US2820751A - Process for producing jacketed bodies - Google Patents

Process for producing jacketed bodies Download PDF

Info

Publication number
US2820751A
US2820751A US323348A US32334852A US2820751A US 2820751 A US2820751 A US 2820751A US 323348 A US323348 A US 323348A US 32334852 A US32334852 A US 32334852A US 2820751 A US2820751 A US 2820751A
Authority
US
United States
Prior art keywords
frame
zirconium
sheets
fuel
steel
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Lifetime
Application number
US323348A
Inventor
Henry A Saller
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Individual
Original Assignee
Individual
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Individual filed Critical Individual
Priority to US323348A priority Critical patent/US2820751A/en
Priority claimed from GB34844/57A external-priority patent/GB838324A/en
Application granted granted Critical
Publication of US2820751A publication Critical patent/US2820751A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • GPHYSICS
    • G21NUCLEAR PHYSICS; NUCLEAR ENGINEERING
    • G21CNUCLEAR REACTORS
    • G21C21/00Apparatus or processes specially adapted to the manufacture of reactors or parts thereof
    • G21C21/02Manufacture of fuel elements or breeder elements contained in non-active casings
    • G21C21/10Manufacture of fuel elements or breeder elements contained in non-active casings by extrusion, drawing, or stretching by rolling, e.g. "picture frame" technique
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23KSOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K20/00Non-electric welding by applying impact or other pressure, with or without the application of heat, e.g. cladding or plating
    • B23K20/22Non-electric welding by applying impact or other pressure, with or without the application of heat, e.g. cladding or plating taking account of the properties of the materials to be welded
    • B23K20/233Non-electric welding by applying impact or other pressure, with or without the application of heat, e.g. cladding or plating taking account of the properties of the materials to be welded without ferrous layer
    • 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
    • Y10T29/30Foil or other thin sheet-metal making or treating
    • Y10T29/301Method
    • Y10T29/302Clad or other composite foil or thin metal making
    • 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
    • Y10T428/00Stock material or miscellaneous articles
    • Y10T428/12All metal or with adjacent metals
    • Y10T428/12014All metal or with adjacent metals having metal particles
    • Y10T428/12028Composite; i.e., plural, adjacent, spatially distinct metal components [e.g., layers, etc.]
    • 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
    • Y10T428/00Stock material or miscellaneous articles
    • Y10T428/12All metal or with adjacent metals
    • Y10T428/12486Laterally noncoextensive components [e.g., embedded, etc.]
    • 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
    • Y10T428/00Stock material or miscellaneous articles
    • Y10T428/12All metal or with adjacent metals
    • Y10T428/12493Composite; i.e., plural, adjacent, spatially distinct metal components [e.g., layers, joint, etc.]
    • Y10T428/12729Group IIA metal-base component
    • 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
    • Y10T428/00Stock material or miscellaneous articles
    • Y10T428/12All metal or with adjacent metals
    • Y10T428/12493Composite; i.e., plural, adjacent, spatially distinct metal components [e.g., layers, joint, etc.]
    • Y10T428/12771Transition metal-base component

