US2301565A - Method of making nosepieces for explosive bodies - Google Patents

Method of making nosepieces for explosive bodies Download PDF

Info

Publication number
US2301565A
US2301565A US374391A US37439141A US2301565A US 2301565 A US2301565 A US 2301565A US 374391 A US374391 A US 374391A US 37439141 A US37439141 A US 37439141A US 2301565 A US2301565 A US 2301565A
Authority
US
United States
Prior art keywords
nose
piece
nose piece
die
side walls
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
US374391A
Inventor
Charles H Moore
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.)
Lenape Hydraulic Pressing & Fo
Lenape Hydraulic Pressing & Forging Co
Original Assignee
Lenape Hydraulic Pressing & Fo
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 Lenape Hydraulic Pressing & Fo filed Critical Lenape Hydraulic Pressing & Fo
Priority to US374391A priority Critical patent/US2301565A/en
Application granted granted Critical
Publication of US2301565A publication Critical patent/US2301565A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B21MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21KMAKING FORGED OR PRESSED METAL PRODUCTS, e.g. HORSE-SHOES, RIVETS, BOLTS OR WHEELS
    • B21K21/00Making hollow articles not covered by a single preceding sub-group
    • B21K21/04Shaping thin-walled hollow articles, e.g. cartridges

Definitions

  • This invention relates to method of forming steel shapes, and particularly to the formatio of nose pieces for explosive bodies.
  • Explosive bombs to be dropped by aircraft for demolition purposes usually comprise elongated cylindrical bodies charged with high explosive or flammable material and equipped with detonating or ignition means operable to explode or ignite upon contact of the bomb with the target.
  • these bodies be so constructed as to oifer the least possible resistance to external pressures or influences, to travel true to the target at which they are directed with a minimum of deviation, and to withstand the shock of impact without collapsing upon reaching the objective.
  • the body is usually rounded or ogival and reenforced at its forward or contact end, and is equipped with fins or a tail piece to accurately steer the body in its flight.
  • the nose piece has been further proposed to form the nose piece from a flat circular disk of uniform thickness throughout, cutting away the surface from adjacent the center to the edges to produce a gradual thinning of the metal at the edges, and then forming the disk into the proper ogival shape. It is the purpose of the present invention to produce a nose piece having the required nose and side wall thicknesses, variations and shapes entirely by forging and extruding steps and to overcome the objections to the methods or processes heretofore adopted or proposed, and particularly to eliminate all expensive and time consuming machining operations, except for drilling and tapping the nose center for the application of the detonator.
  • Figure 1 is a. longitudinal section through a' typical three-piece welded explosive bomb, show ing particularly the desired shape and approximate proportions of the nose piece and its association with the bomb body,
  • Figure 2 is a sectional view taken through a ring die and showing the application thereto of a flat plate in the act of being operated upon in the first step of my improved process
  • Figure 3 is a view similar to Figure 2 and showing the plate as it will appear after the first operation
  • Figure 4 is a view similar to Figure 3 and showing the start of the next extruding opera- Figure 5 is a similar view showing the shape of the nose piece after the said extruding opera- Figure 6 is a similar view showing the start of the next extruding operation,
  • Figure 7 shows the shape and the approximate proportions of the nose pieceafter the said extruding operation.
  • gF-igure 8 is a sectional view showing the shape of the nose piece after the third extruding operation
  • Figure 9 is a sectional view through a shaping die preparatory to expanding the side walls of the nose piece to the desired diameter
  • Figure 10 is a sectional view through the nose piece after the various shaping, extruding and expanding operations
  • Figure 11 is a sectional view through a plate and a die of a coining press and illustrating a step which may be taken preliminary to the initial bowling or shaping step as above described, and
  • Figure 12 is a sectional view of the plate as it will substantially appear after the coining operation.
  • the nose piece is made of a single piece of metal, initially of uniform thickness throughout, and preferably in its initial form is of circular shape. This place will be of a thickness slightly greater than the tip or contact end of the nose piece in its finished form.
  • the plate I is first heated to a proper degree and is placed upon a ring die 15 with its center coaxial with the latter. The internal. diameter of this die which is uniform from one end to the other, will be such as to bowl or cupshape the plate when pressure is applied to the nose plug l1 centrally of the plate.
