and, in the exemplary vent assembly 10, a Type F-3l5 nickel felt metal produced by l-luyck Metals Corporation was used. This material is about 20% dense and allows free passage of gas while preventing the passage of particulate matter and impeding any passage of molten sodium.
  • the air lock tube 18 has, for example, four vent or bleed holes 24 which can be 0.0]35 inch in diameter equiangularly spaced 90 degrees about the air lock tube at a predetermined distance above the lower end thereof.
  • the vent plug 14 has an axially drilled central hole 26 and the baffle 16 also has an axially punched central hole 28.
  • the punched baffle 16 is packed on the vent structure 22 against the upper surface 30 of the vent plug 14 which is joined at its lower end 32 to the lower end of the vent structure by a standing lip electron-beam weld for maximum'cleanliness and minimal disturbance of the surrounding metal.
  • vent holes 24 are located slightly above the upper surface 30 of the vent plug and directly adjacent to the lower side surface of the baffle 16.
  • Welding of the air lock cap 20 to the upper end of the air lock tube 18 forms an air lock chamber 36 containing cover gas which provides an air lock" effect over the vent structure 22 such that liquid sodium does not directly or normally contact the upper vent end 38.
  • the possibility of sodium backflow is virtually eliminated by use of the air lock chamber 36 and the anti-splash porous metal baffle 16 in the vent assembly 10 of control pin 12.
  • the air lock chamber 36 is a plenum chamber which is made large enough to provide a sufficie nt reservoir of gas that prevents liquid sodium which might enter the lower bleed holes 24 and into the battle 16, as in the event of any sudden fluctuation (loss) in gas pressure due to a temporary reactor temperature change (drop), from ever reaching the vent opening in the upper vent end 38 of the vent structure 22.
  • the sodium is subsequently forced out of the chamber 36 following the temperature change as the gas pressure therein builds up to equalize with the environmental (8 feet of liquid sodium) pressure.
  • the bleed holes 24 are made adequately small so that they will not admit the surge of liquid sodium into the air lock chamber 36, which surge can occur when the control pin 12 is first immersed in the sodium.
  • the bleed holes 24 are made adequately large mainly for convenience of drilling very small holes in stainless steel with the presently available drills and methods.
  • the combined size of the bleed holes 24 must be about equal or (and are vastly) larger than the effective size of the vent discharge opening in the upper vent end 38 of the vent structure 22, and allows gas to escape from the chamber 36 at about the rate that it is being released from the vent structure.
  • the vent assembly 10 has general overall dimensions of length A, diameter B, and an approximate gas space length C (connected through vent holes 24 to the exte- 4 rior). Illustrative values for these dimensions are A of 1.80 inches, B of 0.435 inch (maximum), and C of 0.95 inch, for example.
  • This vent assembly 10 is, of course, to be welded to the upper end of the stainless steel tube (control pin 12) having a 0.395 inch inside diameter which accomodates the lower portion of vent plug 14.
  • Other dimensions of the vent assembly 10 can be proportionately estimated adequately from the elevational view of FIG. 1 and, while approximate, will suffice for most purposes.
  • the vent has a gas flow rate sufficient to maintain pressure in the air lock chamber 36 and in control pin 12 to prevent backflow of sodium and any possibly contaminating outside cover gas, respectively.
  • FIG. 2 is a fragmentary elevational view, shown somewhat enlarged in section, of the vent structure 22.
  • the vent structure 22 includes a thin wall tubing 40 having an undeformed lower portion 42, and a flattened and folded (coiled or rolled and pressed) upper portion 44.
  • the flattened upper portion 44 is preferably folded at least twice, as shown.
  • a particulate filter 46 is provided in the lower portion 42 of the tubing 40, and a film or layer 48 of fine particles or powder is provided between the pressed opposing surfaces inside the upper portion 44.
  • the tubing 40 can be made of any material sufficiently ductile to survive the flattening, coiling and pressing operations without cracking, and there are appropriate materials readily available for operation or use under a very wide range of environmental and temperature conditions.
  • the tubing 40 can be made of the same material as the control pin 12 structural material.
  • the tubing 40 can be made of Type 3 l6 stainless steel having an inside diameter D and an outside diameter E as indicated in FIG. 2.
  • the particulate filter 46 can be made of Type F-3 l5 nickel felt metal similar to that of bafile 16 (FIG. I) and having a length F.
  • the cylindrically shaped filter 46 can be installed in the lower portion 42 by press-fitting it into the tubing 40 to a position approximately as illustrated.
  • Exemplary dimensions for the inside diameter D, outside diameter E, and length F are respectively 0.093, (H25, and 0.250 inch, for example.
  • the formed upper portion 44 of the exemplary vent structure 22 has a length G and a thickness H as indicated in FIG. 2.
  • the film or layer 48 can consist essentially of, for example, compacted 0.3 micron diameter aluminum oxide (A1 0 particles. This particle size could be increased to as large as 1 micron or reduced to as small as 0.05 micron for satisfactory operation. A particle size larger than 1 micron would provide individual support points during forming (flattening and pressing) of the upper portion 44 and which may prevent the attainment of low gas flow rates. Of course, a particle size smaller than 0.05 micron may not prevent eventual grain growth across the proximate faces of a flattened tube at high temperatures.
  • vent structure 22 in regular long term and high temperature operations, it is possible for the fonned upper portion 44 of the vent structure to sinter together.
  • the formed vent structure 22, with or without the layer 48 of alumina particles can be used independently as a gas flow metering device in various applications following suitable flow calibration thereof.
  • the illustrative dimensions for the length G and thickness H are respectively about 0.350 and 0.092 inch, for example.
