US681448A - Projectile. - Google Patents

Projectile. Download PDF

Info

Publication number
US681448A
US681448A US70927999A US1899709279A US681448A US 681448 A US681448 A US 681448A US 70927999 A US70927999 A US 70927999A US 1899709279 A US1899709279 A US 1899709279A US 681448 A US681448 A US 681448A
Authority
US
United States
Prior art keywords
projectile
band
shell
groove
gun
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
US70927999A
Inventor
Emil Gathmann
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.)
GATHMANN TORPEDO GUN Co
Original Assignee
GATHMANN TORPEDO GUN Co
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 GATHMANN TORPEDO GUN Co filed Critical GATHMANN TORPEDO GUN Co
Priority to US70927999A priority Critical patent/US681448A/en
Priority to US35387A priority patent/US678557A/en
Application granted granted Critical
Publication of US681448A publication Critical patent/US681448A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42BEXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B14/00Projectiles or missiles characterised by arrangements for guiding or sealing them inside barrels, or for lubricating or cleaning barrels
    • F42B14/02Driving bands; Rotating bands

Definitions

  • This 'invention relates to guns and projectiles therefor, and has for its object to provide a construction whereby the stripping of the compression-band from the projectile by reason of the centrifugal force generated by the whirling of the shell after it leaves the gun may be prevented; and to this end the invention consists in certain novel features, which I will now proceed to describe and will then particularly point out in the claims.
  • Figure 1 represents a longitudinal sectional View of a gun embodying myinvention, a projectile being shown therein in full lines in its initial position.
  • Fig. 2 is an enlarged detail sectional view through a portion of the gun and projectile at the compression-band of thelatter, the parts being shown in the same relative position as in Fig. 1 of the drawings, or, in other words, in theirinitial position.
  • Fig. 3 is a similar view illustrating the position of the parts after the projectile has advanced some distance into the gun.
  • Fig. 4 is asimilar View illustrating the parts in the position they assume when the projectile has entered the normal cylindrical or rifled portion of the gun and the compression-band has engaged
  • Fig. 5 is afdetail view, in longitudinal section, of the base of a shell, illustrating a modified form of connecof the structure shown'in Fig. 5.
  • Fig. 6 is a transverse sectional view
  • Fig. 7 is a view similar to Fig. 6, illustrating a modification of the structure therein shown; and Fig. Sis a similar view illustrating a further modification.
  • the projectile is' usually provided with a compressionband of copper or the like to engage the rifling 'of the gun and impart a rotary motion to the projectile, and this engagement of the band with the projectile is effected by providing the projectile with a circumferential goove having slightly undercut margins, the band being bent so as to permit it to be slipped into place and then flattened out so as to thrust its edges underneath the undercut margins of the groove, and thereby cause it to engage the projectile.
  • the powder-chamber may be of any approved construction, being, as usual, of greater diameter than the shell and being connected with the shell-chamber 12 by means of a short inclined shoulder 14. in the usual manner.
  • the shell-chamber 12 is of a gradually-decreasing diameter from rear to front, as shown in Fig. 1, and merging gradually into the rilled portion of the bore at its forward end, hobos, however, of greater diameter than the body of the shell at its forward end as well as at its rear end.
  • the projectile the body of which is indicated at 15, is provided near its base with a circumferentialgroove 16,havingits front and rear Walls undercut to a comparatively great extent, as will appear more particularly from an examination of Figs. 2, 3, andiof the drawings, and there are preferably formed in the vrbottom of this groove 1G one or more inclined annular grooves 17, as shownin said guros.
  • the compression-band, which is indicated at 18, is constructed o f copper or other like material and is preferably provided with aplurality of circumferential ribs or projections 19 on its exterior,these projections preferably increasing in height rearwardly, as clearly shown in Fig. 2 of the drawings.
  • This compression-band is smooth or without projec- ICO ti'ons on its inner face when applied to the projectile and' may be inserted in position in the manner shown in Fig. 2 by bendingit so as to permit it to pass the comparatively narrow mouth of the groove 16, as in the case of the ordinary compression-band.
  • the undercutting of the said groove 16 is, however, so great that when the compression-band is straightened out or flattened, as shown in Fig. 2, it'does not fully engage underneath the undercut walisof the groove.
  • yA projectile thus constructed when-employed in combination with a gun of the character described operates ⁇ in the following manner: Upon the explosion of the propelling charge the projectile moves forward through the ⁇ shell-chamber, and the tapering or decrease in diameter of the said chamber exercises a compressing action upon the copper band-1S, so as to gradually swage the same into position within the groove 16, as indicated in Figs. 3 and 4.
  • Fig. 1 Fig. 1
  • the shell is shown in thc position wherein the compression-band has engaged the riiiing of the gun, and it will be observed that the body of the band is now fully forced under the frontand rear walls of the groove in the projectile and completely fills the undercut portions thereof, while at the saine time the copper of which the band is composed has been forced into and fills the inclined grooves 17, so that the compression-band is firmly united to and permanently held in engagement with the body of the projectile.
  • This result is obtained by the very act of diseliargin-g the projectile from the gun, and the nature of the union is such that the band is firmly held in position around the projectile after the discharge thereof from the gun and will not be stripped or torn therefrom.
  • I claim- 1 A projectile having a circumferential groove with undercut front and rear walls and supplemental grooves with inclined walls formed in the base or inner face of said main groove, and a compression-band of comparatively soft metal seated within but not normally filling said main and supplemental grooves, said band being adapted to be pressed into engagement with said grooves IOO by the wall of a tapering shell-chamber when the gun is discharged, substantially as described.
  • ⁇ A projectile having a circumferential groove with undercut front and rear walls and annular inclined supplemental grooves formed in the base of the main groove, and a com pression-band of com paratively soft metal seated Within but not normally filling said main groove, said band being adapted to be pressed into engagement with said main or supplemental grooves by the wall of a tapering shell-chamber when the gu n is discharged, substantially as described.

