US3036360A - Shell nosing apparatus - Google Patents

Shell nosing apparatus Download PDF

Info

Publication number
US3036360A
US3036360A US27714A US2771460A US3036360A US 3036360 A US3036360 A US 3036360A US 27714 A US27714 A US 27714A US 2771460 A US2771460 A US 2771460A US 3036360 A US3036360 A US 3036360A
Authority
US
United States
Prior art keywords
shell
nosing
die
base
plunger
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
US27714A
Inventor
Lyon George Albert
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.)
Lyon Inc
Original Assignee
Lyon Inc
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
Priority claimed from US397248A external-priority patent/US2958115A/en
Application filed by Lyon Inc filed Critical Lyon Inc
Priority to US27714A priority Critical patent/US3036360A/en
Application granted granted Critical
Publication of US3036360A publication Critical patent/US3036360A/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
    • B21K21/06Shaping thick-walled hollow articles, e.g. projectiles

Definitions

  • the present invention relates to apparatus for nosing in large drawn metallic shells such as may be used for ordnance purposes and the like.
  • An important object of the present invention is to provide improved apparatus for nosing large size shells having thin tubular walls.
  • Another object of the invention is to provide novel means for taper-nosing thin wall, thickened nose drawn steel shells without collapsing the thin walls during the nosing operation.
  • FIGURE 1 is a vertical sectional view through a drawn shell and nosing apparatus embodying features of the invention
  • FIGURE 2 is a fragmentary side elevational view of the apparatus and shell of FIGURE 1;
  • FIGURE 3 is a vertical sectional view similar to FIG- URE l but showing the apparatus and the shell at the completion of the nosing stroke;
  • FIGURE 4 is a transverse sectional detail view taken substantially on the line IVIV of FIGURE 3.
  • a drawn shell which may be several feet in length and of proportionate diameter has a thickened bottom wall 13, a thinly drawn tubular wall 19 and a thickened initially externally cylindrical nose end portion 25.
  • the lower portion of the wall 19 is back tapered as at 24.
  • nosing apparatus including a die structure having means for supporting the base end portion of the shell 15 and comprising a base member 27 to which is attached a shell base supporting block 28 having there-in a cavity 29 shaped complementary to the back tapered portion 24 of the shell wall 19.
  • a stripper plunger 29a having attached to the lower end portion thereof an actuating rod 30 extending reciprocably through a bore 31 in the base member 27.
  • connection of the operating rod 30 to the stripper plunger 29a is effected through the medium of a reduced diameter head boss 32 on the rod extending into a complementary press-fit bore in the base of the plunger, with access to the tip of the head boss by a punch-out tool through an axial bore 33 opening through the top of the plunger 29a and norm-ally closed by a screw plug 34.
  • the plunger 2% normally rests solidly on the base member 27 so as solidly to support the headed base wall 13 of the shell to the external contour of which the tip or head end of the plunger 29a is complementary in shape.
  • a predetermined range of stripping reciprocation of the plunger 29a is enabled between opposing axially directed limit shoulders 34a and 35 on respectively the plunger and the base block 28 Within which the plunger is mounted.
  • nosing die block 37 supported by a head member 38 which may be operatively related to the ram of a press.
  • a nosing cavity 39 having the tapered shape to which it is desired finally to form the nose of the shell 15.
  • a stripper punch 4t Reciprocably mounted in normally retracted position at the tip or upper end of the cavity 39 is a stripper punch 4t) having a stem 41 projecting upwardly reciprocably through the head member 38 and carrying an upper or head end collar or head block 42.
  • the shell 15 is centered between the base block 28 and the nosing die 37 as seen in FIG. 1, and then nosing die and base block are relatively reciprocably closed toward one another, as for example, by driving of the nosing die toward the base block to efiect driving of the thickened nose portion 25 of the shell 15 into the nosing cavity 39 whereby the shell is taper nosed as shown in FIG. 3.
  • the tapered nose portion of the shell is provided with substantially increased wall thickness attaining maximum thickness at the nose tip of the shell. This affords adequate material for subsequent internal machining and threading to receive a fuse tip or plug or armor piercing point on the head.
  • the dies are separated, the stripper plunger 29a ejecting the shell from the base 28, and the stripper plunger 4% acting, after the shell has been carried by the nosing die '37 away from the base 2% to strip and eject the shell from the nosing die.
  • the sidewall 19 is supported against buckling during the greatest compression strain thereon during nosing.
  • the base block 28 and the nosing die 37 are provided with complementary cooperatively related, relatively axially movable alternating respective anti-buckling fingers 45 and 47 which become operative during the last portion of the nosing stroke of the die asseembly and by their symmetrical radial full external support of the side wall throughout the potential buckling zone as the nosing operation progresses to a conclusion prevent lateral or radial outward buckling of the shell.
  • the anti-buckling fingers 45 and 47 have their major transverse extent radial relative to the shell so that they are strongly resistant to radial outward force exerted thereagainst by the shell Wall 19.
  • a reinforcing annulus collar 48 which may, for convenience, be mounted about the fingers 47 of the nosing die and secured to the nosing die as best seen in FIGS. 1 and 3. Air p'ressure'relief through the reinforcing ring 48 is afforded through one or more exhaust ports 49 therethrough preferably adjacent to the roots of the fingers 47.
  • a base support for a shell, 21 nosing die relatively reciprocably disposed relative to the base support and having a nosing cavity therein, said cavity being adapted to nose a shell casing supported in said base support, and means on said base support and on said nosing die cooperable during nosing cooperation of said base support and said nosing die to supa port the shell against buckling, said means comprising a series of cooperating longitudinally extending supporting fingers disposed symmetrically for encompassing the Wall of a shell being nosed, with certain fingers of the series the shell against buckling, said means comprising a series of cooperating longitudinally extending supporting fingers disposed symmetrically for encompassing the wall of a carried by the'nose die and other fingers'of the series shell being nosed, with certain of the fingers comprising a set carried by the nosing die and other of the fingers comprising a set carried by the base support, and one of saidsets of fingers having a reinforcing annulus thereabout.