  • This nose piece will be of the shape and configuration generally approximating the internal surface of the end of the nose piece, but the said nose plug has straight slightly outwardly diverging walls as shown, to facilitate stripping as well as to produce a desired taper or flare in the side wall of the nose piece.
  • the plate Upon the application of pressure to the plate by the nose plug H, the plate will assume cup-shape as shown in Figure 3, and in so doing will be slightly drawn and thinned in being forced through the ring die. After this operation the piece will be stripped from the ring die I 8 and applied to a ring die is, having slightly smaller internal diameter, and forced through the said ring die by the same nose plug IT.
  • This operation produces a shape in the plate 55 as substantially shown in Figure 5, that is, the tip of the nose piece and the metal immediately adjacent thereto will be slightly reduced in thickness, while the side walls 18 will be somewhat thinned and extruded along the side of the nose plug ll.
  • the nose piece I5 is then removed from the ring die l8 and is applied to ring die 20 of still smaller internal diameter, the same nose plug I! being used to force the nose piece through the restricted opening, of the ring die it.
  • This operation produces a further slight thinning of the tip of the nose piece and the parts immediately adjacent thereto, but further extrudes and works the metal of the sides along the surfaces of the nose plug ll.
  • These several thinning and extruding steps are carried out in order to bring the side walls to substantially the thickness of the cylindrical bomb body, and, if desired or further necessary, the foregoing steps may be repeated with additional ring dies of decreasing internal diameter.
  • the plate l5 and the nose piece which is developed therefrom will be heated to a proper temperature in order that the desired results be accomplished. It will be appreciated that in these several operations upon the nose piece through the several dies of pro gressively smaller internal diameters, the metal drawn in the bowl portion and extruded along the sides of the nose plug will b worked and the fabric of the metal will be thus materially improved. Moreover, any fiaws or defects inherent in the .metal plate will be corrected by these working and extruding operations.
  • the resultant nose body I5 is applied to a shaping die such as is shown in Figure 9 and indicated at 22.
  • This die will have a cavity or recess of substantially the size and contour the finished nose piece should assume, and an expanding plug 23 conforming to the shape and size the interior of the completed piece shall be when properly centered in the nose piece, will expand the latter to shape in the die to substantially the shape shown in Figure 10 of the drawings. Any minor irregularities, deformations or bulges in the shape of the nose piece will be corrected by this final pressing operation, and it will be found that little, if any, machine work upon the nose piecewill be required. It will also be found.
  • the texture and tensile strength of the thinned side walls of the nose piece will be materially strengthened due to the drawing and extruding operations above described, and after the edges of the nose piece are trimmed, the piece may be readily and securely welded to the body to assume the final shape as shown generally in Figure l of the drawings. It is apparent that the application of pressure by the expanding plug 23 in a downward direction will, in its expanding operation, spread the metal and will also return metal to the side walls of the nose piece in a direction reverse of that in which the metal was worked in the earlier steps of the process. At the sam time, the nose piece will be shortened somewhat in this expanding operation, as will be obvious.
  • the metal blank prior to the first of the above described shaping and extruding steps, may be subjected to a coining operation.
  • This coining step is indicated generally in Figure 11, wherein represents the circular blank and 2 3 indicates the die of the coining press.
  • This die will be recessed substantially as shown at its central portion in order that the thickness of the corresponding portion of the blank 65 will not be disturbed, and it will be understood that the application of proper pressure by the die 25 will expand the plate l5 and reduce the thickness of the outer portions thereof as shown generally in Figure 12 of the drawings.
  • the method of shaping steel bodies from a circular plate consisting first of forcing the plate through successive dies each smaller than the preceding die with a die nose whose diameter is less than that of the smallest of said dies, and
  • the method of shaping a body from a steel plate of substantially uniform thickness consisting first in bending the plate into substantially cup-shape and at the same time thinning the side walls by drawing the metal thereof in one direction and without appreciably disturbing the thickness of the bottom of the cup, and then forcing some of the metal of the side walls toward the closed endof the cup.