  • the thickness of the film or layer 48 can be approximately 0.005 inch, when pressed, although the layer thickness in the exemplary vent structure 22 can be generally between 0.003 and 0.007 inch for satisfactory operation.
  • Exact pressing parameters and anneal conditions are functions of the particular size and wall thickness of the tubing 40 used and the desired gas flow rate. The method of fabricating the vent structure 22 will be described later, following a discussion of certain test results thereof.
  • FIGS. 3, 4 and 5 are graphs showing respective plots of helium pressure versus helium flow rate of the vent structure 22, vent temperature versus helium flow rate at 1 atmosphere pressure differential, and thermal cycles versus helium flow rate wherein the cycle period was two minutes from high temperature to low temperature.
  • the curve 50 of FIG. 3 illustrates that a substantially linear relationship exists in the response in helium flow rate of the vent structure 22 to change in helium pressure. As indicated in FIG. 3, helium flow rate drops linearly as the driving pressure decreases.
  • Curve 52 of FIG. 4 illustrates helium release rates of the vent structure 22 as a function of its temperature while maintaining a pressure differential of l atmosphere for the vent structure. Flow rate is, of course, lower at the higher temperatures since there are less gas molecules in a fixed volume at such temperatures with the maintained pressure differential.
  • Curve 54 of FIG. 4 illustrates helium release rates of another vent structure as a function of its temperature at a pressure differential of 1 atmosphere, the vent structure being similar to vent structure 22 but formed to provide a nominally higher flow rate.
  • curve 56 depicts the helium flow rate at the low temperature of 375F and curve 58 depicts such flow rate at the high temperature of ll30F.
  • the vent structure 22 With the helium generation rate per control pin 12 (FIG. 1) at approximately 3 cc/hr, the vent structure 22 provides an average helium diffusion rate of about 0.61 cc/hr at one atmosphere pressure differential after 60 thermal cycles (FIG. 5). This allows a helium pressure of approximately 4 atmospheres inside the control pin 12 to provide a two-fold advantage.
  • pressurized helium has a higher thermal conductivity to dissipate radiation heating in the control pin and, second, the pressure minimizes any possibility of back diffusion of either sodium vapor or cover gas into the control pin.
  • the positive helium pressure maintained in the control pin 12 by the vent structure 22 can drop by a factor of about 2 without compromising the sodium seal provided.
  • FIGS. 6A through 6E illustrate certain main steps in the method of fabricating the vent structure 22.
  • the tubing 40 following ultrasonic inspection of a Type 3 l 6 stainless steel tubing 40 of 0. I25 OD. and 0.0l6 inch wall, the tubing is cut to a predetermined length and vacuum annealed l5 minutes at 1900F, for example. Austenitic stainless steel is virtually unaffected by pure hot sodium at temperatures below 1000F. In the region between l000 and l500F, however, there is evidence of some measurable attack, particularly at the grain boundaries. Based on this constraint, the vent tubing 40 wall thickness was selected to be 0.016 inch to provide a safety factor of at least 3 over the deepest sodium penetration observed at 1500F.
  • the annealed tubing 40 is then uniformly filled loosely with alumina particles of a generally predetermined size as, for example, 0.3 micron diameter. Tamping is unnecessary and it is not critical that the tubing 40 be very uniformly filled. A light shaking of the tubing 40 during filling ordinarily suffices. In fact, one way to fill the tubing 40 is simply to push it into a jar of alumina.
  • a predetermined length of the filled tubing 40 is then flattened in, for example, a Carver hydraulic press at a predetermined flattening pressure.
  • the flattened tubing 40 is illustrated in FIG. 6B.
  • the flattened portion of tubing 40 is next formed by rolling it into a two-bend spiral as shown in FIG. 6C, and a final pressing operation is performed thereon at a predetermined pressing pressure.
  • the compacted alumina throughout the vent wall interface eliminates the operational sintering tendency due to grain growth across the faces of the flattened tubing 40 at high temperatures.
  • the formed tubing 40 is then preferably vacuum annealed l5 minutes at l900F again.
  • a particulate filter 46 is finally press-fitted into the formed tubing 40 as indicated in FIG. 6E to complete the vent structure 22.
  • the formed tubing 40 is preferably annealed particularly where the vent structure 22 is used in high temperature (600C or I l 12F) operation because flow rate doubles in the vent structure going from a stressed to annealed condition and operating at the high temperature of 600C, the vent will self-anneal over a period of 3 weeks.
  • the alumina or aluminum oxide powder is compatible with any vent tubing material and is uniquely suited for operation in the presence of hot sodium vapor. It is an extremely stable oxide and is the only commonly processed oxide resistant to attack by hot sodium and sodium vapor. As mentioned previously, however, exact pressing parameters (and anneal conditions) are a function of the particular size and wall thickness of the vent tubing used and the desired gas flow rate. In the flattening and pressing operations required on the particular vent tubing 40 of 0. inch OD. and 0.016 inch wall, air flow rate at 15 psi differential pressure is illustratively varied according to flattening and pressing pressures as indicated below.
  • gas flow rate through the vent structure 22 is also dependent upon the nature of the gas. As vents are made for lower and lower flow rates, this difference becomes more significant as indicated below.
  • the vent structure 22 can be fabricated for any required flow down to, for example, 0.0036 cc/hr helium at one atmosphere pressure differential. Also, flow through the vent structure 22 can increase greatly in case of a sudden increase in helium pressure within the control pin 12. Thus, the vent structure 22 effectively acts to relieve pressure transients in the control pin 12 to prevent any possible ruptures thereof and then returns by natural springback to normal operation if the elastic limit of the formed tubing 40 has not been exceeded.
