US3197855A - Method of explosively forming a scarf type joint - Google Patents

Method of explosively forming a scarf type joint Download PDF

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US3197855A
US3197855A US248002A US24800262A US3197855A US 3197855 A US3197855 A US 3197855A US 248002 A US248002 A US 248002A US 24800262 A US24800262 A US 24800262A US 3197855 A US3197855 A US 3197855A
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plate
angular
plate end
connecting portion
forming
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US248002A
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William A Carter
William C Keathley
Jerry L Price
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Raytheon Technologies Corp
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United Aircraft Corp
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    • 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
    • Y10T29/49806Explosively shaping

Definitions

  • This invention relates to the formation of a joint between two materials capable of being joined by an explosive charge.
  • An object of this invention is to provide a method for connecting two metals which can be easily set up without elaborate preparations, and without costly equipment.
  • Another object of this invention is to provide a method of connecting two metal plates or sheets whereby the finished weld will be relatively strong in tension.
  • a further object of this invention is to provide a method whereby the plates or sheets of metal to be joined are each angularly positioned so that an explosive charge placed on the moving plate will bring the two plates or sheets into contact upon explosion and have them fixed together in a desired position
  • Another object of this invention is to provide means for holding the metals being joined toobtain a joint having a satisfactory strength in tension.
  • a further object of this invention is to provide a method of making a seam joint between two metal plates or sheets.
  • FIGURE 1 is a top view showing two metal plates or sheets positioned on a holding die in readiness for ignition of the explosive charge;
  • FIGURE 2 is a side view of the invention shown in FIGURE 1; l
  • FIGURE 3 is a side view showing the adaptability of the die to a curved surface
  • FIGURE 4 is a view showing the two plates or sheets of metal joined just after the firing of the explosive charge.
  • FIGURE 5 is a view showing the joint after the excess material has been machined off leaving a smooth scarf joint.
  • the holding die 6 has a recess 8 located in the face thereof for receiving the end of the plate 2.
  • This recess 8 is. formed having a first bottom surface 10 following the top surface of the die at a constantdist'an-ce therebelow equal to the height of the end wall 12, which extends upwardly from one end of said bottom surface, and having a second bottom surface 14 being inclined and extending upwardly from the other end of the'bottomsurface' 10 to the top surface of the die 6.
  • the length of the bottom surface 10 is made small since it does not form pa-rt of the finished joint.
  • the holding die 6 includes two sheet or plate-engaging devices 18 for fixedly holding each of the plates 2 and 4 3,197,855 Patented Aug. 3, 1965 to the base 20 of the die 6 during the firing of the explosive charge.
  • Each plate-engaging device 18 comprises a bar 22 which is pivoted to a bracket 24 extending upwardly from the base 20 of the die.
  • Each bracket 24 comprises two upstanding lugs,
  • the free end of each bar 22 has an attach-detach mechanism which engages a bracket 26 on the die.
  • a handle 28 is operable toengage or disengage the attach-detach device. While one specific holding device 18 has been shown,- it is to be understood that other desirable devices can be used.
  • the recess 8 is formed making the end wall 12 of a heighth approximately equal to the thickness of the plate 2 to be used. After this, the angle 9 is determined. Since it can be seen that the sine of G is equal to the thicknss of the plate '2 divided by the finished scarf weld length, as soon as a desired weld length has been selected and the thickness of the plate is known, the angle 6 can be easily figured. In preparing plates 2 and 4 to be placed on the die 6, the end of the plate 2 is formed having an offset portion 30 with an angular connecting portion 32.
  • the oifset portion 32 is formed so that the end of the plate 2 will be positioned against the end wall 12 of the recess and the bottom of the offset portion will engage the bottom surface 10 of the recess.
  • the angular connecting portion 32 is constructed to form an angle 9 with the offset portion and is formed of such a length so it will engage the second bottom surface 14.
  • the adjacent portion of the plate 2 connected to the angular connecting portion rests on the top-of the die 6.
  • the plate engaging device 18 contacts the plate 2 at this point.
  • the lower face of the main portion is located approximately on a plane with the upper face of the offset portion 20.
  • the plate 4 is then formed having an angular end portion.
  • This angular end portion 34 forms an angle or. with the angular connecting portion 32 of the plate 2. It can be seen then that the angular end portion 34 of plate 4 must be formed at an angle of 9 plus a to provide the proper angular relationship with the angular connecting portion 32 of plate 2.