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Shaping Metal By Deep-Drawing, Or The Like (AREA)

Description

C. H. MOORE Nov. 10, 1942.
METHOD OF MAKING NOSE PIECES FOR EXPLOSIVE BODIES 2 Sheets-Sheet l Filed Jan. 14, 1941 Nov. 10, 1942. c. H. MOORE 2,301,565
METHOD OF MAKING NOSE PIECES FOR EXPLOSIVE BODIES Filed Jan. 14, 1941 2 Sheets-Sheet 2 a 2 7 3mm i591" m 71 Patented Nov. 10, 1942 UNITED METHOD OF MAKING NOSEPIECES FOR EXPLOSIVE BODIES Charles H. Moore, West Chester, Pa., assignor to Lenape Hydraulic Pressing & Forging 00., Lenape, Pa., a corporation of Delaware Application January 14, 1941, Serial No. 374,391
Claims. (01. 29-131) This invention relates to method of forming steel shapes, and particularly to the formatio of nose pieces for explosive bodies.
Explosive bombs to be dropped by aircraft for demolition purposes usually comprise elongated cylindrical bodies charged with high explosive or flammable material and equipped with detonating or ignition means operable to explode or ignite upon contact of the bomb with the target.
It is desirable that these bodies be so constructed as to oifer the least possible resistance to external pressures or influences, to travel true to the target at which they are directed with a minimum of deviation, and to withstand the shock of impact without collapsing upon reaching the objective. To these ends, the body is usually rounded or ogival and reenforced at its forward or contact end, and is equipped with fins or a tail piece to accurately steer the body in its flight.
Originally, these bombs were made of a seamless one-piece steel forging, similar to gas or bottle tanks, but experiment showed that a bomb of greater strength could be more easily made in sections and welded together at considerable saving in time and expense. Such proposal includes a body, a tail piece, both of comparatively thin steel, and a nose piece, all separately formed and then assembled and welded together in a unitary body. The construction of the body and tail piece is a simple matter, but problems have presented themselves in the practical and economical formation of the nose piece, due principally to the fact that the tip or contact part of the nose piece must be sufliciently thick to withstand the shocks of impact, and the side walls thereof must be of gradually diminishing thickness as they round off and expand to the diameter of the body.
It has been proposed in the manufacture of such a nose piece to forge or cast the part to its approximate shape and dimension, and to then machine it to true form. Such procedure is attended with objections; principally, that it is difflcult to cast such a shape, with its varying thicknesses and irregular shape, without producing defects and weaknesses in the finished piece, and
also that the product requires considerable machine work before it can be assembled upon the body. Other proposals include the sli aping of the nose piece from a circular disk having a relatively 'thick center portion, the disk becoming'lt' progressively thinner toward its edges, and this blank has been spun or worked intoa nose piece, the center of the disk forming the nose tip. It
has been further proposed to form the nose piece from a flat circular disk of uniform thickness throughout, cutting away the surface from adjacent the center to the edges to produce a gradual thinning of the metal at the edges, and then forming the disk into the proper ogival shape. It is the purpose of the present invention to produce a nose piece having the required nose and side wall thicknesses, variations and shapes entirely by forging and extruding steps and to overcome the objections to the methods or processes heretofore adopted or proposed, and particularly to eliminate all expensive and time consuming machining operations, except for drilling and tapping the nose center for the application of the detonator. While the following is a description of the method as carried out in the construction of the nose piece of an explosive bomb, it will be understood that the invention may be equally as well employed in the formation of incendiary bombs, explosive shells and other bodies where a relatively heavy or thick nose tip and gradually diminishing or tapering side wall structure is required with a maximum of strength in all parts of the piece.
In the drawings:
Figure 1 is a. longitudinal section through a' typical three-piece welded explosive bomb, show ing particularly the desired shape and approximate proportions of the nose piece and its association with the bomb body,
Figure 2 is a sectional view taken through a ring die and showing the application thereto of a flat plate in the act of being operated upon in the first step of my improved process,
Figure 3 is a view similar to Figure 2 and showing the plate as it will appear after the first operation,
Figure 4 is a view similar to Figure 3 and showing the start of the next extruding opera- Figure 5 is a similar view showing the shape of the nose piece after the said extruding opera- Figure 6 is a similar view showing the start of the next extruding operation,