  • the illustrative vent structure 22 has been tested and found good to over 3500 psi, for example.
  • FIG. 7 is a flow chart illustrating a process of producing the vent assembly 10 (FIG. 1).
  • the Type 316 stainless steel tubing 40 is provided in a step 60, for example.
  • the tubing 40 is checked for proper dimensional tolerances and ultrasonically inspected in step 62, so that it can be certified free from flaws.
  • the tubing 40 is cut to length and ultrasonically cleaned in Freon, for example, in step 64.
  • the cut tubing 40 is next vacuum annealed minutes at l900F in step 66.
  • the annealed tubing 40 is formed in step 68 according to the method shown and described above with respect to FIGS. 6A through 6E.
  • the formed tubing 40 is preferably vacuum annealed 15 minutes at l900F as indicated in step 70 and calibrated for flow in the next step 72.
  • Each formed vent is tested and individually characterized for helium flow in standard cc per hour measuring actual pressure rise in a vacuum system of calibrated volume with helium on the inlet side provided at 760 torr. These tests also serve as the fiow acceptance test for each vent.
  • the unpressed section (lower portion 42 in FIG. 2) of tubing 40 can include the particulate filter 46 which allows free passage of gas.
  • nickel felt metal can be used as indicated in step 74.
  • a foamed instead of felt metal can be used and the metal can be stainless steel instead of nickel, for example, since such materials are resistant to attack by hot sodium and allow free passage of gas.
  • a filter disc or discs of appropriate size can be punched out from the nickel felt metal in step 78 and the disc filter inspected in step 80.
  • Bafile 16 can be fabricated from stainless steel foam metal as indicated in step 82.
  • This baffle material can, of course, be nickel instead of stainless steel and felt in stead of foam metal. Indeed, it is usually convenient and preferable that the baffle 16 and filter 46 be made of the same identical material.
  • the foam metal is punched or otherwise shaped to size and configuration in step 86.
  • the shaped baffle 16 is inspected in step 88.
  • the vent adapter plug 14, air lock tube 18 and air lock cap 20 can be shaped from a Type 316 stainless steel rod provided in step and inspected in step 92.
  • the plug 14, tube 18 and cap 20 can be machined to size and shape in step 94 from the stainless steel rod, and the finished products inspected in step 96. It is, of course, apparent that the formed tubing 40, filter 46, baffle 16, adapter plug 14, air lock tube 18 and air lock cap 20 can be fabricated in any elected sequence or all concurrently.
  • the particulate filter 46 is packed into the formed tubing 40 to complete vent structure 22 and the baffle 16 is packed onto the formed tubing in step 98.
  • the adapter plug 14 is installed on the vent structure 22 against the lower surface of the baffle 16 and is joined at its lower end 32 to the lower end of the vent structure by a standing lip electron-beam weld in step 100.
  • a helium leak check is made of the electron-beam weld in step 102, and the air lock cap 20 is tungsten-inert-gas (TlG) or electronbeam welded to the air lock tube 18 with its vent holes 24 (FIG. 1) located at the opposite end away from the cap in step 104.
  • the air lock tube 18 is then TlG welded to the adapter plug 14 in step 106 to complete vent assembly 10, and acceptance tests are performed thereon in step 108.
  • Completed assemblies can be packaged in plastic bags and sealed for delivery.
  • a method of fabricating a vent structure which comprises the steps of:
  • the invention as defined in claim 1 further comprising the step of initially annealing said tubing at a predetermined temperature for a predetermined time prior to flattening of said upper tubing portion.

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  • Physics & Mathematics (AREA)
  • Plasma & Fusion (AREA)
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Abstract

A vent structure for reliable long term operation at high temperatures is fabricated by annealing a tubing of predetermined length and size, filling the tubing with fine alumina particles, flattening and coiling and pressing an upper portion of the tubing at predetermined pressures, annealing the formed tubing, and installing a particulate filter in the undeformed lower portion of the tubing. For use in venting helium generating reactor control pins located under hot molten sodium, a vent assembly including the vent structure and providing an air lock between the outer molten sodium and the vent is affixed to the upper end of each control pin.

Description

United States Patent McGuire Nov. 18, 1975 [54] METHOD OF FABRICATING A VENT 3.406.094 10/1968 Beisswenger et 211. 176/68 X STRUCTURE CONTAINING SEPARATING g amp e PARTICLES 3.677.300 7/1972 King 138/42 [75] Inventor: Joseph C. McGuire, Kennewick. 3.697.377 lO/l972 Gauthron .1 176/68 Wash 3.708.858 H1973 Sasaki 1. 39/1615 F 3.801.447 4/1974 Heenan 1 1 1 176/36 R [73] Asslgneer McDonnell D gl s p n, 3.838.557 10/1974 McGuire 55/385 Long Beach, Calif. 22 pl M 28, 1974 Primary Emnziner-C W. Lanham 1 1e ay Assistant Eramirzer-D. Cv Reiley, 111 PP N04 473,448 Attorney. Age/11. or Firn1-D. N. .leu; Walter J. Jason;
Related US. Application Data Donald Royer [62] Ser. No. 296.680. Oct. 11. 1972. Pat. No. ABSTRACT A vent structure for reliable long term operation at 52 11.5. CI. 29/1635 F; 29/420; 29/525; high temperatures is fabricated y annealing tubing 17 3; 176/86 R of predetermined length and size. filling the tubing [51] Int. Cl B23p 15/16 with fine alumina P flattening and Coiling and 58 Field of Search 29/1635 F, 420, 01G. 31. Pressing upper Portion of the tubing at predeter- 29/4709 525; 55/331 432 525 10 9; mined pressures, annealing the formed tubing, and in- 133/42 146; 220/371 372 373 374; stalling a particulate filter in the undeformed lower 17 3 A portion of the tubing. For use in venting helium generating reactor controlpins located under hot molten [5 References Cited sodium, a vent assembly including the vent structure UNITED STATES PATENTS and providing an air lock between the outer molten 7 815 889 UN) St I I 38/47 UX sodium and the vent is affixed to the upper end of 1., e 2 B a 3,274,066 9/1966 Zumwalt 176/68 each Comm 3.315.336 4/1967 Parker et al .1 29/1635 F 7 Claims, 11 Drawing Figures \5 R A 46- 7% g US Patent Nov. 18, 1975 Sheet 1 of4 3,919,757
Ala/0M PRESSURE s!) il'lii'r U.S. Patent Nov. 18, 1975 Sheet 2 014 3,919,757
40 HEL/UM FLOW ONE ATMOSPHERE (STD CC/HR) PRESSURE D/FFERE/V TIA L 30 a 1 l I 1/5/1/7' TEMPERA TURE [7-7 as MEL/UM x-zow 870 cc #1? T/lER/l/IAL CYCL ES US. Patent 'Nov. 18,1975 Sheet3of4 3,919,757
U.S. Patent Nov. 18, 1975 Sheet 4 of4 3,919,757
METHOD OF FABRICATING A VENT STRUCTURE CONTAINING SEPARATING PARTICLES This is a division of application Ser. No. 296,680 filed Oct. ll, 1972 and now U.S. Pat. No. 3,876,403.