Definitions

  • This invention relates to the provision of a jacket or cover for a metal core. More specifically, it relates to a process for encasing a metallic memberusable with a neutronic reactor.
  • An object of the present invention is toprovide a method for jacketing a metallic core containing a material fissionable by neutrons of thermal energy, such as uranium, so that the jacket will be tight and completely bonded to the core.
  • a material fissionable by neutrons of thermal energy such as uranium
  • the core will be protected against cor rosion, the heat of fission will efliciently be conducted away through the jacket, and the jacket will retain the fission fragments coming from the core.
  • the fissionable material is U -enriched uranium
  • the core will also contain aluminum or zirconium alloyed with the uranium. With an aluminum-uranium core an aluminum jacket will be used, and with a zirconium-uranium core a zirconium jacket or a tin-zirconium jacket will be employed.
  • control member employed with a neutronic reactor.
  • the control member may be formed of gadolinium oxide and titanium, and in this instance the jacket will be formed of titanium.
  • Fig. 8 is a vertical sectional view taken on the line 88 of Fig. 7;
  • Fig. 9 is a perspective view of a frame that is employed in the process of the third embodiment.
  • Fig. 10 is a perspective View of a modified form of frame used as part of a fuel-element jacket in the third embodiment.
  • uranium alloy employed in the modifications hereinafter mentioned, it is to be understood that the uranium in the alloy is enriched so as to contain 93% U and a balance of other isotopes.
  • degree of enrichment can be varied.
  • - fuel-element core 10 is formed of an alloy composedof 3 to 40% uranium and the balance substantially aluminum.
  • the fuel-element core is placed in a large opening 11 in an aluminum frame 12, which may be formed by a the cutting out of a large central section from a suitable bar.
  • the opening 11 fits the fuel-element core 10 relatively closely.
  • the thickness of the frame 12 is substantially that of the fuel-element core 10.
  • An aluminum sheet 13 is wrapped about the assembled fuel-elementcore 10 and frame 12 so that opposedportions 13a and .
  • a further object is to provide a method of applying a cation of Fermi and Szilard, Serial No.- 568,904, filed-- December 19, 1944, now Patent No. 2,708,656, issued May 17, 1955.
  • Fig. 1 is a plan view, with portions cut away and-in section,of one form ofassembly upon which aprocess of the present invention is performed; 7
  • Fig. 2 is a vertical: sectional view taken on the line 2-2 of Fig.- 1; i
  • Fig. 3 is a vertical sectional view similar to Fig. 2
  • Fig. 6 isv a vertical sectional view taken .,on the line 6-6 of Fig. 5;
  • Fig. 7 is a plan view, with portions cut away, of still another formof assembly upon which a third embodi-' the specifi- 13b of the sheet lie at opposite faces of the frame and the fuel-element core and edges of the sheet portions 13a and 13b are joined in a folded seam 14.
  • the sheet, frame, and fuel-element core are rolled at a suitable elevated temperature so that the structure of Fig. 3 is produced in which both parts'of the sheet are to the frame and to the fuel-element core and the frame bonded and the fuel-element core are bonded to one another.
  • the portions of the sheet 13 protruding beyond the edges of the frame 12 are preferably trimmed ofi.
  • the sheet portions 13a and 13b are of insufiicie'nt thickness after rolling, another similar aluminum sheet 15 is applied thereover as shown in Fig. 4 and the edges are joined in a'folded seam 16. Rolling is again performed at a suitable elevated temperature. The sheet 15 becomes bonded to the sheet portions 13a and 13b, and thus a-thicker aluminum covering is provided on the fuel element. Now the portions of the sheet 15 protruding beyond the frame 12 are preferably trimmed oif.
  • the fuel-element core 10 which is formed by casting, is preferably worked by forging or rolling at an elevated temperature before it is assembled with the frame 12 and the cover 13. This facilitates the formation of bonds of the fuel element core with the cover and the frame.
  • the fuel element has a relatively high percentage of uranium, it is advantageous to form the fuel element by chill-casting andworking.
  • a fuel-' element core 17 is formed of an alloy composed of 3 to 14% uranium and the balance substantially zirconium.
  • the fuel-element core 17 is placed in a large opening 18 in a'zirconium frame 19, which may be formed by the cutting out of a large central section from a suitable bar.
  • the fuel-element core 17 fits the opening 18 relatively closely and may actually be press-fitted in the frame 19.
  • Sheets 20 of zirconium are now applied to opposite faces of the assembled frame and fuel-element core. Now heat and pressure are applied to provide suitable bonds between the sheets 20 and the fuel-element core 17, the
  • assessiassembled sheets, fuelelement core, and frame are heated as rapidly as possible to some elevated temperature, for example, 1300F., and during this time, a pressure of somewhat less than .500 p.- s. i.is. applied. Thereaftera higher pressure, which may be 4000 p. s. i. for a fuela element core containing 4% uranitun, is applied until plastic deformation of the uranium-zirconium fuel-eles ment core 17 occurs, with the result that. the fuel-element core becomes bonded to the zirconium frame 1? and the zirconium sheets 20. Bonding of the frame to the sheets will also have occurred, since an appreciably lower pressure is required for plastic deformation of zirconium. If.
  • the pressure required for plastic deformation of the. uraniumzirconium fuel element is less than 4000 p. s. i.
  • the pressure is lowered just sufficiently to stop plastic deformation and maintainedat the lower value for about thirty minutes. Thereafter the temperature is lowered and thepressure is allowed to. drop to zero.
  • a uranium-zirconium fuel-element core 21, a zirconium frame 22, and zirconium sheets 23 are employed which correspond generally in composition to the fuel-element core 1'7,'the. frame 19, and sheets 20. of the modification of Figs. and 6, but the parts 21, 22, and 23 are bonded to one another by rolling rather; than by being simply pressure-welded to one another.
  • the fuel-element core fits an opening 24 in the frame 22 and may actually be press-fitted therein.
  • the frame 22 and sheets 23 have round corners 25, which fit round corners 26 in a steel frame 27 in which the fuel-element core 21, frame 22, and sheets 23 are positioned, the combined thickness of which isabout that of the steel frame.
  • Steel sheets 28 are laid against the sheets 23 and the steel frame 27.
  • the frame 27 and sheets 28 may be formed of a carbon steel having, for example, .18.23 %v carbon and other normal impurities.