  • Plate 4 is positioned so that the line at which the angular end portion extends upwardly is located adjacent the line at which the angular connecting portion 32 extends upwardly.
  • the flat portion of the plate 4 engages the top surface of the die at that point and the other plate-engaging device 18 fixedly holds the plate 4 in place. It is to be noted that the center line of plate 2 is now in line with the center line of plate 4.
  • An explosive 40 is placed over the face of the angular portion of plate 4 located away from the plate 2. This explosive extends over an area including the bend in the plate 4 to a location on said angular portion 34 including the length of the angular connecting portion 32 of plate 2. This distance from the bend including the port-ion 32, of course, is the finished scarf weld length.
  • This explosive can be of the flexible sheet type. One type is the Du Pont EL-606 series. Further information on this type of explosive is set forth in US. Patent No. 2,992,087. To prevent marking, marring, or burning of the plate 4, a fabric tape or other protective layer can be placed between the explosive sheet and the plate 4.
  • a line wave generator 46 is shown in FIGURES 1 and 2 to initiate an explosion simultaneously over the length of the sheet 46.
  • the generator shown is of the perforated equilateral triangle type. The perforations in the generator are so positioned that a detonation made at any one of the apexes will proceed as a straight line detonation zone to the opposite edge.
  • a detonator 48 is positioned at the apex of the line wave generator 46 which is opposite the side of the generator which is to simultaneously ignite the length of the explosive sheet 40.
  • the detonator 48 is held in position by a support 50.
  • This support can be a block of clay Which can be manuallykneaded or manipulated to properly fit any location at which a detonator needs support.
  • the detonator 48 can be of the standard commercial type which is ignited by the closing of a circuit at a control point located a safe distance from the detonator and resulting explosion. Other types of detonators can be used such as the fuse initiated type.
  • the angle at which the best test joint was formed can be used while varying the thickness of the sheet on either side of the thickness which was originally used. For example, one test can then be set up with an explosive sheet having approximately 19 cal./in. .001 thickness using .a thickness of 1 /2 times the thickness of the rn-oving plate and another test can be set up with an explosive sheet having a thickness of 2 /2 times the thickness of the moving plate.
  • a comparison can be made between the two tests to determine the better joint formed. Then tests can be made in that direction, that is, in a direction calling for more or less explosive.
  • the angle of the moving plate with relation to the fixed plate will range between 2 and for a majority of the cases in which a joint is formed using subject invention. Further, experiments show that a satisfactory charge on the face of the moving plate will fall in the range of from 10 to 85 cal./in. .001 plate thickness in a majority of cases.
  • Angle a used 15 Sheet thickness of EL-S 06A: .200" (3) Material: 17-7PH Stainless Steel to 17-7PH Stainless Steel Thickness of plate: .048" Angle cc used: 10 ⁇ Sheet thickness of EL-506A: .084"
  • a holding die 6 which will permit a joint being made on a curved surface.
  • This die can be made circular or of other desired shapes. When made circular or of any other closed or restricted shape which makes the removal of the die diflicult, the die is made segmented to move out of engage? ment with the parts being joined.
  • plate-engaging devices 18 are used to fixedly hold each of the plates together.
  • the explosive charge 40 is located on the moving portion of plate 4 in the same manner as before and the detonato-r can be positioned with a wave generator or without as shown in FIGURE 3. In this figure, the detonator is located at a corner of the sheet of explosive.
  • FIGURE 4 shows the two plates or sheets of metal joined after the explosion and FIGURE 5 shows the joint with the weld length extending tor a distance equal to approximately the length of the bottom surface 14 of the die 6.

Description

g- 3, 1965 w. A. CARTER ETAL 3,197,855
METHQD 0F EXPLOSIVELY FORMING A SCARF TYPE JOINT Filed Dec. 28. 1962 INV TORS WILLIAM CARTER WILLIAM ATHLEY JERRY F .CE
United States Patent 3,197,855 METHOD OF EXPLOSIVELY FORMING A SCARF TYPE JOINT William A. Carter and William C. Keathley, North Palm Beach, and Jerry L. Price, Lake Park, Fla., assignors to United Aircraft Corporation, East Hartford, Conn., a
corporation of Delaware Filed Dec. 28, 1962, Ser. No. 248,002 11 Claims. (Cl. 29-470.1)
This invention relates to the formation of a joint between two materials capable of being joined by an explosive charge.