BACKGROUND OF THE INVENTION My present invention pertains generally to venting devices. More particularly, the invention relates to a very effective and practical vent structure for use in the control pins of a liquid metal fast breeder reactor (LMFBR), for example, and to a novel method of fabricating the vent structure.
As is well known, helium (He) is generated in the LMFBR control pins as the result of a neutron, alpha (n, a) reaction on boron (B). This helium is generated in each pin up to the rate of 3 cc/hr or 72 cc/day volume at standard temperature and pressure (STP). If all of this generated gas is released from the boron carbide (B C) matrix of a control pin, the resulting 26 liters per year poses a serious containment and pressure problem using closed control pins, especially since sudden onsets of extreme pressure could develop during the reactor power cycles. Conversely, the use of open control pins allows the boron carbide to come into direct contact with the high temperature sodium (Na) liquid metal coolant with the resulting attack thereon and likelihood of boron contamination of the coolant.
SUMMARY OF THE INVENTION Briefly, and in general terms, my invention is prefera bly accomplished by providing a vent structure, including a ductile and relatively thin wall tubing having an undeforrned normally lower portion and a flattened and folded (double coiled and pressed) normally upper portion, in a molten sodium coolant reactor gas generating control pin, for example, to release its generated gas normally at a relatively low flow rate such that the control pin (gas container) is maintained in a slightly pressurized state to prevent backflovv of molten sodium or vapor and consequential contamination thereof. The formed (flattened and folded) upper portion of the vent structure preferably includes a thin film or layer of fine alumina particles between the flattened opposing faces inside the tubing, to prevent the vent from sintering together due to grain growth across the faces occurring at high temperatures and long term operation. The vent structure preferably further includes a particulate filter in the undeformed lower portion of the vent tub- The method of fabricating the vent structure includes the steps, among others, of annealing a metal tubing of predetermined length and size at a predetermined temperature for a predetermined period, uniformly filling the tubing with fine alumina particles, flattening an upper portion of the tubing and then coiling and pressing such upper portion at predetermined pressures, and again annealing the tubing at a predetermined temperature for a predetermined period. Finally, a porous metal particulate filter can be press-fitted into the undeformed lower portion of the tubing. The resultant vent structure is structurally stable and can operate reliably in a high temperature environment over a long term, and gas flow thereof is substantially a linear function of the applied gas pressure differential up to the point where the elastic limit of the metal tubing is reached.
For use in venting helium generating reactor control pins located under a corrosive and reactive liquid environment such as molten sodium, a vent assembly including the vent structure and providing an air lock between the outer molten sodium and vent structure is attached to each pin to ensure that liquid sodium does not directly contact the vent. The vent assembly includes an adapter plug mounting the lower end of the vent structure, cover structure attached to the plug and forming an air lock chamber housing the part of the vent structure above the plug, and a baffle made of porous metal provided in the chamber space between the upper portion of the vent structure and a number of small bleed holes in the cover structure. The adapter plug is shaped to be suitably attached to the upper end of a control pin, and the baffle allows free passage of gas while preventing the passage of particulate matter and impeding the passage of molten sodium. The possibility of sodium backflow is virtually eliminated by use of the air lock and the anti-splash porous metal baffle.
BRIEF DESCRIPTION OF THE DRAWINGS My invention will be more fully understood, and other advantages and features thereof will become apparent, from the following description of an exemplary embodiment and method of the invention. The description is to be taken in conjunction with the accompanying drawings, in which:
FIG. I is an elevational view, shown in section, of a vent assembly which is to be affixed to the normally upper end of a reactor control pin;
FIG. 2 is a fragmentary elevational view, shown in section and enlarged, of a vent structure constructed according to this invention;
FIG. 3 is a graph showing a plot of helium pressure versus helium flow rate of the vent structure;
FIG. 4 is a graph showing plots of vent temperature versus helium flow rate of two vent structures having nominally different helium release rates;
FIG. 5 is a graph showing plots of thermal cycles versus helium flow rate at the low and high temperature limits of the thermal cycles;
FIGS. 6A, 6B, 6C, 6D and 6E illustrate certain main steps in a method of fabricating the vent structure; and
FIG. 7 is a flow chart illustrating a process of producing the vent assembly.