  • One face of thesteel frame against'which one steel sheet 28 rests has a recess 29.
  • a hole. 30 extends from the recess 29 to an outer side of the. steel frame.
  • Thesteel sheets 28 and the steel frame 27 are. welded to one another, for example, by a metal-arc process, as indicated at 31, in order to constitute a box for thefuelelement core 21, the zirconium frame 22, and the. zirconium sheets 23,v which box may be. sealed off by applying a closure at the opening 30.
  • a closure at the opening 30.
  • Such .closure may take the formv of a tube 32 which is welded to the. steel frame 27 at the opening 30.
  • the tightness. of. the welds 31 may be tested by immersion of. the steeLbox and. the contained partsin water and the applicationofa gas.- such. asiargon under pressure to the interior ofthe' box through thetubc 32.
  • Ayacuum is now applied to the tube 32, and when the interior of the steel box is sufficiently evacuated, a region of the tube spaced-from the steel frame. 27 is heated, the tube is bent over on itself at thisregion, and the region is hammered flat until.sealed..
  • the heating of the assembly may be done in air, since the zirconium and zirconium-uranium parts are sealedin a vacuum within the steel parts and thus are not subjected to oxidation or corrosion which might interfere with the formation of good bonds.
  • the assembly is maintained for some time at the elevated temperature before each rolling pass. For example, if there are three passes, the assembly may be soaked or maintained at 1650 F. for thirty minutes before the first pass, reheated and soaked for fifteen minutes before the second pass, and reheated and soaked for ten minutes before the third pass.
  • the steel sheets 28 and the steel frame 27 are stripped off.
  • the round corners 25 on the zirconium frame 22 and the zirconium sheets 23 and the round corners 26 on the apertureinthe steel frame 27 have prevented these parts from diggin'g'into one another during the rolling process and thus facilitate removal of the steel frame.
  • the zirconium-uranium fuel-element core 21 is located by means of radiography, and from this the thicknesses of the zirconium layer are determined. Then the jacketed fuel element is machined if necessary to bring the jacket to desired thickness.
  • the zirconium-uranium fuel-element core 21, the zirconium sheets 23, and the zirconium frame 22 may be formed from ingots that are hot-worked to desired dimensions.
  • the hot-Working improves the bonding qualities andmay involve rolling in air at some elevated temperature such as 1450 F. after heating to this temperature in an argon atmosphere.
  • the parts may be jacketed in steel or copper before being rolled.
  • the parts to be rolled can also be formed by extrusion rather than castmg in ingots.
  • the one-piece zirconium frame 22 may be replaced by a split zirconium frame, shown in Fig. 10, composed of two parts 33 having oblique edges 34 in engagement with one another. It is simpler to manufacture the split frame than the two-part frame because of the ease of machining. The use of the split frame is feasible, because the steel frame 27 holds it together during the rolling of the entire assembly. The edges 34 of the parts 33 will become bonded to one another as a result of the rolling.
  • the entire assembly may be clamped between water-cooled plates in order to be protected fromoverheating due to the welding.
  • the welding maybe performed when the entire assembly is in an argon atmosphere.
  • corroslon-resistant' welds of the above composition are obtainable in air by means of an argon-shielded a frame. and sheets of the jacket material will be applied about the core, and rolling or'pressure welding will be performed on the core and jacket to bond the jacket to the core.
  • a process for enclosing a body of a first metal with a second metal comprising inserting the body into an aperture in a frame of the second metal, placing a. sheet of the second metal on each of opposite sides of the assembled body and frame, and bonding the sheets to the body and the frame and the body and the frame to one another.
  • a process for enclosing a body of a first metal with a second metal comprising inserting the body into an aperture in a frame of the second metal, the aperture generally fitting the body, placing a sheet of the second metal on each of opposite sides of the assembled body and frame, and applying heat and pressure to bond the sheets to the body and the frame and the body and the frame to one another.
  • a process for enclosing a body of an aluminumenn'ched-uranium alloy with aluminum comprising inserting the body into an aluminum frame having an aperture substantially the same shape as the body, applying the legs of a U-shaped aluminum sheet against the opposite sides of the assembled body and frame, interlocking the free ends of said legs, and rolling the sheet, the body, and the frame to bond the sheet to the body and the frame and the body and the frame to one another.
  • a process for enclosing a body of a zirconiumenriched uranium alloy in zirconium comprising inserting the body into a zirconium frame having an aperture substantially the same shape as the body, placing zirconium sheets over opposite sides of the frame and body, and applying pressure simultaneously over the entire areas of the sheets to bond them to the frame and the body and the body and the frame to one another.
  • a process for enclosing a body of a zirconiumenriched uranium alloy in zirconium comprising inserting the body in a zirconium frame, placing zirconium sheets on opposite sides of the frame and body in contact therewith, welding the sheets to the frame about the periphery thereof, and rolling the sheets, the frame, and the body to reduce them and to bond them to one another.
  • a process for enclosing a body of a zirconiumenriehed uranium alloy in zirconium comprising inserting the body in a zirconium frame having round outer corners, placing zirconium sheets on opposite sides of the frame and body in contact therewith, applying a steel frame having round inner corners about the zirconium frame and steel sheets against the zirconium sheets, welding the steel frame to the steel sheets, rolling the entire assembly to reduce the body and the zirconium frame and sheets and bond them to one another, and stripping off the steel sheets and the steel frame.
  • the steel frame being provided with a recess in one face contacted by one steel sheet and a hole leading from the recess to an outer side of the steel frame, the steel frame being further provided with a tube bonded to said hole and etxending externally of the steel frame, the steps prior to rolling of exhausting the space within the steel frame and the steel plates being carried out by the application of a vacuum to said tube, the step of sealing said space being carried out by the heating of a region of the tube spaced from the steel .frame and the bending over of the tube at said region to close the tube.