Figure 7 shows the shape and the approximate proportions of the nose pieceafter the said extruding operation.
gF-igure 8 is a sectional view showing the shape of the nose piece after the third extruding operation,
Figure 9 is a sectional view through a shaping die preparatory to expanding the side walls of the nose piece to the desired diameter,
Figure 10 is a sectional view through the nose piece after the various shaping, extruding and expanding operations,
Figure 11 is a sectional view through a plate and a die of a coining press and illustrating a step which may be taken preliminary to the initial bowling or shaping step as above described, and
Figure 12 is a sectional view of the plate as it will substantially appear after the coining operation.
As has been above stated, it is desirable in a structure of this type to provide a relatively thick wall at the tip of the nose piece, becoming progressively thinner toward the open end of the blank. This is in order that a maximum of strength is possessed by the contact part of the nose piece, and at the same time it is equally desirable that the thinner side walls of the nose piece possess a maximum of strength, or at least a strength equal to that of the body of the bomb.
In carrying out the invention, the nose piece is made of a single piece of metal, initially of uniform thickness throughout, and preferably in its initial form is of circular shape. This place will be of a thickness slightly greater than the tip or contact end of the nose piece in its finished form. The plate I is first heated to a proper degree and is placed upon a ring die 15 with its center coaxial with the latter. The internal. diameter of this die which is uniform from one end to the other, will be such as to bowl or cupshape the plate when pressure is applied to the nose plug l1 centrally of the plate. This nose piece will be of the shape and configuration generally approximating the internal surface of the end of the nose piece, but the said nose plug has straight slightly outwardly diverging walls as shown, to facilitate stripping as well as to produce a desired taper or flare in the side wall of the nose piece. Upon the application of pressure to the plate by the nose plug H, the plate will assume cup-shape as shown in Figure 3, and in so doing will be slightly drawn and thinned in being forced through the ring die. After this operation the piece will be stripped from the ring die I 8 and applied to a ring die is, having slightly smaller internal diameter, and forced through the said ring die by the same nose plug IT. This operation produces a shape in the plate 55 as substantially shown in Figure 5, that is, the tip of the nose piece and the metal immediately adjacent thereto will be slightly reduced in thickness, while the side walls 18 will be somewhat thinned and extruded along the side of the nose plug ll. The nose piece I5 is then removed from the ring die l8 and is applied to ring die 20 of still smaller internal diameter, the same nose plug I! being used to force the nose piece through the restricted opening, of the ring die it. This operation produces a further slight thinning of the tip of the nose piece and the parts immediately adjacent thereto, but further extrudes and works the metal of the sides along the surfaces of the nose plug ll. These several thinning and extruding steps are carried out in order to bring the side walls to substantially the thickness of the cylindrical bomb body, and, if desired or further necessary, the foregoing steps may be repeated with additional ring dies of decreasing internal diameter.
ployed in forcing the cup through the restricted die openings, and it will be observed that while the lower end of the cup obtains but slight difference in its original thicknessthe side walls have been materially thinned, extruded and out- The same nose piece H is emwardly flared along the side walls of the nose plug Hi.
It will be understood that throughout the several operations here described, the plate l5 and the nose piece which is developed therefrom will be heated to a proper temperature in order that the desired results be accomplished. It will be appreciated that in these several operations upon the nose piece through the several dies of pro gressively smaller internal diameters, the metal drawn in the bowl portion and extruded along the sides of the nose plug will b worked and the fabric of the metal will be thus materially improved. Moreover, any fiaws or defects inherent in the .metal plate will be corrected by these working and extruding operations.