An object of this invention is to provide a method for connecting two metals which can be easily set up without elaborate preparations, and without costly equipment.
Another object of this inventionis to provide a method of connecting two metal plates or sheets whereby the finished weld will be relatively strong in tension.
A further object of this invention is to provide a method whereby the plates or sheets of metal to be joined are each angularly positioned so that an explosive charge placed on the moving plate will bring the two plates or sheets into contact upon explosion and have them fixed together in a desired position Another object of this invention is to provide means for holding the metals being joined toobtain a joint having a satisfactory strength in tension.
A further object of this invention is to provide a method of making a seam joint between two metal plates or sheets.
Other objects and advantages will be apparent from the specification and from the accompanying drawings which illustrate the invention.
FIGURE 1 is a top view showing two metal plates or sheets positioned on a holding die in readiness for ignition of the explosive charge;
FIGURE 2 is a side view of the invention shown in FIGURE 1; l
FIGURE 3 is a side view showing the adaptability of the die to a curved surface; I
FIGURE 4 is a view showing the two plates or sheets of metal joined just after the firing of the explosive charge; and
FIGURE 5 is a view showing the joint after the excess material has been machined off leaving a smooth scarf joint.
In the field of explosively joining metals, some work has been done which was reported, for example, in an article entitled Explosive Bonding Gains Ground Through Simplified Setups, which appeared in the May 31, 1962, issue of The Iron Age. Another article of interest is one entitled Now Its Explosive Welding, and this article appeared in the April 17, 1961, issue of American Machinist/Metalworking Manufacturing.
With reference to FIGURES l and 2, two plates 2 and 4 are shown fixedly positioned in a holdingdie 6. The holding die 6 has a recess 8 located in the face thereof for receiving the end of the plate 2. This recess 8 is. formed having a first bottom surface 10 following the top surface of the die at a constantdist'an-ce therebelow equal to the height of the end wall 12, which extends upwardly from one end of said bottom surface, and having a second bottom surface 14 being inclined and extending upwardly from the other end of the'bottomsurface' 10 to the top surface of the die 6. The length of the bottom surface 10 is made small since it does not form pa-rt of the finished joint.
The holding die 6 includes two sheet or plate-engaging devices 18 for fixedly holding each of the plates 2 and 4 3,197,855 Patented Aug. 3, 1965 to the base 20 of the die 6 during the firing of the explosive charge. Each plate-engaging device 18 comprises a bar 22 which is pivoted to a bracket 24 extending upwardly from the base 20 of the die. Each bracket 24 comprises two upstanding lugs, The free end of each bar 22 has an attach-detach mechanism which engages a bracket 26 on the die. A handle 28 is operable toengage or disengage the attach-detach device. While one specific holding device 18 has been shown,- it is to be understood that other desirable devices can be used.
'In making a holding die 6 with which to practice the disclosed method of joining two plates, the recess 8 is formed making the end wall 12 of a heighth approximately equal to the thickness of the plate 2 to be used. After this, the angle 9 is determined. Since it can be seen that the sine of G is equal to the thicknss of the plate '2 divided by the finished scarf weld length, as soon as a desired weld length has been selected and the thickness of the plate is known, the angle 6 can be easily figured. In preparing plates 2 and 4 to be placed on the die 6, the end of the plate 2 is formed having an offset portion 30 with an angular connecting portion 32. The oifset portion 32 is formed so that the end of the plate 2 will be positioned against the end wall 12 of the recess and the bottom of the offset portion will engage the bottom surface 10 of the recess. The angular connecting portion 32 is constructed to form an angle 9 with the offset portion and is formed of such a length so it will engage the second bottom surface 14. The adjacent portion of the plate 2 connected to the angular connecting portion rests on the top-of the die 6. The plate engaging device 18 contacts the plate 2 at this point. When the end of plate 2 has been prepared, the lower face of the main portion is located approximately on a plane with the upper face of the offset portion 20. g
The plate 4 is then formed having an angular end portion. This angular end portion 34 forms an angle or. with the angular connecting portion 32 of the plate 2. It can be seen then that the angular end portion 34 of plate 4 must be formed at an angle of 9 plus a to provide the proper angular relationship with the angular connecting portion 32 of plate 2. Plate 4 is positioned so that the line at which the angular end portion extends upwardly is located adjacent the line at which the angular connecting portion 32 extends upwardly. The flat portion of the plate 4 engages the top surface of the die at that point and the other plate-engaging device 18 fixedly holds the plate 4 in place. It is to be noted that the center line of plate 2 is now in line with the center line of plate 4.