Landscapes

  • Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Mechanical Engineering (AREA)
  • Manufacturing & Machinery (AREA)
  • Plasma & Fusion (AREA)
  • General Engineering & Computer Science (AREA)
  • High Energy & Nuclear Physics (AREA)
  • Monitoring And Testing Of Nuclear Reactors (AREA)

Description

H. A. SALLER PROCESS FOR PRODUCING JACKETED BODIES Jan. 21, 1958 Filed Dec. 1, 1952 FIE- 3 I a l? ffa I PIE. 5
zzvmvroze. 135! aLaazzer- BY Jan. 21, 1958 H. A. SALLER PROCESS FOR PRODUCING JACKETED BODIES Filed Dec. 1, 1952 2 Sheets-Sheet z IN V EN TOR.
Sal/er 2,820,751 rnocnss Fun PRODUCING JACKETED BODIES Henry A. Stiller, Columbus, Ohio, assignor to the United States of America as represented by the United States Atomic Energy Commission Application December 1, 1952, Serial No. 323,348
9 Claims. (Cl. 204- 1542) This invention relates to the provision of a jacket or cover for a metal core. More specifically, it relates to a process for encasing a metallic memberusable with a neutronic reactor.
An object of the present invention is toprovide a method for jacketing a metallic core containing a material fissionable by neutrons of thermal energy, such as uranium, so that the jacket will be tight and completely bonded to the core. Thus the core will be protected against cor rosion, the heat of fission will efliciently be conducted away through the jacket, and the jacket will retain the fission fragments coming from the core. If the fissionable material is U -enriched uranium, the core will also contain aluminum or zirconium alloyed with the uranium. With an aluminum-uranium core an aluminum jacket will be used, and with a zirconium-uranium core a zirconium jacket or a tin-zirconium jacket will be employed.-
I Another object is to provide a'method; of encasing a control member employed with a neutronic reactor. The control member may be formed of gadolinium oxide and titanium, and in this instance the jacket will be formed of titanium.
2,820,751 littered ee-, 1i.1 5
ice
. 2 ment of the process. of the present invention is carried out;
Fig. 8 is a vertical sectional view taken on the line 88 of Fig. 7; Fig. 9 is a perspective view of a frame that is employed in the process of the third embodiment; and
Fig. 10 is a perspective View of a modified form of frame used as part of a fuel-element jacket in the third embodiment.
Wherever a uranium alloy is employed in the modifications hereinafter mentioned, it is to be understood that the uranium in the alloy is enriched so as to contain 93% U and a balance of other isotopes. In utilizing the invention for fuel elements of other nuclear reactors, the degree of enrichment can be varied.
In the modification illustrated in Figs. 1, 2, and'3, a
- fuel-element core 10 is formed of an alloy composedof 3 to 40% uranium and the balance substantially aluminum. The fuel-element core is placed in a large opening 11 in an aluminum frame 12, which may be formed by a the cutting out of a large central section from a suitable bar. The opening 11 fits the fuel-element core 10 relatively closely. The thickness of the frame 12 is substantially that of the fuel-element core 10. An aluminum sheet 13 is wrapped about the assembled fuel-elementcore 10 and frame 12 so that opposedportions 13a and .A further object is to provide a method of applying a cation of Fermi and Szilard, Serial No.- 568,904, filed-- December 19, 1944, now Patent No. 2,708,656, issued May 17, 1955. For further information on reactors that I,
can utilize fuel elements disclosed in the present applica-' tiou, reference is made to copending application of Zinn, Serial No. 721,108, filed January 8, 1947,and the copending, application of Eugene P. Wiguer,=Seria1 No. 314,595, filed October 14, 1952.
,Other objects will become apparent from cation and the drawings, in which: a
Fig. 1 is a plan view, with portions cut away and-in section,of one form ofassembly upon which aprocess of the present invention is performed; 7
. Fig. 2 is a vertical: sectional view taken on the line 2-2 of Fig.- 1; i
Fig. 3 is a vertical sectional view similar to Fig. 2
.Fig. 6 isv a vertical sectional view taken .,on the line 6-6 of Fig. 5;
Fig. 7 is a plan view, with portions cut away, of still another formof assembly upon which a third embodi-' the specifi- 13b of the sheet lie at opposite faces of the frame and the fuel-element core and edges of the sheet portions 13a and 13b are joined in a folded seam 14. The sheet, frame, and fuel-element core are rolled at a suitable elevated temperature so that the structure of Fig. 3 is produced in which both parts'of the sheet are to the frame and to the fuel-element core and the frame bonded and the fuel-element core are bonded to one another. Now the portions of the sheet 13 protruding beyond the edges of the frame 12 (indicated in dotted lines in Fig. 3) are preferably trimmed ofi.
If the sheet portions 13a and 13b are of insufiicie'nt thickness after rolling, another similar aluminum sheet 15 is applied thereover as shown in Fig. 4 and the edges are joined in a'folded seam 16. Rolling is again performed at a suitable elevated temperature. The sheet 15 becomes bonded to the sheet portions 13a and 13b, and thus a-thicker aluminum covering is provided on the fuel element. Now the portions of the sheet 15 protruding beyond the frame 12 are preferably trimmed oif.
' The fuel-element core 10, which is formed by casting, is preferably worked by forging or rolling at an elevated temperature before it is assembled with the frame 12 and the cover 13. This facilitates the formation of bonds of the fuel element core with the cover and the frame.
If the fuel element has a relatively high percentage of uranium, it is advantageous to form the fuel element by chill-casting andworking.
vIn the modification illustrated in Figs. 5 and 6, a fuel-' element core 17 is formed of an alloy composed of 3 to 14% uranium and the balance substantially zirconium. The fuel-element core 17 is placed in a large opening 18 in a'zirconium frame 19, which may be formed by the cutting out of a large central section from a suitable bar.
' The fuel-element core 17 fits the opening 18 relatively closely and may actually be press-fitted in the frame 19. Sheets 20 of zirconium are now applied to opposite faces of the assembled frame and fuel-element core. Now heat and pressure are applied to provide suitable bonds between the sheets 20 and the fuel-element core 17, the
sheets 20 and the frame 19, and'the fuel-element core 17 and the frame 19. Pressure is applied uniformly and simultaneously across the entire areas of the sheets 20 by a suitable pressure-welding unit. This may be done in a vacuum or anargon or helium atmosphere. The
assessiassembled sheets, fuelelement core, and frame are heated as rapidly as possible to some elevated temperature, for example, 1300F., and during this time, a pressure of somewhat less than .500 p.- s. i.is. applied. Thereaftera higher pressure, which may be 4000 p. s. i. for a fuela element core containing 4% uranitun, is applied until plastic deformation of the uranium-zirconium fuel-eles ment core 17 occurs, with the result that. the fuel-element core becomes bonded to the zirconium frame 1? and the zirconium sheets 20. Bonding of the frame to the sheets will also have occurred, since an appreciably lower pressure is required for plastic deformation of zirconium. If. a temperature higher than; l300F. is employed, the pressure required for plastic deformation of the. uraniumzirconium fuel element is less than 4000 p. s. i. When the desired amountof plastic deformation has occurred, the pressure is lowered just sufficiently to stop plastic deformation and maintainedat the lower value for about thirty minutes. Thereafter the temperature is lowered and thepressure is allowed to. drop to zero.
. The aforementioned heating to the elevated temperature which was given as 1300 F. should take place as rapidly as possible in order that any beneficial effects of recrystallization and grain growth may be obtained.
Although this is not essential for bonding, it is desirable that the surfaces of the fuel-element core 17, frame 19, and sheets 20 be cold-worked before the pres sure-welding process is carried out, in' order that recrystallization across the bonds may be facilitated.
In the modification shown in Figs. 7, 8, and 9, a uranium-zirconium fuel-element core 21, a zirconium frame 22, and zirconium sheets 23 are employed which correspond generally in composition to the fuel-element core 1'7,'the. frame 19, and sheets 20. of the modification of Figs. and 6, but the parts 21, 22, and 23 are bonded to one another by rolling rather; than by being simply pressure-welded to one another. The fuel-element core fits an opening 24 in the frame 22 and may actually be press-fitted therein. The frame 22 and sheets 23 have round corners 25, which fit round corners 26 in a steel frame 27 in which the fuel-element core 21, frame 22, and sheets 23 are positioned, the combined thickness of which isabout that of the steel frame. Steel sheets 28 are laid against the sheets 23 and the steel frame 27. The frame 27 and sheets 28 may be formed of a carbon steel having, for example, .18.23 %v carbon and other normal impurities. One face of thesteel frame against'which one steel sheet 28 rests has a recess 29. A hole. 30 extends from the recess 29 to an outer side of the. steel frame.