After the last of the extruding steps, the resultant nose body I5 is applied to a shaping die such as is shown in Figure 9 and indicated at 22. This die will have a cavity or recess of substantially the size and contour the finished nose piece should assume, and an expanding plug 23 conforming to the shape and size the interior of the completed piece shall be when properly centered in the nose piece, will expand the latter to shape in the die to substantially the shape shown in Figure 10 of the drawings. Any minor irregularities, deformations or bulges in the shape of the nose piece will be corrected by this final pressing operation, and it will be found that little, if any, machine work upon the nose piecewill be required. It will also be found. that the texture and tensile strength of the thinned side walls of the nose piece will be materially strengthened due to the drawing and extruding operations above described, and after the edges of the nose piece are trimmed, the piece may be readily and securely welded to the body to assume the final shape as shown generally in Figure l of the drawings. It is apparent that the application of pressure by the expanding plug 23 in a downward direction will, in its expanding operation, spread the metal and will also return metal to the side walls of the nose piece in a direction reverse of that in which the metal was worked in the earlier steps of the process. At the sam time, the nose piece will be shortened somewhat in this expanding operation, as will be obvious.
The several steps of the process may result in a nose piece whose relatively thin side Walls too abruptly join the thicker portion of the body, or wherein a bulge may develop from metal in the piece which is not sufficiently thinned or worked in the extruding process. To obviate such occurrence, the metal blank, prior to the first of the above described shaping and extruding steps, may be subjected to a coining operation. This coining step is indicated generally in Figure 11, wherein represents the circular blank and 2 3 indicates the die of the coining press. This die will be recessed substantially as shown at its central portion in order that the thickness of the corresponding portion of the blank 65 will not be disturbed, and it will be understood that the application of proper pressure by the die 25 will expand the plate l5 and reduce the thickness of the outer portions thereof as shown generally in Figure 12 of the drawings.
From the foregoing it is apparent that the objections referred to in connection with known processes of producing nose pieces are generally overcome. The combined thinning and extruding operations upon the side walls of the nose piece, without appreciably disturbing the thickness or fabricof the operative end of the nose piece.
creates in the side walls such strength as will reduce to a minimum the possibility of failure or collapsing of such walls upon the bomb strik-v ing its target.
Having thus described my invention, what I claim as new and useful is:
l. The method of shaping steel bodies from a circular plate, consisting first of forcing the plate through successive dies each smaller than the preceding die with a die nose whose diameter is less than that of the smallest of said dies, and
then expanding the edges of the body thus formed by application of pressure by a plug larger than the diameter of the body in a direction opposite to that of the forcing operations.
2. The method of shaping a steel body from a steelplate, consisting of forming the body into cup-shape, forcing said cup through a ring die by an axially moving nose die whose clearance from the ring die is less than the thickness of said plate whereby the side walls are thinned and elongated, forcing said cup through additional ring dleslof successively reduced diameters by the same nose die to further thin and elongate said side walls, and flaring the side walls of the resultant body and simultaneously returning a,
stantially cup-shape, forcing the bowled plate through a ring die of less diameter than the cup with a nose plug of predetermined diameter, furtherforcing the cup with the same nose plug through a ring die of smaller diameter than the first, flaring the side walls of the cup to the desired finished diameter, and machining excess metal from the exterior of the nose piece thus formed.
4. The method of shaping abody from a steel plate of substantially uniform thickness, consisting first in bending the plate into substantially cup-shape and at the same time thinning and drawing the metal of the side walls of the cup in one direction without appreciably disturbing the thickness of the bottom, and then expanding the open end of the cup and simultaneously forcing some of the metal of the side walls toward the closed end of the cup.
5. The method of shaping a body from a steel plate of substantially uniform thickness, consisting first in bending the plate into substantially cup-shape and at the same time thinning the side walls by drawing the metal thereof in one direction and without appreciably disturbing the thickness of the bottom of the cup, and then forcing some of the metal of the side walls toward the closed endof the cup.
H. MOORE.
US374391A 1941-01-14 1941-01-14 Method of making nosepieces for explosive bodies Expired - Lifetime US2301565A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US374391A US2301565A (en) 1941-01-14 1941-01-14 Method of making nosepieces for explosive bodies