Description

May 29, 1962 Original Filed Dec. 9, 1953 G. A. LYON SHELL NOSING APPARATUS 2 Sheets-Sheet 1 17711 -52 IZQI'T George Alberz L901;
May 29, 1962 G. A. LYON v 3,036,360
SHELL NOSING APPARATUS Original Filed Dec. 9, 1953 2 Sheets-Sheet 2 I27 FE '77227 2- George Albert 5027 3,636,360 SHELL NGSING APPARATUS George Albert Lyon, Detroit, Mich, msignor to Lyon Incorporated, Detroit, Mich, a corporation of Deiaware Griginal application Dec. 9, 1953, Ser. No. 397,248 now Patent No. 2,958,115, dated Nov. 1, 1969.. Divided and this application May 9, 196%, Ser. No. 27,714
3 Ciairns. (ill. 21.21)
The present invention relates to apparatus for nosing in large drawn metallic shells such as may be used for ordnance purposes and the like.
This application is a division of my pending application Serial No. 397,248 filed December 9, 1953, 'now Patent 2,958,115.
An important object of the present invention is to provide improved apparatus for nosing large size shells having thin tubular walls.
Another object of the invention is to provide novel means for taper-nosing thin wall, thickened nose drawn steel shells without collapsing the thin walls during the nosing operation.
Other objects, features and advantages of the present invention will be readily apparent from the following detailed description of a preferred embodiment thereof taken in conjunction with the accompanying drawings, in which:
FIGURE 1 is a vertical sectional view through a drawn shell and nosing apparatus embodying features of the invention;
FIGURE 2 is a fragmentary side elevational view of the apparatus and shell of FIGURE 1;
FIGURE 3 is a vertical sectional view similar to FIG- URE l but showing the apparatus and the shell at the completion of the nosing stroke; and
FIGURE 4 is a transverse sectional detail view taken substantially on the line IVIV of FIGURE 3.
According to the present invention, a drawn shell which may be several feet in length and of proportionate diameter has a thickened bottom wall 13, a thinly drawn tubular wall 19 and a thickened initially externally cylindrical nose end portion 25. The lower portion of the wall 19 is back tapered as at 24.
As a final step in shaping of the shell 15 it is placed in nosing apparatus including a die structure having means for supporting the base end portion of the shell 15 and comprising a base member 27 to which is attached a shell base supporting block 28 having there-in a cavity 29 shaped complementary to the back tapered portion 24 of the shell wall 19. In the bottom portion of the cavity 29 is a stripper plunger 29a having attached to the lower end portion thereof an actuating rod 30 extending reciprocably through a bore 31 in the base member 27. Connection of the operating rod 30 to the stripper plunger 29a is effected through the medium of a reduced diameter head boss 32 on the rod extending into a complementary press-fit bore in the base of the plunger, with access to the tip of the head boss by a punch-out tool through an axial bore 33 opening through the top of the plunger 29a and norm-ally closed by a screw plug 34. At its base end the plunger 2% normally rests solidly on the base member 27 so as solidly to support the headed base wall 13 of the shell to the external contour of which the tip or head end of the plunger 29a is complementary in shape. A predetermined range of stripping reciprocation of the plunger 29a is enabled between opposing axially directed limit shoulders 34a and 35 on respectively the plunger and the base block 28 Within which the plunger is mounted.
Operatively cooperable in relatively reciprocable rela- 3,@3h,3h Patented May 29, 1962 tion with the base block 28 is a nosing die block 37 supported by a head member 38 which may be operatively related to the ram of a press. Within the nosing block '37 is a nosing cavity 39 having the tapered shape to which it is desired finally to form the nose of the shell 15. Reciprocably mounted in normally retracted position at the tip or upper end of the cavity 39 is a stripper punch 4t) having a stem 41 projecting upwardly reciprocably through the head member 38 and carrying an upper or head end collar or head block 42. A coiled compression spring 43 thrusting against the underside of the head 42 and at its opposite end within a recess 44 in the head member 33 about the stem 41 normally biases the plunger 40 into retracted position but is yieldable upon engagement of the head 42 with a stop (not shown) to enable projection of the stripping plunger 49 into the cavity 39 for ejecting the nosed shell therefrom.
