US3141236A - Method of cladding - Google Patents

Method of cladding Download PDF

Info

Publication number
US3141236A
US3141236A US33133A US3313360A US3141236A US 3141236 A US3141236 A US 3141236A US 33133 A US33133 A US 33133A US 3313360 A US3313360 A US 3313360A US 3141236 A US3141236 A US 3141236A
Authority
US
United States
Prior art keywords
core
jacketed
rod
jacket
explosive
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
US33133A
Inventor
Brian B Dunne
Perry B Ritter
Ronald A Kelsey
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.)
General Dynamics Corp
Original Assignee
General Dynamics Corp
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 General Dynamics Corp filed Critical General Dynamics Corp
Priority to US33133A priority Critical patent/US3141236A/en
Application granted granted Critical
Publication of US3141236A publication Critical patent/US3141236A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • 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
    • B23K20/06Non-electric welding by applying impact or other pressure, with or without the application of heat, e.g. cladding or plating by means of high energy impulses, e.g. magnetic energy
    • B23K20/08Explosive welding
    • 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
    • Y10T29/49805Shaping by direct application of fluent pressure
    • 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
    • Y10T29/49908Joining by deforming
    • Y10T29/49925Inward deformation of aperture or hollow body wall
    • Y10T29/49927Hollow body is axially joined cup or tube
    • Y10T29/49929Joined to rod