An explosive 40 is placed over the face of the angular portion of plate 4 located away from the plate 2. This explosive extends over an area including the bend in the plate 4 to a location on said angular portion 34 including the length of the angular connecting portion 32 of plate 2. This distance from the bend including the port-ion 32, of course, is the finished scarf weld length. This explosive can be of the flexible sheet type. One type is the Du Pont EL-606 series. Further information on this type of explosive is set forth in US. Patent No. 2,992,087. To prevent marking, marring, or burning of the plate 4, a fabric tape or other protective layer can be placed between the explosive sheet and the plate 4.
A line wave generator 46 is shown in FIGURES 1 and 2 to initiate an explosion simultaneously over the length of the sheet 46. The generator shown is of the perforated equilateral triangle type. The perforations in the generator are so positioned that a detonation made at any one of the apexes will proceed as a straight line detonation zone to the opposite edge.
As shown in FIGURES 1 and 2, a detonator 48 is positioned at the apex of the line wave generator 46 which is opposite the side of the generator which is to simultaneously ignite the length of the explosive sheet 40. The detonator 48 is held in position by a support 50. This support can be a block of clay Which can be manuallykneaded or manipulated to properly fit any location at which a detonator needs support. The detonator 48 can be of the standard commercial type which is ignited by the closing of a circuit at a control point located a safe distance from the detonator and resulting explosion. Other types of detonators can be used such as the fuse initiated type.
In determining a satisfactory angle or and a satisfactory amount of explosives to be placed on the upper face of the angular portion of moving plate 4, it is necessary to know the material of each of the plates 2 and 4. One way of determining a satisfactory angle a and satisfactory amount of explosive is to perform a series of tests as follows:
' (1) obtain sample pieces of the materials to be joined representing plates 2 and 4;
(a) for one set of pieces turn up the moving end of plate 4 so that it forms an angle of 5 with plate 2; and
(b) for another set of pieces turn up the moving end of plate 4 so that it forms an angle of with plate 2;
(2) place a sheet of explosive having approximately 19 cal./in. /.0O1 sheet thickness over the proper area of each plate 4 having a thickness of approximately twice the thickness of the moving plate 4. It is to be understood that if an explosive sheet is used having approximately 38 ca-l./in. .001 thickness then the sheet is made the thickness of the plate 4; and
i (3) detonate each sheet of explosive and examine the joint formed if any;
(a) if either of the testsresults in the formation of a joint which is satisfactory, then a predetermined charge and a predeterminedangle are known which will explosively join the two metals so tested; and
(b) if one joint was formed, but it is not quite a satisfactory one, then set up two more tests to be run, with an angle of 2 above and 2 below the original angle setting. For example, if the 15 joint was found to be the better of the two, then angles of 13 and 17 should then be tried. As these are inspected, the same considerations are taken into effect for another joint formation inthe event a satisfactory one was not obtained by the last two tests. Changing the angle is not the only variable to be considered, since the thickness of the explosive sheet can also be varied, which is in effect changing the amount of explosive which will react on the face of the moving plate. If a satisfactory joint is not formed by some angle using the explosive sheets above which were approxiinately twice the thickness of the moving plate, then the angle at which the best test joint was formed can be used while varying the thickness of the sheet on either side of the thickness which was originally used. For example, one test can then be set up with an explosive sheet having approximately 19 cal./in. .001 thickness using .a thickness of 1 /2 times the thickness of the rn-oving plate and another test can be set up with an explosive sheet having a thickness of 2 /2 times the thickness of the moving plate. Here, as before, a comparison can be made between the two tests to determine the better joint formed. Then tests can be made in that direction, that is, in a direction calling for more or less explosive.
Experiments indicate that of the metals capable of being explosively joined, the angle of the moving plate with relation to the fixed plate will range between 2 and for a majority of the cases in which a joint is formed using subject invention. Further, experiments show that a satisfactory charge on the face of the moving plate will fall in the range of from 10 to 85 cal./in. .001 plate thickness in a majority of cases.