Thesteel sheets 28 and the steel frame 27 are. welded to one another, for example, by a metal-arc process, as indicated at 31, in order to constitute a box for thefuelelement core 21, the zirconium frame 22, and the. zirconium sheets 23,v which box may be. sealed off by applying a closure at the opening 30. Such .closure may take the formv of a tube 32 which is welded to the. steel frame 27 at the opening 30. The tightness. of. the welds 31 may be tested by immersion of. the steeLbox and. the contained partsin water and the applicationofa gas.- such. asiargon under pressure to the interior ofthe' box through thetubc 32. Ayacuum is now applied to the tube 32, and when the interior of the steel box is sufficiently evacuated, a region of the tube spaced-from the steel frame. 27 is heated, the tube is bent over on itself at thisregion, and the region is hammered flat until.sealed..
Now theparts are ready. to be. rolled.. This is carried? out in one or more passes through'rolls (not. shown): of the entire assembly composedt'o the. steel frame 27,.steeli sheets 23, zirconium-uranium fuel-elementicore 21, zirconium frame 22., and zirconium sheets23. Iris-"desirableto carry: out some appreciablev reduction. onthe: fuel. element andzirconium; frame and sheets; such as:3 to: 1. The rolling shouldbe performed at some suitable elevated: temperature" such as 1450 to 1650 F. Care:
must .be exercised-to .prevent bonding of the steel to the zirconium, and this requires a proper balance of elevated temperature and the amount of time at the elevated temperature used for the rolling. In other words, the more elevated the temperature, the less the permissible time at the temperature. The heating of the assembly may be done in air, since the zirconium and zirconium-uranium parts are sealedin a vacuum within the steel parts and thus are not subjected to oxidation or corrosion which might interfere with the formation of good bonds. The assembly is maintained for some time at the elevated temperature before each rolling pass. For example, if there are three passes, the assembly may be soaked or maintained at 1650 F. for thirty minutes before the first pass, reheated and soaked for fifteen minutes before the second pass, and reheated and soaked for ten minutes before the third pass.
After the assembly has cooled sufficiently, the steel sheets 28 and the steel frame 27 are stripped off. The round corners 25 on the zirconium frame 22 and the zirconium sheets 23 and the round corners 26 on the apertureinthe steel frame 27 have prevented these parts from diggin'g'into one another during the rolling process and thus facilitate removal of the steel frame. Now the zirconium-uranium fuel-element core 21 is located by means of radiography, and from this the thicknesses of the zirconium layer are determined. Then the jacketed fuel element is machined if necessary to bring the jacket to desired thickness.
The zirconium-uranium fuel-element core 21, the zirconium sheets 23, and the zirconium frame 22 may be formed from ingots that are hot-worked to desired dimensions. The hot-Working improves the bonding qualities andmay involve rolling in air at some elevated temperature such as 1450 F. after heating to this temperature in an argon atmosphere. The parts may be jacketed in steel or copper before being rolled. The parts to be rolled can also be formed by extrusion rather than castmg in ingots.
The one-piece zirconium frame 22 may be replaced by a split zirconium frame, shown in Fig. 10, composed of two parts 33 having oblique edges 34 in engagement with one another. It is simpler to manufacture the split frame than the two-part frame because of the ease of machining. The use of the split frame is feasible, because the steel frame 27 holds it together during the rolling of the entire assembly. The edges 34 of the parts 33 will become bonded to one another as a result of the rolling.
When thesteel plates 28 are being welded to the steel frame 27 as indicated at 31, the entire assembly may be clamped between water-cooled plates in order to be protected fromoverheating due to the welding. The welding maybe performed when the entire assembly is in an argon atmosphere.
An alternative processis to roll the assembled uraniumzirconium fuel-element core 21, the zirconium frame 22, and-the zirconium sheets 23'without encasing them in the steel frame'and steel-sheets; In this event the peripheries of the zirconium sheets are welded to' the zirconium frame-before the rolling by suitable means such as an argon-shielded tungsten-electrode are. This alternate process is specially adapted to a frame 22 and sheets 23 composed of about 5%- tin and the balance substantially zirconium. The small amount of tin im roves the cor-' rosion resistance of the zirconium with respect to water. Thus corroslon-resistant' welds of the above composition are obtainable in air by means of an argon-shielded a frame. and sheets of the jacket material will be applied about the core, and rolling or'pressure welding will be performed on the core and jacket to bond the jacket to the core.
While various embodiments of the instant invention have been presented, various modifications within the scope of the invention will be apparent to those skilled in the art. The invention is not limited by these embodiments but only by the claims which follow.
What is claimed is:
l. A process for enclosing a body of a first metal with a second metal, comprising inserting the body into an aperture in a frame of the second metal, placing a. sheet of the second metal on each of opposite sides of the assembled body and frame, and bonding the sheets to the body and the frame and the body and the frame to one another.
2. A process for enclosing a body of a first metal with a second metal, comprising inserting the body into an aperture in a frame of the second metal, the aperture generally fitting the body, placing a sheet of the second metal on each of opposite sides of the assembled body and frame, and applying heat and pressure to bond the sheets to the body and the frame and the body and the frame to one another.
3. A process for enclosing a body of an aluminumenn'ched-uranium alloy with aluminum, comprising inserting the body into an aluminum frame having an aperture substantially the same shape as the body, applying the legs of a U-shaped aluminum sheet against the opposite sides of the assembled body and frame, interlocking the free ends of said legs, and rolling the sheet, the body, and the frame to bond the sheet to the body and the frame and the body and the frame to one another.
4. The process specified in claim 3 and further comprising the steps of cutting off the interlocked free ends of the legs of the U-shaped sheet and the base thereof, applying a second U-shaped aluminum sheet against the portions of the first sheet now bonded to the frame and the body, interlocking the free ends of the legs of the second U-shaped sheet, and rolling to bond the second sheet to the said portions of the first sheet.
5. A process for enclosing a body of a zirconiumenriched uranium alloy in zirconium, comprising inserting the body into a zirconium frame having an aperture substantially the same shape as the body, placing zirconium sheets over opposite sides of the frame and body, and applying pressure simultaneously over the entire areas of the sheets to bond them to the frame and the body and the body and the frame to one another.
6. A process for enclosing a body of a zirconiumenriched uranium alloy in zirconium, comprising inserting the body in a zirconium frame, placing zirconium sheets on opposite sides of the frame and body in contact therewith, welding the sheets to the frame about the periphery thereof, and rolling the sheets, the frame, and the body to reduce them and to bond them to one another.
7. A process for enclosing a body of a zirconiumenriehed uranium alloy in zirconium, comprising inserting the body in a zirconium frame having round outer corners, placing zirconium sheets on opposite sides of the frame and body in contact therewith, applying a steel frame having round inner corners about the zirconium frame and steel sheets against the zirconium sheets, welding the steel frame to the steel sheets, rolling the entire assembly to reduce the body and the zirconium frame and sheets and bond them to one another, and stripping off the steel sheets and the steel frame.
8. The process specified in claim 7 and further comprising, prior to rolling, exhausting the space within the 'steel frame and steel sheets and sealing said space to produce better bonds between the body, the zirconium frame, and the zirconium sheets when they are reduced by rolling.
9. The process specified in claim 7, the steel frame being provided with a recess in one face contacted by one steel sheet and a hole leading from the recess to an outer side of the steel frame, the steel frame being further provided with a tube bonded to said hole and etxending externally of the steel frame, the steps prior to rolling of exhausting the space within the steel frame and the steel plates being carried out by the application of a vacuum to said tube, the step of sealing said space being carried out by the heating of a region of the tube spaced from the steel .frame and the bending over of the tube at said region to close the tube.
References Cited in the file of this patent UNITED STATES PATENTS 1,374,110 Pittevil Apr. 5, 1921 1,886,615 Johnson Nov. 8, 1932 2,059,584 Johnson Nov. 3, 1936 2,064,684 Ostendorf Dec. 15, 1936