Definitions

  • This invention relates to a method of cladding which is of particular value for applying coverings of metal or other similar materials to objects of irregular shape or of non-uniform cross section.
  • the object of this invention is to provide a convenient, economical and efficient method of applying a protective jacket or other relatively thin metal covering to an object made of a rigid material such as metal, for example, a fuel rod of irregular cross section such as may be used in nuclear reactor.
  • a further object of the invention is to provide a cladding method as an incident to which method there is evacuated from the interior of the sleeve any air or other gas which might be present in or about the object in such amounts as might interfere with the efficient prac tice of the method, or which might later interfere with the use of the finished product.
  • these objects and results are effected by detonating an explosive charge within liquid in which there has been immersed the rigid metal object around which has been placed a jacket of deformable material such as loosely fitting metal sleeve.
  • a jacket of deformable material such as loosely fitting metal sleeve.
  • the pressure created within the liquid adjacent the jacketed object will almost instantaneously cause the jacket to be forced into intimate engagement with the exterior of the rigid object.
  • the space between the metal object and the jacket is preferably evacuated prior to the detonation of the explosive.
  • FIGURE 1 of the drawings represents a side view of a partial vertical section through a tank in which the fuel rod with its prospective shield has been assembled in a treatment tank before detonating the explosive;
  • FIGURE 2 is a plan view of the set-up shown in FIG- URE 1, partly in section, and taken through the line 2-2 of FIGURE 1;
  • FIGURE 3 is a side elevation, partly in section, of the jacketed fuel rod after the cladding has been applied and the ends of the cladding sleeve have been scaled by insertion of the upper and lower heads.
  • the fuel or meat of the rod is represented by the numeral 10 which, as shown in FIGURE 1, is provided with a series of circumferentially extending grooves 11. Except for the said grooves 11, the fuel rod 10 is in United States Patent "ice the form of a cylinder which may be two or more feet in length and one and one-half inches or more in diameter.
  • the sleeve or jacket 12 which can be of aluminum or other appropriate metal, has a wall thickness of about .030 inch, and has an interior diameter about 0.003 inch greater than that of the rod 10 so that it will loosely fit the exterior of the rod 10 whereby said core rod 10 may be easily slipped into the sleeve 12, as shown in FIG- URE 1.
  • the ends of the sleeve 12 are sealed. This may be done by means of a pair of end plates or discs 13 and 14 made of lucite or other suitable material. Each of these end plates is made with an internal circumferentially extending groove 15, preferably rectangular in cross section, and fitted at its inner end with an O-ring 16 or similar gasket serving as a seal to prevent air or other gas from leaking back.
  • the evacuated assembly with the sealing caps 13 and 14 still in place is now placed in a tank of water large enough so as to avoid distortions in the inwardly directed pressure waves which are subsequently formed in the water.
  • the assembly In the case of a rod one and one-half inches in diameter, the assembly should be completely surrounded by at least about twelve inches of water.
  • a pair of thin discs 18 and 19 are secured to the outer surfaces of the plates 13 and 14. These serve to position the explosive charge which, in the present instance, comprises a plurality of, preferably three or more, vertically extending, generally parallel cords 20, 21 and 22, the upper ends of which are tied or otherwise brought together at the firing point 23.
  • the explosive charge which, in the present instance, comprises a plurality of, preferably three or more, vertically extending, generally parallel cords 20, 21 and 22, the upper ends of which are tied or otherwise brought together at the firing point 23.
  • these cords may be located in a cylindrical zone and about one inch from the sleeve or jacket 12, the cords being equally spaced around the axis and positioned at an angle of as shown in FIGURE 2.
  • the explosive cords are formed of an explosive which preferably has a relatively high detonation velocity, for example, such as that which is marketed by The Du Pont Company under the name Primacord and contains PETN (pentaerithritoltetranitrate). In the present case, it may have an outside diameter of about onequarter inch and contain about thirty grains of PETN per foot. It has been found that when this explosive cord is detonated at the firing point 23, the explosion will be propagated simultaneously at the same rate through each of the three explosive cords, and since the three cords are symmetrically positioned around the axis of the rod and of equal length, the shock waves from the three cords will be at the same level and the combined shock wave will travel progressively downward from the disc 18 to the disc 19. This will produce a sudden hydraulic pressure, around the jacketed rod, of about three to four kilobars above the yield point of the aluminum sleeve 12, causing it to flow plastically.
  • PETN pentaerithritoltetranitrate
  • the shock wave will travel down the Primacord cords at an extremely high velocity (about 6000 meters per second) whereas the propagation velocity through water is only about 1500 meters per second, the pressure around the sleeve will be well distributed and concentrated around the circumference of the outside of the sleeve with the result that the sleeve contracted onto the object.
  • seals preferably of the same metal as the sleeve 12, aluminum in this case, are then applied and welded in place in the ends of the sleeve, as
  • the air in the space between the object and the cladding may The expelleclby the progressive downward passage of the shock wave which will force the air between the rod and cladding to move downwardly as the cladding is In such a case, the prior evacuation of the air from the assembly will not be necessary.
  • a method of applying a tight-fitting layer of metal to a rigid elongated core which comprises inserting the core in a loose fitting jacket of malleable metal, evacuating the space defined between the core and the jacket, immersing the jacketed core in a liquid, providing a plurality of elongated bodies of an explosive substance which,are spaced from and which extend generally parallel to the jacketed core and which are positioned in generally equi-spaced relationship around the jacketed core, and simultaneously detonating said elongated bodies of explosive substance from the same ends to thereby provide a generally uniform shock wave in the liquid which extends around the jacketed core and which travels progressively along the length of the jacketed core to progressively contract the jacket into generally intimate contact with the core; L p n v 2.
  • a method of applying a tight-fitting layer of metal to a rigid elongated rod which comprises inserting the rod in a loose jacket of malleable metal, placing the jacketed rod in a tank of liquid, providing at least three explosive cords which are spaced from and which extend generally parallel to the jacketed rod and which are positioned in generally equi-spaced relationship around the jacketed rod, and simultaneously detonating said explosive cords from the same ends to thereby.
  • a method of applying a tight-fitting layer of metal to a rigid elongated rod which comprises inserting the vrod in a loose fitting jacket of malleable metal, evacuating the space defined between the rod and the jacket, placing the jacketed rod in a tank of liquid, providing at least three explosive cords which extend from a cornmon detonating point and which are spaced from and extend generally parallel to the jacketed rod and which are positioned in generally equi-spaced relationship around the jacketed rod, said explosiveco'rds extending along the entire length of the rod, and simultaneously detonating said explosive cords from said common detonating point to thereby provide a uniform shock wave in the liquid which extends, around the jacketed rod andrwhich travels progressively along the length of the jacketed rod to progressively contract the jacket into generally intimate contact with the rod.