Description

`with the riing thereof.
UNITED STATES V)MIL GATIIMANN, OF CHICAGO, ILLINOIS, ASSIGNOR TO Tllll GA'llllvlANN PATENT OFFICE.
TORIEDO GUN COMPANY, OF SAME PLACE.
PROJECTILE.
SPECIFICATION forming part of Letters Patent No..681,448, dated August 27, 1901. Application filed March 16, 1899. Serial No. 7091279. (No model.)
T @ZZ whom, it 17mg/ cm1/cern:
lle it known that I, EMIL GATHMANN, of Ohi- `cago, in the county of Cook and State of Illinois, have invented certain new and useful Improvements in Guns and Projectiles Therefor, of which the following is a specification.
This 'invention relates to guns and projectiles therefor, and has for its object to provide a construction whereby the stripping of the compression-band from the projectile by reason of the centrifugal force generated by the whirling of the shell after it leaves the gun may be prevented; and to this end the invention consists in certain novel features, which I will now proceed to describe and will then particularly point out in the claims.
In the accompanying drawings, Figure 1 represents a longitudinal sectional View of a gun embodying myinvention, a projectile being shown therein in full lines in its initial position. Fig. 2 is an enlarged detail sectional view through a portion of the gun and projectile at the compression-band of thelatter, the parts being shown in the same relative position as in Fig. 1 of the drawings, or, in other words, in theirinitial position. Fig. 3 is a similar view illustrating the position of the parts after the projectile has advanced some distance into the gun. Fig. 4 is asimilar View illustrating the parts in the position they assume when the projectile has entered the normal cylindrical or rifled portion of the gun and the compression-band has engaged Fig. 5 is afdetail view, in longitudinal section, of the base of a shell, illustrating a modified form of connecof the structure shown'in Fig. 5.
tion between the projectile and compressionband. Fig. 6 is a transverse sectional view Fig. 7 isa view similar to Fig. 6, illustrating a modification of the structure therein shown; and Fig. Sis a similar view illustrating a further modification.
Inordnance as now constructed the projectile is' usually provided with a compressionband of copper or the like to engage the rifling 'of the gun and impart a rotary motion to the projectile, and this engagement of the band with the projectile is effected by providing the projectile with a circumferential goove having slightly undercut margins, the band being bent so as to permit it to be slipped into place and then flattened out so as to thrust its edges underneath the undercut margins of the groove, and thereby cause it to engage the projectile. In practice it is found, particularly with high-explosive shells of large diameter, thatthis method of engaging the compression-band and projectile docs not hold the band in place with sufficient strength to resist the centrifugal force produced by the whirling of the shell after it leaves the muzzle of the gun, in consequence of which the band is frequently torn or stripped from its place. I obviate this objection by the construction shown in the accompanying drawings, in which-- 10 indicates the body of agunhaving atits rear end the usual powder or charge chamber 11 and in advance of this a shell-chamber 12,.lying intermediate between the powderchamber and the chase or rifled bore. 12 of the gun extending from the shell-chamber to the muzzle. The powder-chamber may be of any approved construction, being, as usual, of greater diameter than the shell and being connected with the shell-chamber 12 by means of a short inclined shoulder 14. in the usual manner. The shell-chamber 12 is of a gradually-decreasing diameter from rear to front, as shown in Fig. 1, and merging gradually into the rilled portion of the bore at its forward end, heilig, however, of greater diameter than the body of the shell at its forward end as well as at its rear end.