Claims (1)

1. A PROCESS FOR ENCLOSING A BODY OF A FIRST METAL WITH A SECOND METAL, COMPRISING INSERTING THE BODY INTO AN APERTURE IN A FRAME OF THE SECOND METAL, PLACING A SHEET OF THE SECOND METAL ON EACH OF OPPOSITE SIDES OF THE ASSEMBLED BODY AND FRAME, AND BONDING THE SHEETS TO THE BODY AND THE FRAME AND THE BODY AND THE FRAME TO ONE ANOTHER.
US323348A 1952-12-01 1952-12-01 Process for producing jacketed bodies Expired - Lifetime US2820751A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US323348A US2820751A (en) 1952-12-01 1952-12-01 Process for producing jacketed bodies

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US323348A US2820751A (en) 1952-12-01 1952-12-01 Process for producing jacketed bodies
GB34844/57A GB838324A (en) 1957-11-08 1957-11-08 Process for enclosing a body containing fissionable material in a jacket

Publications (1)

Publication Number Publication Date
US2820751A true US2820751A (en) 1958-01-21

Family

ID=26262463

Family Applications (1)

Application Number Title Priority Date Filing Date
US323348A Expired - Lifetime US2820751A (en) 1952-12-01 1952-12-01 Process for producing jacketed bodies

Country Status (1)

Country Link
US (1) US2820751A (en)