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US374391A US2301565A (en) 1941-01-14 1941-01-14 Method of making nosepieces for explosive bodies

Publications (1)

Publication Number Publication Date
US2301565A true US2301565A (en) 1942-11-10

Family

ID=23476601

Family Applications (1)

Application Number Title Priority Date Filing Date
US374391A Expired - Lifetime US2301565A (en) 1941-01-14 1941-01-14 Method of making nosepieces for explosive bodies

Country Status (1)

Country Link
US (1) US2301565A (en)

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2770034A (en) * 1952-03-14 1956-11-13 Lyon George Albert Method of coining and cupping metal
US2772470A (en) * 1951-12-17 1956-12-04 Lyon George Albert Metallic cartridge casings
US2941289A (en) * 1954-04-21 1960-06-21 Thomas B Chace Method of making clad metal cooking utensils
US2975511A (en) * 1957-11-15 1961-03-21 Motor Wheel Corp Method of making tapered wheel disks
US3058195A (en) * 1958-11-17 1962-10-16 Svenska Metallverken Ab Method for the manufacture from sheet metal of hollow objects having a wall thickness in the closed end exceeding the wall thickness of the starting material
US3137057A (en) * 1959-11-13 1964-06-16 Lyon Inc Manufacture of missile casings
US4365498A (en) * 1977-07-05 1982-12-28 Toyo Seikan Kaisha, Limited Method of manufacturing formed articles, equipment for practicing same, and formed articles manufactured by the method
EP0106411A2 (en) * 1982-10-18 1984-04-25 Schweizerische Eidgenossenschaft vertreten durch die Eidg. Munitionsfabrik Thun der Gruppe für Rüstungsdienste Small arms ammunition, and manufacturing process therefor

Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2772470A (en) * 1951-12-17 1956-12-04 Lyon George Albert Metallic cartridge casings
US2770034A (en) * 1952-03-14 1956-11-13 Lyon George Albert Method of coining and cupping metal
US2941289A (en) * 1954-04-21 1960-06-21 Thomas B Chace Method of making clad metal cooking utensils
US2975511A (en) * 1957-11-15 1961-03-21 Motor Wheel Corp Method of making tapered wheel disks
US3058195A (en) * 1958-11-17 1962-10-16 Svenska Metallverken Ab Method for the manufacture from sheet metal of hollow objects having a wall thickness in the closed end exceeding the wall thickness of the starting material
US3137057A (en) * 1959-11-13 1964-06-16 Lyon Inc Manufacture of missile casings
US4365498A (en) * 1977-07-05 1982-12-28 Toyo Seikan Kaisha, Limited Method of manufacturing formed articles, equipment for practicing same, and formed articles manufactured by the method
EP0106411A2 (en) * 1982-10-18 1984-04-25 Schweizerische Eidgenossenschaft vertreten durch die Eidg. Munitionsfabrik Thun der Gruppe für Rüstungsdienste Small arms ammunition, and manufacturing process therefor
EP0106411A3 (en) * 1982-10-18 1984-09-05 Eidgenoess Munitionsfab Thun Small arms ammunition, and manufacturing process therefor

Similar Documents

Publication Publication Date Title
US3143966A (en) Expanding bullet
US2366965A (en) Tubular rivet
US10369622B2 (en) Precision forged cartridge case
US3311962A (en) Method of making an expanding point bullet
US3399560A (en) Method of cold forming a solid ring
US2301565A (en) Method of making nosepieces for explosive bodies
US2668345A (en) Shell making process
US3072933A (en) Method of extruding shank portions with 50% or less cross-sectional area than that of the original blanks
US2748932A (en) Process and apparatus for cold shaping steel
US2170811A (en) Method of forming cold-worked articles
US2751676A (en) Method of cold working metal
US3036366A (en) Method of making ball studs
US2312094A (en) Method of making hollow propellers
US12070782B2 (en) Method for producing a hollow part made of a metal material and use of this method for producing a landing gear rod or beam
US3644973A (en) Method of making ball studs from metal rods
US2080850A (en) Manufacture of nuts
US2891298A (en) Method of cold shaping partitioned tubular steel articles
US3517536A (en) Method of machining the inside wall of a tube
US1365987A (en) Manufacture of gun-tubes and like tubular bodies
US2700211A (en) Propeller blade blank construction
US3032857A (en) Apparatus for forming integral ribs upon the circumference of a rigid tubular shape
US2958115A (en) Method for making bomb heads or the like
US1480843A (en) Method for the cold spurting of tubes and thin-walled metal pipes of lead, tin, and especially aluminium
US2361771A (en) Manufacture of rivets
US1437690A (en) Tubular forging and process for making the same