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Pressure Welding/Diffusion-Bonding (AREA)

Description

y 21, 1964 B. B. DUNNE ETAL METHOD OF CLADDING 2 Sheets-Sheet 1 Filed June 1, 1960 .005 Climfg m m 7 mm? m MWZ 3B4, NVOm p w 50W 6?. {as
y 21, 1964 B. B. DUNNE ETAL METHOD OF CLADDING 2 Sheets-Sheet 2 Filed June 1. 1960 By PZ/F/PVB 7F/77Z WON/41D H KEZSfy S OMS andvbsm a oeals 3,141,236 NETHOD OF CLADDING Brian B. Dunne, San Diego, Perry E. Ritter, Encinitas,
and Ronald A. Kelsey, Del Mar, Califi, assignors to General Dynamics Corporation, New York, N.Y., a
corporation of Delaware Filed June 1, 1960, Ser. No. 33,133 3 Claims. (Cl. 29421) This invention relates to a method of cladding which is of particular value for applying coverings of metal or other similar materials to objects of irregular shape or of non-uniform cross section.
In the application of thin protective metallic sleeves or jackets, in certain cases, it is not possible to employ a rolling, swaging or extrusion process. This is particularly true in the case of an element of such character that it is either not feasible to use an extrusion process because of the nature of the product, or where the element is irregular in shape or has circumferential grooves or other indentations.
The object of this invention is to provide a convenient, economical and efficient method of applying a protective jacket or other relatively thin metal covering to an object made of a rigid material such as metal, for example, a fuel rod of irregular cross section such as may be used in nuclear reactor.
A further object of the invention is to provide a cladding method as an incident to which method there is evacuated from the interior of the sleeve any air or other gas which might be present in or about the object in such amounts as might interfere with the efficient prac tice of the method, or which might later interfere with the use of the finished product.
Other more specific objects and advantages of the invention will be disclosed as the description proceeds.
In general, it may be said that these objects and results are effected by detonating an explosive charge within liquid in which there has been immersed the rigid metal object around which has been placed a jacket of deformable material such as loosely fitting metal sleeve. When the explosive is detonated, the pressure created within the liquid adjacent the jacketed object will almost instantaneously cause the jacket to be forced into intimate engagement with the exterior of the rigid object. To avoid air pockets between the jacket and the metal object, the space between the metal object and the jacket is preferably evacuated prior to the detonation of the explosive.
The drawings which accompany this specification illustrate an embodiment of the invention which has successfully been employed in the cladding of nuclear reactor fuel rods, the exterior surfaces of which have exterior indentations, for example, in the present instance, circumferential grooves or recesses.
FIGURE 1 of the drawings represents a side view of a partial vertical section through a tank in which the fuel rod with its prospective shield has been assembled in a treatment tank before detonating the explosive;
FIGURE 2 is a plan view of the set-up shown in FIG- URE 1, partly in section, and taken through the line 2-2 of FIGURE 1; and
FIGURE 3 is a side elevation, partly in section, of the jacketed fuel rod after the cladding has been applied and the ends of the cladding sleeve have been scaled by insertion of the upper and lower heads.
Referring to the drawings, which disclose the invention as applied to the cladding of a nuclear reactor fuel rod, the fuel or meat of the rod is represented by the numeral 10 which, as shown in FIGURE 1, is provided with a series of circumferentially extending grooves 11. Except for the said grooves 11, the fuel rod 10 is in United States Patent "ice the form of a cylinder which may be two or more feet in length and one and one-half inches or more in diameter. The sleeve or jacket 12 which can be of aluminum or other appropriate metal, has a wall thickness of about .030 inch, and has an interior diameter about 0.003 inch greater than that of the rod 10 so that it will loosely fit the exterior of the rod 10 whereby said core rod 10 may be easily slipped into the sleeve 12, as shown in FIG- URE 1.
For the purpose of evacuating any gas, such as air, which may be contained within the grooves 11 or elsewhere in the assembled or jacketed rod, the ends of the sleeve 12 are sealed. This may be done by means of a pair of end plates or discs 13 and 14 made of lucite or other suitable material. Each of these end plates is made with an internal circumferentially extending groove 15, preferably rectangular in cross section, and fitted at its inner end with an O-ring 16 or similar gasket serving as a seal to prevent air or other gas from leaking back.
into the assembly after it has been evacuated. Such evacuation may be effected through a small pipe 17 in the upper lucite cover plate 13. It is not generally necessary to evacuate the assembly to a very low pressure. Evacuation to a level of the order of 1 mm. of mercury (absolute pressure) will ordinarily be sufiicient.
The evacuated assembly with the sealing caps 13 and 14 still in place is now placed in a tank of water large enough so as to avoid distortions in the inwardly directed pressure waves which are subsequently formed in the water. In the case of a rod one and one-half inches in diameter, the assembly should be completely surrounded by at least about twelve inches of water.
Before the sealed and evacuated assembly is lowered into the tank of water, a pair of thin discs 18 and 19 are secured to the outer surfaces of the plates 13 and 14. These serve to position the explosive charge which, in the present instance, comprises a plurality of, preferably three or more, vertically extending, generally parallel cords 20, 21 and 22, the upper ends of which are tied or otherwise brought together at the firing point 23. In the case of a rod one and one-half inches in diameter, and where three explosive cords are used, these cords may be located in a cylindrical zone and about one inch from the sleeve or jacket 12, the cords being equally spaced around the axis and positioned at an angle of as shown in FIGURE 2.