Materials which have been explosively joined are the following:
Dissimilar metals Beryllium Copper/ Haynes 25 Beryllium Copper/606.1 Aluminum (T6) Beryllium Copper/347 Stainless Steel Tantalum/347 Stainless Steel Tantalum/Columbium- 1 Zirconium Tantalum/Haynes 25 Tantalum/Hastelloy N Tantalum/Inconel 718 Colum-bium-1% Zirconium /Hastelloy N Columbium-l Zirconium/Inconel 718 347 Stainless Steel/ 6061 Aluminum (T6) 347 Stainless Steel/ Haynes 25 347 Stainless Steel/Inconel X 347 Stainless Steel/Hastelloy X 347 Stainless Steel/Inconel Haynes 25/ 6061 Aluminum (T6) Haynes .25 Greek Ascoloy Haynes 25 Hastelloy X Inconel X/Haynes 25 Inconel X/Waspaloy (21) Inconel X/ Greek Ascoloy (22) Waspaloy/Greek Ascoloy (23) Greek Ascoloy/347 Stainless Steel (24) Greek Ascoloy/Haynes 25 (25) Inconel/Inconel X (26) Waspaloy/Hastelloy X Similar metals Examples are set forth below showing materials on which subject invention has been used:
(1) Material: 347 Stainless Steel to 347 Stainless Steel 7 Thickness of plate: .050
Angle a used: 20 Sheet thickness of EL-506A: .200"
(2) Material: Waspaloy to Waspaloy Thickness of plate: .050"
Angle a used: 15 Sheet thickness of EL-S 06A: .200" (3) Material: 17-7PH Stainless Steel to 17-7PH Stainless Steel Thickness of plate: .048" Angle cc used: 10 {Sheet thickness of EL-506A: .084"
While one way of determining a predetermined angle or and amount of explosive has been set forth, it is to be understood that other ways can also be used. For two plates to be explosively joined, there is a range of satisfactory angles on and of explosive charge amounts.
'With reference to FIGURE 3, a holding die 6 is shown which will permit a joint being made on a curved surface. This die can be made circular or of other desired shapes. When made circular or of any other closed or restricted shape which makes the removal of the die diflicult, the die is made segmented to move out of engage? ment with the parts being joined. As in the die shown in FIGURES 1 and 2, plate-engaging devices 18 are used to fixedly hold each of the plates together. The explosive charge 40 is located on the moving portion of plate 4 in the same manner as before and the detonato-r can be positioned with a wave generator or without as shown in FIGURE 3. In this figure, the detonator is located at a corner of the sheet of explosive.
FIGURE 4 shows the two plates or sheets of metal joined after the explosion and FIGURE 5 shows the joint with the weld length extending tor a distance equal to approximately the length of the bottom surface 14 of the die 6. i i
It is to be understood that the invention is not limited to the specific form herein illustrated and described, but may be used in other ways without de'par-ture from its spirit as defined by the following claims.
We claim: I t
1. Method of joining metal plate ends capable of being explosively joined: I
(a) forming a first plate end with an offset portion having an .angular connecting portion;
-(b) form-ing a second plate end with an tending portion; Y i
(c) placing said second plate end i on the oflset portion of said first plate end with the angular portion forming an angle with the angular connecting portion of the first plate end;
(d) supporting thefirst plate end under the ofiset portion, angular connecting portion, and adjacent plate portion;
(e). placing an explosive charge over the face of the angular portion of said second plate end remote from said first plate end to move said angular portion of said second plate end into joining engagement with the angular connecting portion of said first plate end; i
( f) fixingsaid plate ends .in position; and
g) igniting said explosive charge.
2. Method of joining metal plate ends capable of being explosively j oined:
(a) forming a first plate end with an offset having an angular .connecting portion;
(b) torming a. second plate end with an angular extending portion;
(c) placing said second plate end on the .oifset portion of said first plate end with the angular portion forming an angle with the angular connecting portion of the first plate end;
(d) supporting the first plate end under the offset portion, angular connecting portion, and adjacent plate portion;
(e) placing an explosivecharge over the face of the angular portion of said second plate end facing away from said first plate end to move said angular portion of said second plate end into joining engagement with the angular connecting portion of said first plate end;
(f) fixing said plate ends in position;
(g) igniting said explosive charge; and
('h) removing the excess portion of the overlapped plate ends to form a scar-f joint.
3. Method of joining metal plate ends capable of bein g explosively joined:
(a) forming a first plate end with an offset portion having an angular connecting portion;
(b) forming a second plate end with an angular extending portion;
(c) placing said second plate end on the offset portion of said first plate end with the angular portion forming a predetermined angle with the angular connecting portion of the first plate end;
(d) supporting the first plate end under the offset portion, angular connecting portion, and adjacent plate portion;
(e) placing an explosive charge over the face of the angular exportion 6 angular portion of said second plate end facing away from said first plate end to move said angular portion of said second plate end into joining engagement with the angular connecting portion of said first plate end;
(f) fixing said plate ends in position; and
(-g) igniting said explosive charge.