In operation, the shell 15 is centered between the base block 28 and the nosing die 37 as seen in FIG. 1, and then nosing die and base block are relatively reciprocably closed toward one another, as for example, by driving of the nosing die toward the base block to efiect driving of the thickened nose portion 25 of the shell 15 into the nosing cavity 39 whereby the shell is taper nosed as shown in FIG. 3. By the contraction thus effected, the tapered nose portion of the shell is provided with substantially increased wall thickness attaining maximum thickness at the nose tip of the shell. This affords adequate material for subsequent internal machining and threading to receive a fuse tip or plug or armor piercing point on the head. At the conclusion of the nosing operation, the dies are separated, the stripper plunger 29a ejecting the shell from the base 28, and the stripper plunger 4% acting, after the shell has been carried by the nosing die '37 away from the base 2% to strip and eject the shell from the nosing die.
During the nosing operation, not only is radially inward compression and contraction of the nose portion 25 of the shell effected, but a considerable axial compression force is applied in driving the nose portion of the shell into the nosing cavity 39. Since the major extent of the Wall 19 of the shell is comparatively quite thin, the axial compression force tends to cause buckling of the side wall. In the approximately first half of the nosing stroke of the nosing die assembly, while the nose portion 25 of the shell is moving into the larger gradually tapering portion of the nosing cavity 39, the axial compression force is reasonably moderate since resistance of the nose material of the shell to contraction is still moderate. However, maximum compression force is exerted in the last portion of the nosing stroke and it is at this time that the tendency toward buckling of the side wall 19 of the shell is greatest.
According to the present invention, the sidewall 19 is supported against buckling during the greatest compression strain thereon during nosing. To this end, the base block 28 and the nosing die 37 are provided with complementary cooperatively related, relatively axially movable alternating respective anti-buckling fingers 45 and 47 which become operative during the last portion of the nosing stroke of the die asseembly and by their symmetrical radial full external support of the side wall throughout the potential buckling zone as the nosing operation progresses to a conclusion prevent lateral or radial outward buckling of the shell. On inspection of PEG. 4 it will be observed that the anti-buckling fingers 45 and 47 have their major transverse extent radial relative to the shell so that they are strongly resistant to radial outward force exerted thereagainst by the shell Wall 19.
Additional reinforcement against radially outward displacement of the fingers 45 and 47 is afforded by a reinforcing annulus collar 48 which may, for convenience, be mounted about the fingers 47 of the nosing die and secured to the nosing die as best seen in FIGS. 1 and 3. Air p'ressure'relief through the reinforcing ring 48 is afforded through one or more exhaust ports 49 therethrough preferably adjacent to the roots of the fingers 47.
It will be understood that modifications and variations may be efifected Without departing from the scope of the novel concepts of the present invention.
I claim as my invention:
'1'. In a shell nosing apparatus, a base support for a shell, 21 nosing die relatively reciprocably disposed relative to the base support and having a nosing cavity therein, said cavity being adapted to nose a shell casing supported in said base support, and means on said base support and on said nosing die cooperable during nosing cooperation of said base support and said nosing die to supa port the shell against buckling, said means comprising a series of cooperating longitudinally extending supporting fingers disposed symmetrically for encompassing the Wall of a shell being nosed, with certain fingers of the series the shell against buckling, said means comprising a series of cooperating longitudinally extending supporting fingers disposed symmetrically for encompassing the wall of a carried by the'nose die and other fingers'of the series shell being nosed, with certain of the fingers comprising a set carried by the nosing die and other of the fingers comprising a set carried by the base support, and one of saidsets of fingers having a reinforcing annulus thereabout.
References Cited in the file of this patent UNITED STATES PATENTS 271,178 Wiesel Ian. 23, 1883 346,213 Morse July 27, 1886 501,547 Thomson July 18, 1893 977,639 Lachman Dec. 6, 1910 1,332,798 Brown Mar. 2, 1920 2,067,568 Grunthal Jan. 12, 1937 2,357,110 Heineman Aug. 29, 1944 2,404,304 Layton July 16, 1946 2,515,841 Stuart July 18, 1950 2,958,116 Lyon Nov. 1, 1960
US27714A 1953-12-09 1960-05-09 Shell nosing apparatus Expired - Lifetime US3036360A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US27714A US3036360A (en) 1953-12-09 1960-05-09 Shell nosing apparatus