DESCRIPTION OF THE PRESENT EMBODIMENT AND METHOD In the following description and accompanying drawings of an illustrative embodiment and method of my invention, some specific dimensions and types of materials are disclosed. It is to be understood, of course, that such dimensions and types of materials are given as examples only and are not intended to limit the scope of this invention in any manner.
FIG. I is an elevational view, shown in section, of the upper vent assembly 10 of a control pin I2 which is used, for example, in a liquid metal (sodium) cooled fast breeder nuclear reactor (not shown). The control pin 12 and its upper vent assembly 10 are normally fully immersed deeply in (under approximately 8 feet of) the molten sodium reactor coolant operating at temperatures of about 900 to ll00F. Each control pin 12 contains a series of boron carbide pellets (not shown) and is a source of generated helium. The vent assembly 10 is, of course, hermetically attached to the upper end of the control pin 12 and generally includes a vent adapter plug 14, baffle l6, air lock tube 18, air lock cap 20, and vent structure 22.
The vent plug 14, air lock tube 18, and air lock cap are preferably made of a material similar to that of the control pin 12 structural material such as Type 316 stainless steel, which is compatible with a hot sodium (liquid and vapor) environment. Baffle 16 is made of a porous metal which is resistant to attack by hot sodium. A felt or foam metal can be used and, in the exemplary vent assembly 10, a Type F-3l5 nickel felt metal produced by l-luyck Metals Corporation was used. This material is about 20% dense and allows free passage of gas while preventing the passage of particulate matter and impeding any passage of molten sodium.
The air lock tube 18 has, for example, four vent or bleed holes 24 which can be 0.0]35 inch in diameter equiangularly spaced 90 degrees about the air lock tube at a predetermined distance above the lower end thereof. The vent plug 14 has an axially drilled central hole 26 and the baffle 16 also has an axially punched central hole 28. The punched baffle 16 is packed on the vent structure 22 against the upper surface 30 of the vent plug 14 which is joined at its lower end 32 to the lower end of the vent structure by a standing lip electron-beam weld for maximum'cleanliness and minimal disturbance of the surrounding metal.
When the lower end of the air lock tube 18 is welded to flange 34 of the vent plug 14, the vent holes 24 are located slightly above the upper surface 30 of the vent plug and directly adjacent to the lower side surface of the baffle 16. Welding of the air lock cap 20 to the upper end of the air lock tube 18 forms an air lock chamber 36 containing cover gas which provides an air lock" effect over the vent structure 22 such that liquid sodium does not directly or normally contact the upper vent end 38. The possibility of sodium backflow is virtually eliminated by use of the air lock chamber 36 and the anti-splash porous metal baffle 16 in the vent assembly 10 of control pin 12.
The air lock chamber 36 is a plenum chamber which is made large enough to provide a sufficie nt reservoir of gas that prevents liquid sodium which might enter the lower bleed holes 24 and into the battle 16, as in the event of any sudden fluctuation (loss) in gas pressure due to a temporary reactor temperature change (drop), from ever reaching the vent opening in the upper vent end 38 of the vent structure 22. Of course, the sodium is subsequently forced out of the chamber 36 following the temperature change as the gas pressure therein builds up to equalize with the environmental (8 feet of liquid sodium) pressure.
The bleed holes 24 are made adequately small so that they will not admit the surge of liquid sodium into the air lock chamber 36, which surge can occur when the control pin 12 is first immersed in the sodium. On the other hand, the bleed holes 24 are made adequately large mainly for convenience of drilling very small holes in stainless steel with the presently available drills and methods. In any event, the combined size of the bleed holes 24 must be about equal or (and are vastly) larger than the effective size of the vent discharge opening in the upper vent end 38 of the vent structure 22, and allows gas to escape from the chamber 36 at about the rate that it is being released from the vent structure.
The vent assembly 10 has general overall dimensions of length A, diameter B, and an approximate gas space length C (connected through vent holes 24 to the exte- 4 rior). Illustrative values for these dimensions are A of 1.80 inches, B of 0.435 inch (maximum), and C of 0.95 inch, for example. This vent assembly 10 is, of course, to be welded to the upper end of the stainless steel tube (control pin 12) having a 0.395 inch inside diameter which accomodates the lower portion of vent plug 14. Other dimensions of the vent assembly 10 can be proportionately estimated adequately from the elevational view of FIG. 1 and, while approximate, will suffice for most purposes. The vent has a gas flow rate sufficient to maintain pressure in the air lock chamber 36 and in control pin 12 to prevent backflow of sodium and any possibly contaminating outside cover gas, respectively.
FIG. 2 is a fragmentary elevational view, shown somewhat enlarged in section, of the vent structure 22. The vent structure 22 includes a thin wall tubing 40 having an undeformed lower portion 42, and a flattened and folded (coiled or rolled and pressed) upper portion 44. The flattened upper portion 44 is preferably folded at least twice, as shown. A particulate filter 46 is provided in the lower portion 42 of the tubing 40, and a film or layer 48 of fine particles or powder is provided between the pressed opposing surfaces inside the upper portion 44. The tubing 40 can be made of any material sufficiently ductile to survive the flattening, coiling and pressing operations without cracking, and there are appropriate materials readily available for operation or use under a very wide range of environmental and temperature conditions.