4. Method of joining metal plate ends capable of being explosively joined:
(a) forming a first plate end with an offset portion having an angular connecting portion;
(0) forming a second plate end with an angular extending portion;
(0) placing said second plate end on the offset portion of said first plate end with the angular portion forming an angle with the angular connecting portion of the first plate end;
(d) supporting the first plate end under the ofiset portion, angular connecting portion, and adjacent plate portion;
(e) placing a predetermined explosive charge over the face of the angular. portion of said second plate end facing away from said first plate end to move said angular portion of said second plate end into joining engagement with the angular connecting portion of said first plate end;
(f) fixing said plate ends in position; and
(g) igniting said explosive charge.
5. Method of joining metal plate ends capable of being explosively joined:
(a) forming a first plate end with an offset portion having an angular connecting portion;
(b) forming a second plate end with an angular extending portion;
(c) placing said second plate end on the olfset portion of said first plate end with the angular portion forming a predetermined angle with the angular connecting portion of the first plate end;
(d) supporting the first plate under the ofiset portion,
angular connecting portion, and adjacent plate portion;
(e) placing a predetermined explosive charge over the face of the angular portion of said second plate end 'facing away from said first plate end to move said angular portion of said second plate end into joining engagement with the angular connecting portion of said first plate end,
(f fixing said plate ends in position; and
(g) igniting said explosive charge.
6. Method of joining metal plate ends capable of being explosively joined:
(a) forming a first plate and with an ofiset portion having an angular connecting portion with a predetermined angular setting;
(b) forming a second plate end with an angular extending portion; i
(c) placing said second plate end on the offset portion of said first plate end with the angular end portion forming an angle with the angular portion forming an angle with the angular connecting portion of the first plate end;
(d) supporting the first plate end under the offset portion, angular connecting portion, and adjacent plate portion;
(e) placing an explosive charge over the face of the angular portion of said second plate end facing away from said first plate end to move said angular portion of said second plate end into joining engagement with the angular connecting portion of said first plate end;
(i) fixing said plate ends in position; and
(g) igniting said explosive charge.
7. Method of joining metal plate ends capable of being explosively joined:
(a) forming a first plate end with an offset portion having an angularconnecting portion with a predetermined angular setting;
(b) forming a'second'plate end with an angular extending portion With a predetermined angular setting;
(c) placing said second plate end on the offset portion of said first plate end With the angular portion forming an angle with the angular connecting'portion of the first plate end;
(d) supporting the first plate end under the otfset portion, angular connecting portion, and adjacent plate portion;
(e) placing an explosive charge over the face of the angular portion of said second plate end facing away from said first plate end to move said angular portion of said second plate end into joining engagement with the angular connecting portion of said first plate end;
(g) igniting said explosive charge.
8. Method of joining metal plate ends capable of being explosively joined:
(a) forming a first plate end with an offset portion having an angular connecting portion With a predetermined angular setting;
(b) forming a second plate end with an angular extending portion with a predetermined angular setting;
(c) placing said second plate end on the offset portion of said first plate end with the angular portion forming an angle with the angular connecting portion of the first plate end;
(d) supporting the first plate end under the offset portion, angular connecting portion, and adjacent plate portion;
(e) placing a predetermined explosive charge over the face of the angular portion of said second plate end facing away from saidfirst plate end to move said angular portion of said second plate end into joining engagement with the angular connecting portion of said first plate end;
(f) fixing said plateendsinposition; and
(g) igniting said explosive charge.
9. Method of joining metal plate ends capable of being explosivelyjoined: I
(a) forming a first plate end with an offset port1on having an angular connecting portion with a predetermined angular setting; r
(b) forming a second plate end with an angular extending portion with a predetermined angular setting;
(c)'.placing said second plate end on the offset portion of said first plate end with the angular portion forming an angle with the angular connecting portion of the first plate end;
(d) supporting the first plate end under the offset portion, angular connecting portion, and adjacent plate portion;
(e) placing a predetermined explosive charge over the face of the angular portion of said second plate end facing away from said first plate end to move said angular portion of said second plate end into joining engagement with the angular connecting portion of said first plate end;
(f) fixing said plate ends in position;
(g) igniting said explosive charge; and
(h) removing the excess portion of the overlapped plate ends to form a scarf joint.