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US397248A US2958115A (en) 1953-12-09 1953-12-09 Method for making bomb heads or the like
US27714A US3036360A (en) 1953-12-09 1960-05-09 Shell nosing apparatus

Publications (1)

Publication Number Publication Date
US3036360A true US3036360A (en) 1962-05-29

Family

ID=26702810

Family Applications (1)

Application Number Title Priority Date Filing Date
US27714A Expired - Lifetime US3036360A (en) 1953-12-09 1960-05-09 Shell nosing apparatus

Country Status (1)

Country Link
US (1) US3036360A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4419796A (en) * 1981-09-24 1983-12-13 Honeywell Inc. Method of making spin stabilized discarding sabot projectile

Citations (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US271178A (en) * 1883-01-23 Max wieser
US346213A (en) * 1886-07-27 moese
US501547A (en) * 1893-07-18 Shaping and spinning metals by electricity
US977639A (en) * 1910-01-29 1910-12-06 Welded Steel Wheel Company Die.
US1332798A (en) * 1918-05-18 1920-03-02 American Equipment Company Machine for automatically nosing in shells
US2067568A (en) * 1932-02-08 1937-01-12 Grunthal Moritz Die for automatically working mechanical forging machines for manufacturing of seamless hollow bodies
US2357110A (en) * 1941-09-15 1944-08-29 Smith Corp A O Method of making bombshells
US2404304A (en) * 1942-06-04 1946-07-16 Lansdowne Steel & Iron Company Nosing-in apparatus for shell forgings
US2515841A (en) * 1943-12-16 1950-07-18 Moe Brothers Mfg Company Tube closing apparatus
US2958116A (en) * 1954-06-16 1960-11-01 Lyon George Albert Method of and means for tapering shells

Patent Citations (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US271178A (en) * 1883-01-23 Max wieser
US346213A (en) * 1886-07-27 moese
US501547A (en) * 1893-07-18 Shaping and spinning metals by electricity
US977639A (en) * 1910-01-29 1910-12-06 Welded Steel Wheel Company Die.
US1332798A (en) * 1918-05-18 1920-03-02 American Equipment Company Machine for automatically nosing in shells
US2067568A (en) * 1932-02-08 1937-01-12 Grunthal Moritz Die for automatically working mechanical forging machines for manufacturing of seamless hollow bodies
US2357110A (en) * 1941-09-15 1944-08-29 Smith Corp A O Method of making bombshells
US2404304A (en) * 1942-06-04 1946-07-16 Lansdowne Steel & Iron Company Nosing-in apparatus for shell forgings
US2515841A (en) * 1943-12-16 1950-07-18 Moe Brothers Mfg Company Tube closing apparatus
US2958116A (en) * 1954-06-16 1960-11-01 Lyon George Albert Method of and means for tapering shells

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4419796A (en) * 1981-09-24 1983-12-13 Honeywell Inc. Method of making spin stabilized discarding sabot projectile

Similar Documents

Publication Publication Date Title
EP0000438B1 (en) Process for producing tubular articles
US3435653A (en) Forming method and apparatus
US2932889A (en) Pipe upsetting
US2668345A (en) Shell making process
US2980993A (en) Method of and apparatus for forming flanged casing bottom
US2739557A (en) Method and apparatus for deep drawing of metals
US3036360A (en) Shell nosing apparatus
US3177688A (en) Forging machine for the internal profiling of tubular workpieces, particularly of barrels for firearms
US3644973A (en) Method of making ball studs from metal rods
US2958115A (en) Method for making bomb heads or the like
US2991552A (en) Cold forging process
US2606516A (en) Apparatus for forming sheet metal material
CN208245721U (en) A kind of undershoot header structure with scalable material returning sleeve
US2159901A (en) Metalworking machine
US2701018A (en) Punching and extrusion unit
US3394572A (en) Method and apparatus for forming a curled edge on a tubular article
US1054669A (en) Process of making a combined bolt and grease-cup from sheet-metal blanks.
CN108380806A (en) A kind of undershoot header structure with scalable material returning sleeve
US3513681A (en) Means for performing an extrusion process in a cold forging press
US2961744A (en) Method of making bearing rings
US1467264A (en) of cincinnati
US2564193A (en) Apparatus for shaping the ends of can bodies
US1913492A (en) Method of wheel hub forging
US2812059A (en) Die shaping device
US3113540A (en) Single ram press