In the interests of compatibility and uniformity, the tubing 40 can be made of the same material as the control pin 12 structural material. Thus, the tubing 40 can be made of Type 3 l6 stainless steel having an inside diameter D and an outside diameter E as indicated in FIG. 2. Likewise, the particulate filter 46 can be made of Type F-3 l5 nickel felt metal similar to that of bafile 16 (FIG. I) and having a length F. The cylindrically shaped filter 46 can be installed in the lower portion 42 by press-fitting it into the tubing 40 to a position approximately as illustrated. Exemplary dimensions for the inside diameter D, outside diameter E, and length F are respectively 0.093, (H25, and 0.250 inch, for example.
The formed upper portion 44 of the exemplary vent structure 22 has a length G and a thickness H as indicated in FIG. 2. The film or layer 48 can consist essentially of, for example, compacted 0.3 micron diameter aluminum oxide (A1 0 particles. This particle size could be increased to as large as 1 micron or reduced to as small as 0.05 micron for satisfactory operation. A particle size larger than 1 micron would provide individual support points during forming (flattening and pressing) of the upper portion 44 and which may prevent the attainment of low gas flow rates. Of course, a particle size smaller than 0.05 micron may not prevent eventual grain growth across the proximate faces of a flattened tube at high temperatures. Thus, in regular long term and high temperature operations, it is possible for the fonned upper portion 44 of the vent structure to sinter together. Note that the formed vent structure 22, with or without the layer 48 of alumina particles, can be used independently as a gas flow metering device in various applications following suitable flow calibration thereof.
illustrative dimensions for the length G and thickness H are respectively about 0.350 and 0.092 inch, for example. The thickness of the film or layer 48 can be approximately 0.005 inch, when pressed, although the layer thickness in the exemplary vent structure 22 can be generally between 0.003 and 0.007 inch for satisfactory operation. Exact pressing parameters and anneal conditions are functions of the particular size and wall thickness of the tubing 40 used and the desired gas flow rate. The method of fabricating the vent structure 22 will be described later, following a discussion of certain test results thereof.
FIGS. 3, 4 and 5 are graphs showing respective plots of helium pressure versus helium flow rate of the vent structure 22, vent temperature versus helium flow rate at 1 atmosphere pressure differential, and thermal cycles versus helium flow rate wherein the cycle period was two minutes from high temperature to low temperature. The curve 50 of FIG. 3 illustrates that a substantially linear relationship exists in the response in helium flow rate of the vent structure 22 to change in helium pressure. As indicated in FIG. 3, helium flow rate drops linearly as the driving pressure decreases.
In testing the vent structure 22, it was thermally cycled 60 times between 375 and l130F wherein the cycle period was 2 minutes from high temperature to low temperature and 2 minutes back to high temperature. Curve 52 of FIG. 4 illustrates helium release rates of the vent structure 22 as a function of its temperature while maintaining a pressure differential of l atmosphere for the vent structure. Flow rate is, of course, lower at the higher temperatures since there are less gas molecules in a fixed volume at such temperatures with the maintained pressure differential. Curve 54 of FIG. 4 illustrates helium release rates of another vent structure as a function of its temperature at a pressure differential of 1 atmosphere, the vent structure being similar to vent structure 22 but formed to provide a nominally higher flow rate.
The effect of thermal cycling between 375 and ll30F of the vent structure 22 is illustrated by the curves 56 and 58 of FIG. 5. Curve 56 depicts the helium flow rate at the low temperature of 375F and curve 58 depicts such flow rate at the high temperature of ll30F. After the vent structure 22 has been thermally cycled 60 times between these temperatures, it can be seen that there are slight but not functionally significant changes in performance thereof.
With the helium generation rate per control pin 12 (FIG. 1) at approximately 3 cc/hr, the vent structure 22 provides an average helium diffusion rate of about 0.61 cc/hr at one atmosphere pressure differential after 60 thermal cycles (FIG. 5). This allows a helium pressure of approximately 4 atmospheres inside the control pin 12 to provide a two-fold advantage. First, pressurized helium has a higher thermal conductivity to dissipate radiation heating in the control pin and, second, the pressure minimizes any possibility of back diffusion of either sodium vapor or cover gas into the control pin. The positive helium pressure maintained in the control pin 12 by the vent structure 22 can drop by a factor of about 2 without compromising the sodium seal provided.
FIGS. 6A through 6E illustrate certain main steps in the method of fabricating the vent structure 22. In FIG. 6A, following ultrasonic inspection of a Type 3 l 6 stainless steel tubing 40 of 0. I25 OD. and 0.0l6 inch wall, the tubing is cut to a predetermined length and vacuum annealed l5 minutes at 1900F, for example. Austenitic stainless steel is virtually unaffected by pure hot sodium at temperatures below 1000F. In the region between l000 and l500F, however, there is evidence of some measurable attack, particularly at the grain boundaries. Based on this constraint, the vent tubing 40 wall thickness was selected to be 0.016 inch to provide a safety factor of at least 3 over the deepest sodium penetration observed at 1500F. The annealed tubing 40 is then uniformly filled loosely with alumina particles of a generally predetermined size as, for example, 0.3 micron diameter. Tamping is unnecessary and it is not critical that the tubing 40 be very uniformly filled. A light shaking of the tubing 40 during filling ordinarily suffices. In fact, one way to fill the tubing 40 is simply to push it into a jar of alumina.
A predetermined length of the filled tubing 40 is then flattened in, for example, a Carver hydraulic press at a predetermined flattening pressure. The flattened tubing 40 is illustrated in FIG. 6B. The flattened portion of tubing 40 is next formed by rolling it into a two-bend spiral as shown in FIG. 6C, and a final pressing operation is performed thereon at a predetermined pressing pressure. This produces the configuration illustrated in FIGS. 6D and 6E and which creates a flat tortuous path for the escaping gas. The compacted alumina throughout the vent wall interface eliminates the operational sintering tendency due to grain growth across the faces of the flattened tubing 40 at high temperatures. The formed tubing 40 is then preferably vacuum annealed l5 minutes at l900F again. A particulate filter 46 is finally press-fitted into the formed tubing 40 as indicated in FIG. 6E to complete the vent structure 22. The formed tubing 40 is preferably annealed particularly where the vent structure 22 is used in high temperature (600C or I l 12F) operation because flow rate doubles in the vent structure going from a stressed to annealed condition and operating at the high temperature of 600C, the vent will self-anneal over a period of 3 weeks.