The explosive cords are formed of an explosive which preferably has a relatively high detonation velocity, for example, such as that which is marketed by The Du Pont Company under the name Primacord and contains PETN (pentaerithritoltetranitrate). In the present case, it may have an outside diameter of about onequarter inch and contain about thirty grains of PETN per foot. It has been found that when this explosive cord is detonated at the firing point 23, the explosion will be propagated simultaneously at the same rate through each of the three explosive cords, and since the three cords are symmetrically positioned around the axis of the rod and of equal length, the shock waves from the three cords will be at the same level and the combined shock wave will travel progressively downward from the disc 18 to the disc 19. This will produce a sudden hydraulic pressure, around the jacketed rod, of about three to four kilobars above the yield point of the aluminum sleeve 12, causing it to flow plastically.
In view of the fact that the shock wave will travel down the Primacord cords at an extremely high velocity (about 6000 meters per second) whereas the propagation velocity through water is only about 1500 meters per second, the pressure around the sleeve will be well distributed and concentrated around the circumference of the outside of the sleeve with the result that the sleeve contracted onto the object.
n) will be forced into close fitting intimate engagement with the rod As a result, the sleeve will be forced tightly into intimate contact with the rod 10 progressively threuLgrhout its entire length of two feet or more.
After the explosion has been effected, the assembly may be removed from the tank. To form the fuel element shown in FIGURE 3, seals, preferably of the same metal as the sleeve 12, aluminum in this case, are then applied and welded in place in the ends of the sleeve, as
jshown in FIGURE'3, Where 25 represents the seal at the upper end of the rod and 26 represents the seal at the lower end of the rod.
v In some instances, particularly when the object which is to be clad is of generally nniformpcross section, the air in the space between the object and the cladding may The expelleclby the progressive downward passage of the shock wave which will force the air between the rod and cladding to move downwardly as the cladding is In such a case, the prior evacuation of the air from the assembly will not be necessary.
' The method of cladding described above has been used to successfully clad objects of various shapes, including cruciform shaped rods, hexagonal rods, rods of rectangular cross section, rods provided with spiral grooves, rods provided with elongated fins, etc. It should be understood that the optimum number of explosive cords and the path of the cords relative to the object being clad will depend upon the specific shape of the object being clad. If the plurality of Primacord elements is such that they are adjacent, or nearly adjacent to one another,
they may be conveniently replaced by a thin sheet of 'or a sheet of the explosive material, one may use a single co-axial strand of the explosive material or a sheet of the explosive formed into a tubular shape.
Various of the features of the present invention believed to be new are set forth in theappended claims.
What is claimed is:
1. A method of applying a tight-fitting layer of metal to a rigid elongated core, which comprises inserting the core in a loose fitting jacket of malleable metal, evacuating the space defined between the core and the jacket, immersing the jacketed core in a liquid, providing a plurality of elongated bodies of an explosive substance which,are spaced from and which extend generally parallel to the jacketed core and which are positioned in generally equi-spaced relationship around the jacketed core, and simultaneously detonating said elongated bodies of explosive substance from the same ends to thereby provide a generally uniform shock wave in the liquid which extends around the jacketed core and which travels progressively along the length of the jacketed core to progressively contract the jacket into generally intimate contact with the core; L p n v 2. A method of applying a tight-fitting layer of metal to a rigid elongated rod, which comprises inserting the rod in a loose jacket of malleable metal, placing the jacketed rod in a tank of liquid, providing at least three explosive cords which are spaced from and which extend generally parallel to the jacketed rod and which are positioned in generally equi-spaced relationship around the jacketed rod, and simultaneously detonating said explosive cords from the same ends to thereby. provide a generally uniform shock wave in the liquid which extends around the jacketed rod and which travels progressively along the length of the jacketed rod to progressively contract the jacket into generally intimate contact with the rod while simultaneously exuding air from the space between the jacket and the rod.
3. A method of applying a tight-fitting layer of metal to a rigid elongated rod, which comprises inserting the vrod in a loose fitting jacket of malleable metal, evacuating the space defined between the rod and the jacket, placing the jacketed rod in a tank of liquid, providing at least three explosive cords which extend from a cornmon detonating point and which are spaced from and extend generally parallel to the jacketed rod and which are positioned in generally equi-spaced relationship around the jacketed rod, said explosiveco'rds extending along the entire length of the rod, and simultaneously detonating said explosive cords from said common detonating point to thereby provide a uniform shock wave in the liquid which extends, around the jacketed rod andrwhich travels progressively along the length of the jacketed rod to progressively contract the jacket into generally intimate contact with the rod.
References Cited in the file of this patent UNITED STATES PATENTS OTHER REFERENCES Explosives Form Space Age Shapes, Steel, Aug. 25, 1958, pages 82-86.
Explosive Forming, American Machinist, June 15, 1959, vol. 103, No. 12, pages 127-138.