explosively joined:
- (a) forming a first plate end with an offset portion having an angular connecting portion so' that the offset portion is oifset by an amount approximately equal to the thickness of the first plate end;
(b) forming a second plate end having a thickness approximately equal to the thickness of the first plate end with an angular extending portion;
(c) placing said second plate end on the offset portion of said first plate end with the angular portion forming an angle with the angular connecting portion of the first plate end;
(d) supporting the first plate end and second plate end under the offset portion, angular connecting portion, and adjacent plate portions;
(e) placing an explosive charge over the face of the angular portion 'of saidsecond plate end remote from said first plate end to move rsaid angular portion of said second plate end lIltO joining engagement with the angular connecting portion of said first plate r r (f) fixing said plate ends in position;rand
(g) igniting said explosive charge.
11. Method of joining metalplate ends capable of being explosively joined:
(a) forming a first plate endshaving firstand second plate surfaces with an offset portionhaving an angular'connecting portionso" that! the firstsurface of the offset portion is in approximately the same'plane as the second surface of the platehaving'the first plate end; Y
(b) forming a secondplateiend having third and fourth plate surfaces with an angularextending:portion;
(c) placing said fourth plate surfaceof said second plate end on the first plate surface of saidoifset portion of said first .plate end'with'the angular portion forming an angle with the angularconnecting portion of. the firstlplate lend;
(d) supporting the second plate surface of said first plate end under'the offset portion, angular connecting portion, and'adjacent'plate portion;
(e) 'placing an explosive charge-overthe faceof the angular portion of said second plate end remote from said first plate-end to move'said angular portion of said second plate-end into joining engage- -ment with the, angular conneting portion of said first plate end;
(f) fixing said plate ends imposition; and
(g) igniting said explosive charge.
References Citedby theExaminer UNITED STATES PATENTS 2,535,836 712/50 Cameron et al 2l964 3,137,937 6/64 Cowan et al. 29486 OTHER REFERENCES Hayes & Pearson, Metallurgical Properties ofSome ,60 Explosivelyi Welded 'Metals, June -1962. ASTIA Report 278354.
Davenport et al., Explosive vWelding, SP l61. Pearson'Explo'sive Welding, SP7 60-159. (Both papers are in Section III of Advanced High v Energy" Rate Forming, published by American Society of Tool & Manufacturing Engineers.)
JOHN F CAMPBELL, Primary Examiner.
UNITED STATES PATENT OFFICE CERTIFICATE OF CORRECTION Patent No. 3,197,855 August 3, 1965 William A. Carter et al.
It is hereby certified that error appears in the above numbered patent requiring correction and that the said Letters Patent should read as corrected below.
Column 7, after line 18, insert the following:
(f) fixing said plate ends in position; and
(SEAL) Attest:
ERNEST W. SWIDER Attesting Officer EDWARD J. BRENNER Commissioner of Patents

Claims (1)

1. METHOD OF JOINING METAL PLATE ENDS CAPABLE OF BEING EXPOSIVELY JOINED: (A) FORMING A FIRST PLATE END WITH AN OFFSET PORTION HAVING AN ANGULAR CONNECTING PORTION; (B) FORMING A SECOND PLATE END WITH AN ANGULAR EXTENDING PORTION; (C) PLACING SAID SECOND PLATE END ON THE OFFSET PORTION OF SAID FIRST PLATE END WITH THE ANGULAR PORTION FORMING AN ANGLE WITH THE ANGULAR CONNECTING PORTION OF THE FIRST PLATE END; (D) SUPPORTING THE FIRST PLATE END UNDER THE OFFSET PORTION, ANGULAR CONNECTING PORTION, AND ADJACENT PLATE PORTION; (E) PLACING AN EXPLOSIVE CHARGE OVER THE FACE OF THE ANGULAR PORTION OF SAID SECOND PLATE END REMOTE FROM SAID FIRST PLATE END TO MOVE SAID ANGULAR PORTION OF SAID SECOND PLATE END INTO JOINING ENGAGE-MENT WITH THE ANGULAR CONNECTING PORTION OF SAID FIRST PLATE END; (F) FIXING SAID PLATE ENDS IN POSITION; AND (G) IGNITING SAID EXPLOSIVE CHARGE