The alumina or aluminum oxide powder is compatible with any vent tubing material and is uniquely suited for operation in the presence of hot sodium vapor. It is an extremely stable oxide and is the only commonly processed oxide resistant to attack by hot sodium and sodium vapor. As mentioned previously, however, exact pressing parameters (and anneal conditions) are a function of the particular size and wall thickness of the vent tubing used and the desired gas flow rate. In the flattening and pressing operations required on the particular vent tubing 40 of 0. inch OD. and 0.016 inch wall, air flow rate at 15 psi differential pressure is illustratively varied according to flattening and pressing pressures as indicated below.
It is noted that gas flow rate through the vent structure 22 is also dependent upon the nature of the gas. As vents are made for lower and lower flow rates, this difference becomes more significant as indicated below.
Air Flow Rate Helium Flow Rate (cc/hr) (cc/hr) By changes in pressing pressures and techniques, the vent structure 22 can be fabricated for any required flow down to, for example, 0.0036 cc/hr helium at one atmosphere pressure differential. Also, flow through the vent structure 22 can increase greatly in case of a sudden increase in helium pressure within the control pin 12. Thus, the vent structure 22 effectively acts to relieve pressure transients in the control pin 12 to prevent any possible ruptures thereof and then returns by natural springback to normal operation if the elastic limit of the formed tubing 40 has not been exceeded. The illustrative vent structure 22 has been tested and found good to over 3500 psi, for example. While the doubly folded, formed tubing 40 does not actually un roll in order to relieve high increases in pressure, it tends to do so. This was substantiated in testing a vent structure 22 with increasing pressure until it burst at a very high pressure, when the formed tubing 40 did unroll to some extent.
FIG. 7 is a flow chart illustrating a process of producing the vent assembly 10 (FIG. 1). ln the process, the Type 316 stainless steel tubing 40 is provided in a step 60, for example. The tubing 40 is checked for proper dimensional tolerances and ultrasonically inspected in step 62, so that it can be certified free from flaws. The tubing 40 is cut to length and ultrasonically cleaned in Freon, for example, in step 64. The cut tubing 40 is next vacuum annealed minutes at l900F in step 66. The annealed tubing 40 is formed in step 68 according to the method shown and described above with respect to FIGS. 6A through 6E. The formed tubing 40 is preferably vacuum annealed 15 minutes at l900F as indicated in step 70 and calibrated for flow in the next step 72. Each formed vent is tested and individually characterized for helium flow in standard cc per hour measuring actual pressure rise in a vacuum system of calibrated volume with helium on the inlet side provided at 760 torr. These tests also serve as the fiow acceptance test for each vent.
Because of the production of lithium as a result of the (neutron, alpha) reaction on boron carbide and the possibility of boron carbide disintegration under irradiation, the unpressed section (lower portion 42 in FIG. 2) of tubing 40 can include the particulate filter 46 which allows free passage of gas. To produce the particulate filter 46, nickel felt metal can be used as indicated in step 74. Of course, a foamed instead of felt metal can be used and the metal can be stainless steel instead of nickel, for example, since such materials are resistant to attack by hot sodium and allow free passage of gas. Following the material inspection step 75, a filter disc or discs of appropriate size can be punched out from the nickel felt metal in step 78 and the disc filter inspected in step 80.
Bafile 16 can be fabricated from stainless steel foam metal as indicated in step 82. This baffle material can, of course, be nickel instead of stainless steel and felt in stead of foam metal. Indeed, it is usually convenient and preferable that the baffle 16 and filter 46 be made of the same identical material. Following material inspection step 84, the foam metal is punched or otherwise shaped to size and configuration in step 86. The shaped baffle 16 is inspected in step 88. In similar manner, the vent adapter plug 14, air lock tube 18 and air lock cap 20 can be shaped from a Type 316 stainless steel rod provided in step and inspected in step 92. The plug 14, tube 18 and cap 20 can be machined to size and shape in step 94 from the stainless steel rod, and the finished products inspected in step 96. It is, of course, apparent that the formed tubing 40, filter 46, baffle 16, adapter plug 14, air lock tube 18 and air lock cap 20 can be fabricated in any elected sequence or all concurrently.
The particulate filter 46 is packed into the formed tubing 40 to complete vent structure 22 and the baffle 16 is packed onto the formed tubing in step 98. The adapter plug 14 is installed on the vent structure 22 against the lower surface of the baffle 16 and is joined at its lower end 32 to the lower end of the vent structure by a standing lip electron-beam weld in step 100. A helium leak check is made of the electron-beam weld in step 102, and the air lock cap 20 is tungsten-inert-gas (TlG) or electronbeam welded to the air lock tube 18 with its vent holes 24 (FIG. 1) located at the opposite end away from the cap in step 104. The air lock tube 18 is then TlG welded to the adapter plug 14 in step 106 to complete vent assembly 10, and acceptance tests are performed thereon in step 108. Completed assemblies can be packaged in plastic bags and sealed for delivery.
While an exemplary embodiment and method of this invention have been described above and shown in the accompanying drawings, it is to be understood that such embodiment and method are merely illustrative of, and not restrictive on, the broad invention and that I do not desire to be limited in my invention to the specific constructions or arrangements or steps shown and described, for various obvious modifications may occur to persons having ordinary skill in the art.