Cited By (42)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2914847A (en) * 1958-03-28 1959-12-01 Storchheim Samuel Solid state bonding of thorium with aluminum
US2915815A (en) * 1957-04-30 1959-12-08 Charles H Bean Method of making fuel elements
US2986504A (en) * 1958-05-23 1961-05-30 Martin Co Flat plate type fuel elements
US2990360A (en) * 1959-04-08 1961-06-27 Jr Stanley W Porembka Neutronic reactor control rod and method of fabrication
US3004907A (en) * 1958-06-19 1961-10-17 Martin Co Fuel tube element and method of preparing the same
US3004906A (en) * 1956-11-09 1961-10-17 North American Aviation Inc Uranium foil nuclear fuel element
US3009242A (en) * 1958-01-03 1961-11-21 Richard J Beaver Zirconium-cladding of thorium
US3054035A (en) * 1956-05-17 1962-09-11 Gulton Ind Inc Ceramic components and method of making same
US3062016A (en) * 1957-12-31 1962-11-06 Air Reduction Maintaining high purity argon atmosphere
US3070880A (en) * 1959-09-30 1963-01-01 Texas Instruments Inc Method of bonding the abutted edges of metal members
US3091847A (en) * 1958-10-29 1963-06-04 Ernest J Peters Method of manufacture of metal encased core material
US3097152A (en) * 1958-12-01 1963-07-09 Gen Electric Nuclear reactor fuel element and method for producing such fuel element
US3098024A (en) * 1959-01-27 1963-07-16 Engelhard Ind Inc Composite fuel elements for nuclear reactors
US3109797A (en) * 1957-10-01 1963-11-05 Martin Marietta Corp Tubular fuel elements and fabricating techniques therefor
US3110961A (en) * 1959-04-06 1963-11-19 North American Aviation Inc Honeycomb sandwich panel brazing
US3122423A (en) * 1960-04-04 1964-02-25 Beryllium Corp Method and apparatus for hot rolling high quality metal sheet
US3123893A (en) * 1964-03-10 Method of working sheet
US3136051A (en) * 1962-10-11 1964-06-09 Frank B Quinlan Cladding of nuclear fuel elements
US3139681A (en) * 1958-05-13 1964-07-07 Martin Marietta Corp Method of manufacturing nuclear reactor fuel elements
US3141227A (en) * 1958-09-29 1964-07-21 Gen Electric Method of nuclear fuel and control element fabrication
US3145150A (en) * 1960-01-04 1964-08-18 North American Aviation Inc Fuel-moderator element for a nuclear reactor and method of making
US3151037A (en) * 1961-02-21 1964-09-29 Minnesota Mining & Mfg Encased fuel
US3160951A (en) * 1957-10-29 1964-12-15 Babcock & Wilcox Co Method of making fuel pins by extrusion
US3161950A (en) * 1960-04-01 1964-12-22 United Nuclear Corp Electron beam welding process
US3185652A (en) * 1960-04-29 1965-05-25 Nuclear Corp Of America Refractory rare earth material
US3199189A (en) * 1962-03-29 1965-08-10 Alloys Unltd Inc Gold alloy cladding
US3210256A (en) * 1960-12-08 1965-10-05 Atomic Energy Authority Uk Manufacture of nuclear reactor fuel elements
US3243350A (en) * 1956-01-13 1966-03-29 Lustman Benjamin Clad alloy fuel elements
US3297543A (en) * 1964-07-07 1967-01-10 Babcock & Wilcox Co Plate-type nuclear fuel element
US3322951A (en) * 1964-08-28 1967-05-30 Paul M Yavorsky Efficient beta-ray emission source for irradiation applications
US3336656A (en) * 1962-03-27 1967-08-22 Atomic Energy Authority Uk Manufacture of cermet bodies
US3349466A (en) * 1960-05-02 1967-10-31 Martin Marietta Corp Method of manufacturing aluminumclad nuclear fuel elements by hotswaging in air
US3352004A (en) * 1963-08-09 1967-11-14 Commissariat Energie Atomique Process for cladding uranium rods
US3413195A (en) * 1964-10-22 1968-11-26 Kernforschungsanlage Juelich Fuel or fertile element for nuclear reactors
US3522111A (en) * 1967-10-24 1970-07-28 Republic Steel Corp Method of making a composite metal product
US3601884A (en) * 1968-05-20 1971-08-31 Westinghouse Electric Corp Method of constructing parts suitable for high heat flux removal in arc heaters
US3602978A (en) * 1969-04-14 1971-09-07 Us Navy Method of forming bimetallic transition joints
US3849867A (en) * 1957-10-02 1974-11-26 Atomic Energy Commission Process of jacketing fuel elements
EP0154267A2 (en) * 1984-03-07 1985-09-11 Nukem GmbH Method of manufacturing plate-shaped fuel elements for research reactors
US4709848A (en) * 1957-10-02 1987-12-01 The United States Of America As Represented By The United States Department Of Energy Method of bonding
US5296310A (en) * 1992-02-14 1994-03-22 Materials Science Corporation High conductivity hydrid material for thermal management
US6075701A (en) * 1999-05-14 2000-06-13 Hughes Electronics Corporation Electronic structure having an embedded pyrolytic graphite heat sink material

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1374110A (en) * 1918-10-14 1921-04-05 Pittevil Alois Gerar Corneille Welding of different metals to form a. composite ingot
US1886615A (en) * 1932-04-01 1932-11-08 Plykrome Corp Manufacture of composite metal sheets
US2059584A (en) * 1935-07-12 1936-11-03 Plykrome Corp Process of making composite metal
US2064684A (en) * 1933-11-02 1936-12-15 Peter Ostendorf Method of welding

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1374110A (en) * 1918-10-14 1921-04-05 Pittevil Alois Gerar Corneille Welding of different metals to form a. composite ingot
US1886615A (en) * 1932-04-01 1932-11-08 Plykrome Corp Manufacture of composite metal sheets
US2064684A (en) * 1933-11-02 1936-12-15 Peter Ostendorf Method of welding
US2059584A (en) * 1935-07-12 1936-11-03 Plykrome Corp Process of making composite metal