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Cited By (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3258841A (en) * 1963-01-23 1966-07-05 Du Pont Method for explosively bonding metal layers
US3263324A (en) * 1963-01-23 1966-08-02 Du Pont Process for explosively bonding metal layers
US3281930A (en) * 1962-10-24 1966-11-01 Ici Ltd Joining clad metal parts
US3313021A (en) * 1964-03-02 1967-04-11 Stanford Research Inst Explosive butt welding
US3346946A (en) * 1964-01-17 1967-10-17 Dynamit Nobel Ag Method for connecting metal plates
US3358349A (en) * 1964-08-05 1967-12-19 Darlite Corp Method of explosion cladding irregular aluminum objects
US3364562A (en) * 1962-11-08 1968-01-23 North American Aviation Inc Method of making a butt joint by explosive welding
US3377693A (en) * 1964-09-24 1968-04-16 Asahi Kaseio Kogyo Kabushiki K Process for producing clad metal plates by explosive bonding
US3409975A (en) * 1966-08-23 1968-11-12 Air Force Usa Welding by high energy stress front
US3433384A (en) * 1966-08-02 1969-03-18 Reynolds Metals Co Cryogenic constructions and methods for making the same
US3434197A (en) * 1964-08-03 1969-03-25 Singer General Precision Explosive welding
US3477114A (en) * 1967-05-15 1969-11-11 Whittaker Corp Method and apparatus for edge-bonding metallic sheets
US3520049A (en) * 1965-10-14 1970-07-14 Dmitry Nikolaevich Lysenko Method of pressure welding
US3535767A (en) * 1965-08-19 1970-10-27 Aerojet General Co Method for joining metallic tubes by explosive bonding
US3842485A (en) * 1972-11-01 1974-10-22 Nasa Method of making an explosively welded scarf joint
CN103328146A (en) * 2012-01-16 2013-09-25 丰田自动车株式会社 Panel joining structure

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2535836A (en) * 1947-10-08 1950-12-26 Continental Can Co Method of and apparatus for soldering the side seams of can bodies
US3137937A (en) * 1960-10-26 1964-06-23 Du Pont Explosive bonding

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2535836A (en) * 1947-10-08 1950-12-26 Continental Can Co Method of and apparatus for soldering the side seams of can bodies
US3137937A (en) * 1960-10-26 1964-06-23 Du Pont Explosive bonding

Cited By (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3281930A (en) * 1962-10-24 1966-11-01 Ici Ltd Joining clad metal parts
US3364562A (en) * 1962-11-08 1968-01-23 North American Aviation Inc Method of making a butt joint by explosive welding
US3263324A (en) * 1963-01-23 1966-08-02 Du Pont Process for explosively bonding metal layers
US3258841A (en) * 1963-01-23 1966-07-05 Du Pont Method for explosively bonding metal layers
US3346946A (en) * 1964-01-17 1967-10-17 Dynamit Nobel Ag Method for connecting metal plates
US3313021A (en) * 1964-03-02 1967-04-11 Stanford Research Inst Explosive butt welding
US3434197A (en) * 1964-08-03 1969-03-25 Singer General Precision Explosive welding
US3358349A (en) * 1964-08-05 1967-12-19 Darlite Corp Method of explosion cladding irregular aluminum objects
US3377693A (en) * 1964-09-24 1968-04-16 Asahi Kaseio Kogyo Kabushiki K Process for producing clad metal plates by explosive bonding
US3535767A (en) * 1965-08-19 1970-10-27 Aerojet General Co Method for joining metallic tubes by explosive bonding
US3520049A (en) * 1965-10-14 1970-07-14 Dmitry Nikolaevich Lysenko Method of pressure welding
US3433384A (en) * 1966-08-02 1969-03-18 Reynolds Metals Co Cryogenic constructions and methods for making the same
US3409975A (en) * 1966-08-23 1968-11-12 Air Force Usa Welding by high energy stress front
US3477114A (en) * 1967-05-15 1969-11-11 Whittaker Corp Method and apparatus for edge-bonding metallic sheets
US3842485A (en) * 1972-11-01 1974-10-22 Nasa Method of making an explosively welded scarf joint
CN103328146A (en) * 2012-01-16 2013-09-25 丰田自动车株式会社 Panel joining structure
CN103328146B (en) * 2012-01-16 2014-07-09 丰田自动车株式会社 Panel joining structure
US8979416B2 (en) * 2012-01-16 2015-03-17 Toyota Jidosha Kabushiki Kaisha Panel joint structure

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