Claims (1)

1. A METHOD OF APPLYING A TIGHT-FITTING LAYER OF METAL TO A RIGID ELONGATED CORE, WHICH COMPRISES INSERTING THE CORE IN A LOOSE FITTING JACKET OF MALLEABLE METAL, EVACUATING THE SPACE DEFINED BETWEEN THE CORE AND THE JACKET, IMMERSING THE JACKETED CORE IN A LIQUID, PROVIDING A PLURALITY OF ELONGATED BODIES OF AN EXPLOSIVE SUBSTANCE WHICH ARE SPACED FROM AND WHICH EXTEND GENERALLY PARALLEL TO THE JACKETED CORE AND WHICH ARE POSITIONED IN GENERALLY EQUI-SPACED RELATIONSHIP AROUND THE JACKETED CORE, AND SIMU-SPACED RELATIONSHIP AROUND THE JACKETED CORE, AND SIMULTANEOUSLY DETONATING SAID ELONGATED BODIES OF EXPLOSIVE SUBSTANCE FROM THE SAME ENDS TO THEREBY PROVIDE A GENERALLY UNIFORM SHOCK WAVE IN THE LIQUID WHICH EXTENDS AROUND THE JACKETED CORE AND WHICH TRAVELS PROGRESSIVELY ALONG THE LENGTH OF THE JACKETED CORE TO PROGRESSIVELY CONTRACT THE JACKET INTO GENERALLY INTIMATE CONTACT WITH THE CORE.
US33133A 1960-06-01 1960-06-01 Method of cladding Expired - Lifetime US3141236A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US33133A US3141236A (en) 1960-06-01 1960-06-01 Method of cladding

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US33133A US3141236A (en) 1960-06-01 1960-06-01 Method of cladding

Publications (1)

Publication Number Publication Date
US3141236A true US3141236A (en) 1964-07-21

Family

ID=21868728

Family Applications (1)

Application Number Title Priority Date Filing Date
US33133A Expired - Lifetime US3141236A (en) 1960-06-01 1960-06-01 Method of cladding

Country Status (1)

Country Link
US (1) US3141236A (en)