I claim:
1. A method of fabricating a vent structure, which comprises the steps of:
uniformly filling a ductile and relatively thin-walled tubing of predetermined length and size with fine separating particles;
then flattening a normally upper portion of said tubing at a predetermined flattening pressure;
coiling said flattened tubing portion against itself;
and
pressing said coiled tubing portion at a predetermined pressing pressure.
2. The invention as defined in claim 1 wherein said flattened tubing portion is coiled into at least a generally two-bend spiral configuration prior to pressing the same.
3. The invention as defined in claim 1 further comprising the step of press fitting a porous metal particulate filter into the undeformed portion of the tubing.
4. The invention as defined in claim 3 wherein said flattened tubing portion is coiled into at least a generally two-bend spiral configuration prior to pressing the same.
5. The invention as defined in claim 1 further comprising the step of initially annealing said tubing at a predetermined temperature for a predetermined time prior to flattening of said upper tubing portion.
3,919,757 9 10 6. The invention as defined in claim 5 further com- 7. The invention as defined in claim 6 further comprising the step of filling said upper tubing portion with prising the step of finally annealing said tubing at a preseparating particles following initial annealing of said determined temperature for a predetermined time foltubing and prior to flattening of said upper tubing por- 5 lowing flattening of said upper tubing portion. tion

Claims (7)

1. A method of fabricating a vent structure, which comprises the steps of: uniformly filling a ductile and relatively thin-walled tubing of predetermined length and size with fine separating particles; then flattening a normally upper portion of said tubing at a predetermined flattening pressure; coiling said flattened tubing portion against itself; and pressing said coiled tubing portion at a predetermined pressing pressure.
2. The invention as defined in claim 1 wherein said flattened tubing portion is coiled into at least a generally two-bend spiral configuration prior to pressing the same.
3. The invention as defined in claim 1 further comprising the step of press fitting a porous metal particulate filter into the undeformed portion of the tubing.
4. The invention as defined in claim 3 wherein said flattened tubing portion is coiled into at least a generally two-bend spiral configuration prior to pressing the same.
5. The invention as defined in claim 1 further comprising the step of initially annealing said tubing at a predetermined temperature for a predetermined time prior to flattening of said upper tubing portion.
6. The invention as defined in claim 5 further comprising the step of filling said upper tubing portion with separating particles following initial annealing of said tubing and prior to flattening of said upper tubing portion.
7. The invention as defined in claim 6 further comprising the step of finally annealing said tubing at a predetermined temperature for a predetermined time following flattening of said upper tubing portion.
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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5593085A (en) * 1995-03-22 1997-01-14 Solar Turbines Incorporated Method of manufacturing an impeller assembly

Citations (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2815889A (en) * 1955-07-28 1957-12-10 Engine Parts Mfg Company Metering device controlling discharge of fluids from aerosol containers
US3274066A (en) * 1965-10-05 1966-09-20 Lloyd R Zumwalt Unpurged fuel element
US3315336A (en) * 1962-05-07 1967-04-25 Rockwell Standard Co Method of making filter element
US3406094A (en) * 1964-06-03 1968-10-15 Beisswenger Heinrich Process and device for the discharge of fission gases from nuclear fuel elements
US3459636A (en) * 1968-07-24 1969-08-05 Atomic Energy Commission Vented fuel pin
US3573168A (en) * 1967-05-16 1971-03-30 Atomic Energy Authority Uk Nuclear fuel venting elements for the discharge of fission gases
US3677300A (en) * 1970-01-15 1972-07-18 Dunlop Holdings Ltd Pressure reducing devices
US3697377A (en) * 1967-07-13 1972-10-10 Commissariat Energie Atomique Vented nuclear fuel element
US3708858A (en) * 1971-01-15 1973-01-09 J Sasaki Method for preparation of a filter medium
US3801447A (en) * 1971-11-16 1974-04-02 W Heenan Ventillation of nuclear reaction fuel rods
US3838557A (en) * 1973-09-04 1974-10-01 Mc Donnell Douglas Corp Vent structure

Patent Citations (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2815889A (en) * 1955-07-28 1957-12-10 Engine Parts Mfg Company Metering device controlling discharge of fluids from aerosol containers
US3315336A (en) * 1962-05-07 1967-04-25 Rockwell Standard Co Method of making filter element
US3406094A (en) * 1964-06-03 1968-10-15 Beisswenger Heinrich Process and device for the discharge of fission gases from nuclear fuel elements
US3274066A (en) * 1965-10-05 1966-09-20 Lloyd R Zumwalt Unpurged fuel element
US3573168A (en) * 1967-05-16 1971-03-30 Atomic Energy Authority Uk Nuclear fuel venting elements for the discharge of fission gases
US3697377A (en) * 1967-07-13 1972-10-10 Commissariat Energie Atomique Vented nuclear fuel element
US3459636A (en) * 1968-07-24 1969-08-05 Atomic Energy Commission Vented fuel pin
US3677300A (en) * 1970-01-15 1972-07-18 Dunlop Holdings Ltd Pressure reducing devices
US3708858A (en) * 1971-01-15 1973-01-09 J Sasaki Method for preparation of a filter medium
US3801447A (en) * 1971-11-16 1974-04-02 W Heenan Ventillation of nuclear reaction fuel rods
US3838557A (en) * 1973-09-04 1974-10-01 Mc Donnell Douglas Corp Vent structure

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5593085A (en) * 1995-03-22 1997-01-14 Solar Turbines Incorporated Method of manufacturing an impeller assembly

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