Cited By (45)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3123893A (en) * 1964-03-10 Method of working sheet
US3243350A (en) * 1956-01-13 1966-03-29 Lustman Benjamin Clad alloy fuel elements
US3054035A (en) * 1956-05-17 1962-09-11 Gulton Ind Inc Ceramic components and method of making same
US3004906A (en) * 1956-11-09 1961-10-17 North American Aviation Inc Uranium foil nuclear fuel element
US2915815A (en) * 1957-04-30 1959-12-08 Charles H Bean Method of making fuel elements
US3109797A (en) * 1957-10-01 1963-11-05 Martin Marietta Corp Tubular fuel elements and fabricating techniques therefor
US3849867A (en) * 1957-10-02 1974-11-26 Atomic Energy Commission Process of jacketing fuel elements
US4709848A (en) * 1957-10-02 1987-12-01 The United States Of America As Represented By The United States Department Of Energy Method of bonding
US3160951A (en) * 1957-10-29 1964-12-15 Babcock & Wilcox Co Method of making fuel pins by extrusion
US3062016A (en) * 1957-12-31 1962-11-06 Air Reduction Maintaining high purity argon atmosphere
US3009242A (en) * 1958-01-03 1961-11-21 Richard J Beaver Zirconium-cladding of thorium
US2914847A (en) * 1958-03-28 1959-12-01 Storchheim Samuel Solid state bonding of thorium with aluminum
US3139681A (en) * 1958-05-13 1964-07-07 Martin Marietta Corp Method of manufacturing nuclear reactor fuel elements
US2986504A (en) * 1958-05-23 1961-05-30 Martin Co Flat plate type fuel elements
US3004907A (en) * 1958-06-19 1961-10-17 Martin Co Fuel tube element and method of preparing the same
US3141227A (en) * 1958-09-29 1964-07-21 Gen Electric Method of nuclear fuel and control element fabrication
US3091847A (en) * 1958-10-29 1963-06-04 Ernest J Peters Method of manufacture of metal encased core material
US3097152A (en) * 1958-12-01 1963-07-09 Gen Electric Nuclear reactor fuel element and method for producing such fuel element
US3098024A (en) * 1959-01-27 1963-07-16 Engelhard Ind Inc Composite fuel elements for nuclear reactors
US3110961A (en) * 1959-04-06 1963-11-19 North American Aviation Inc Honeycomb sandwich panel brazing
US2990360A (en) * 1959-04-08 1961-06-27 Jr Stanley W Porembka Neutronic reactor control rod and method of fabrication
US3070880A (en) * 1959-09-30 1963-01-01 Texas Instruments Inc Method of bonding the abutted edges of metal members
US3145150A (en) * 1960-01-04 1964-08-18 North American Aviation Inc Fuel-moderator element for a nuclear reactor and method of making
US3161950A (en) * 1960-04-01 1964-12-22 United Nuclear Corp Electron beam welding process
US3122423A (en) * 1960-04-04 1964-02-25 Beryllium Corp Method and apparatus for hot rolling high quality metal sheet
US3185652A (en) * 1960-04-29 1965-05-25 Nuclear Corp Of America Refractory rare earth material
US3349466A (en) * 1960-05-02 1967-10-31 Martin Marietta Corp Method of manufacturing aluminumclad nuclear fuel elements by hotswaging in air
US3210256A (en) * 1960-12-08 1965-10-05 Atomic Energy Authority Uk Manufacture of nuclear reactor fuel elements
US3210255A (en) * 1960-12-08 1965-10-05 Atomic Energy Authority Uk Manufacture of nuclear reactor fuel elements
US3151037A (en) * 1961-02-21 1964-09-29 Minnesota Mining & Mfg Encased fuel
US3336656A (en) * 1962-03-27 1967-08-22 Atomic Energy Authority Uk Manufacture of cermet bodies
US3199189A (en) * 1962-03-29 1965-08-10 Alloys Unltd Inc Gold alloy cladding
US3136051A (en) * 1962-10-11 1964-06-09 Frank B Quinlan Cladding of nuclear fuel elements
US3352004A (en) * 1963-08-09 1967-11-14 Commissariat Energie Atomique Process for cladding uranium rods
US3297543A (en) * 1964-07-07 1967-01-10 Babcock & Wilcox Co Plate-type nuclear fuel element
US3322951A (en) * 1964-08-28 1967-05-30 Paul M Yavorsky Efficient beta-ray emission source for irradiation applications
US3472734A (en) * 1964-10-22 1969-10-14 Kernforschungsanlage Juelich Fuel element for liquid-cooled nuclear reactors
US3413195A (en) * 1964-10-22 1968-11-26 Kernforschungsanlage Juelich Fuel or fertile element for nuclear reactors
US3522111A (en) * 1967-10-24 1970-07-28 Republic Steel Corp Method of making a composite metal product
US3601884A (en) * 1968-05-20 1971-08-31 Westinghouse Electric Corp Method of constructing parts suitable for high heat flux removal in arc heaters
US3602978A (en) * 1969-04-14 1971-09-07 Us Navy Method of forming bimetallic transition joints
EP0154267A2 (en) * 1984-03-07 1985-09-11 Nukem GmbH Method of manufacturing plate-shaped fuel elements for research reactors
EP0154267A3 (en) * 1984-03-07 1988-04-20 Nukem Gmbh Method of manufacturing plate-shaped fuel elements for research reactors
US5296310A (en) * 1992-02-14 1994-03-22 Materials Science Corporation High conductivity hydrid material for thermal management
US6075701A (en) * 1999-05-14 2000-06-13 Hughes Electronics Corporation Electronic structure having an embedded pyrolytic graphite heat sink material

Similar Documents

Publication Publication Date Title
US2820751A (en) Process for producing jacketed bodies
US5517541A (en) Inner liners for fuel cladding having zirconium barriers layers
US4675153A (en) Zirconium alloy fuel cladding resistant to PCI crack propagation
US5620536A (en) Manufacture of zirconium cladding tube with internal liner
US4664881A (en) Zirconium base fuel cladding resistant to PCI crack propagation
US5517540A (en) Two-step process for bonding the elements of a three-layer cladding tube
RU2239892C2 (en) Method for producing thin components from zirconium base alloy and plates produced by this method
US5475723A (en) Nuclear fuel cladding with hydrogen absorbing inner liner
US2915815A (en) Method of making fuel elements
JPH0843567A (en) Manufacture of coating pipe
US4613479A (en) Water reactor fuel cladding
US5805656A (en) Fuel channel and fabrication method therefor
US2873238A (en) Method of making jacketed fissionable slug
US3115702A (en) Production of composite metal sheet or strip
US7100670B1 (en) Method for fabricating uranium foils and uranium alloy foils
US3200491A (en) Cladding process
US3136051A (en) Cladding of nuclear fuel elements
US3091847A (en) Method of manufacture of metal encased core material
US2846762A (en) Metal plating process
NO133808B (en)
US3154845A (en) Method of fabricating a fuel element
JPS60122386A (en) Control body for absorbing neutron
JPS61207989A (en) Water cooling type reactor fuel coated material
Komuro Welding of zirconium alloys
US3344508A (en) Process for producing cladded fuel elements