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3353258A (en) * 1964-02-17 1967-11-21 American Mach & Foundry Bowling pin
US3364561A (en) * 1966-02-10 1968-01-23 Du Pont Explosive tube bonding
US3431625A (en) * 1965-02-20 1969-03-11 Siemens Ag Method for the precise assembly of apparatus
US3439403A (en) * 1965-07-13 1969-04-22 Siemens Ag Magnetoform method assembly device
US5318213A (en) * 1990-11-30 1994-06-07 British Aerospace Public Limited Company Explosive bonding
US5706319A (en) * 1996-08-12 1998-01-06 Joseph Oat Corporation Reactor vessel seal and method for temporarily sealing a reactor pressure vessel from the refueling canal

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
SE105422C1 (en) * 1939-07-07 1942-09-08
US2367206A (en) * 1942-03-11 1945-01-16 Du Pont Method of joining objects
GB766741A (en) * 1954-12-23 1957-01-23 Martin Horeth Method of permanently connecting metal pipes
US2779279A (en) * 1952-03-08 1957-01-29 Paul S Maiwurm Apparatus for securing a tube or tubes in a body member
US2903843A (en) * 1957-10-01 1959-09-15 Du Pont Method for the preparation of seized metal-stranded cable
US3055095A (en) * 1957-11-29 1962-09-25 Jersey Prod Res Co Method of anchoring a well packer reinforcement

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
SE105422C1 (en) * 1939-07-07 1942-09-08
US2367206A (en) * 1942-03-11 1945-01-16 Du Pont Method of joining objects
US2779279A (en) * 1952-03-08 1957-01-29 Paul S Maiwurm Apparatus for securing a tube or tubes in a body member
GB766741A (en) * 1954-12-23 1957-01-23 Martin Horeth Method of permanently connecting metal pipes
US2903843A (en) * 1957-10-01 1959-09-15 Du Pont Method for the preparation of seized metal-stranded cable
US3055095A (en) * 1957-11-29 1962-09-25 Jersey Prod Res Co Method of anchoring a well packer reinforcement

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3353258A (en) * 1964-02-17 1967-11-21 American Mach & Foundry Bowling pin
US3431625A (en) * 1965-02-20 1969-03-11 Siemens Ag Method for the precise assembly of apparatus
US3439403A (en) * 1965-07-13 1969-04-22 Siemens Ag Magnetoform method assembly device
US3364561A (en) * 1966-02-10 1968-01-23 Du Pont Explosive tube bonding
US5318213A (en) * 1990-11-30 1994-06-07 British Aerospace Public Limited Company Explosive bonding
US5706319A (en) * 1996-08-12 1998-01-06 Joseph Oat Corporation Reactor vessel seal and method for temporarily sealing a reactor pressure vessel from the refueling canal

Similar Documents

Publication Publication Date Title
US3394569A (en) Forming method and apparatus
US4319660A (en) Mechanical noise suppressor for small rocket motors
US3141236A (en) Method of cladding
GB1364782A (en) Method for the production of fragmentation casings with utilisa tion of pre formed fragments
US6016753A (en) Explosive pipe cutting
GB1281002A (en) Method of subjecting solids to high dynamic pressures
US2891477A (en) Initiation device desensitized by fluids
US3495455A (en) Nuclear blast pressure simulator
AR199096A1 (en) METHOD AND APPARATUS FOR FORMING FINS ON THE EXTERIOR OF METALLIC TUBES AND THE TUBE SO OBTAINED
DE2241753B2 (en) Device for closing damaged heat exchanger pipes
CN108917500B (en) Lead core type blasting element and basic detonator composed of same
US3222144A (en) Polycellular tubular grid structures and method of manufacture
Benham et al. Experimental-theoretical correlation on the containment of explosions in closed cylindrical vessels
GB1247309A (en) A device for the shaping of workpieces
US3182392A (en) Method and apparatus for explosively bonding a plurality of metal laminae to uraniumalloy
ES472678A1 (en) Method for protecting the casing tubes of nuclear reactor fuel rods
US3090113A (en) Forming of metals
US3782283A (en) Defined disintegration of the casing of an explosive element
CN103639584A (en) Explosive cladding tube manufacturing process
DE2138924C3 (en) Pressure vessel for nuclear reactors
Baron et al. Explosive forming
USRE30380E (en) Mold for continuous casting of metal
US3206963A (en) Method and apparatus for explosive forming of metal articles
US3282743A (en) Process for relieving residual stresses in metals
US3433039A (en) Method and apparatus of forming integral ribs on tubes