The projectile, the body of which is indicated at 15, is provided near its base with a circumferentialgroove 16,havingits front and rear Walls undercut to a comparatively great extent, as will appear more particularly from an examination of Figs. 2, 3, andiof the drawings, and there are preferably formed in the vrbottom of this groove 1G one or more inclined annular grooves 17, as shownin said guros. The compression-band, which is indicated at 18, is constructed o f copper or other like material and is preferably provided with aplurality of circumferential ribs or projections 19 on its exterior,these projections preferably increasing in height rearwardly, as clearly shown in Fig. 2 of the drawings. This compression-band is smooth or without projec- ICO ti'ons on its inner face when applied to the projectile and' may be inserted in position in the manner shown in Fig. 2 by bendingit so as to permit it to pass the comparatively narrow mouth of the groove 16, as in the case of the ordinary compression-band. The undercutting of the said groove 16 is, however, so great that when the compression-band is straightened out or flattened, as shown in Fig. 2, it'does not fully engage underneath the undercut walisof the groove. yA projectile thus constructed when-employed in combination with a gun of the character described operates` in the following manner: Upon the explosion of the propelling charge the projectile moves forward through the `shell-chamber, and the tapering or decrease in diameter of the said chamber exercises a compressing action upon the copper band-1S, so as to gradually swage the same into position within the groove 16, as indicated in Figs. 3 and 4. In Fig. 3 ofthe drawings the shell is shown in the condition in which it exists when the compression-band has passed partly through the shell-chamber, and it will be observed that the body of the band has not only been forced outward to a considerably greater extent underneath the un` Y dercut walls of the groove 1G, but that a portion of the body at the base or inner face thereof has also been forced intothe inclined grooves 17. In Fig. I of the drawings the shell is shown in thc position wherein the compression-band has engaged the riiiing of the gun, and it will be observed that the body of the band is now fully forced under the frontand rear walls of the groove in the projectile and completely fills the undercut portions thereof, while at the saine time the copper of which the band is composed has been forced into and fills the inclined grooves 17, so that the compression-band is firmly united to and permanently held in engagement with the body of the projectile. This result is obtained by the very act of diseliargin-g the projectile from the gun, and the nature of the union is such that the band is firmly held in position around the projectile after the discharge thereof from the gun and will not be stripped or torn therefrom.
'lhe invention is of course capable of embodiment in numerous modified forms, although the specific form which I have just described and which is shown in Figs. 1 to et of the drawings is that which I prefer. In Fig. 5 of the drawings, 4for instance, I have shown the projectile l5 as a shell having a breech-plug 2O and having the base portion of its body rabbeted and threaded to receive a clamping-ring 21, which has a beveled or undercut forward edge 22, which forms one h of the shoulders of the circumferential groove 16, which receives the compression-band. In
this construction the compression-band is placed in position within the groove before the ring 2l-is screwed into place. I have also shown in this construction the base of the groove 16 `as provided with supplemental grooves 23, extending longitudinally of the shell instead of circumferentially, as in the ycase of the grooves 17 shown in Figs. 2, 3, and 4. These grooves 23 are dovetailed in the construction shown in Fig. 6, and in order to facilitate the formation of these dovetailed grooves by the use of ordinary milling machinery or the like there is provided at thc the drawings I have shown grooves 25 which are rectangular in crosssection,while in Fig. S of the drawings IA have shown the bottom of the groove 16 as serrated or provided with grooves 26, having one inclined and one substantially radial face, the arrangement being such` of course that the radial face resists the tendency of the band to move around the body of the projectile. Other rnoditications in the details of construction may be made, and I do not wish to be understood as limiting myself to the precise construction hereinbefore set forth,and shown in the drawings.
I claim- 1..A projectile having a circumferential groove with undercut front and rear walls and supplemental grooves with inclined walls formed in the base or inner face of said main groove, and a compression-band of comparatively soft metal seated within but not normally filling said main and supplemental grooves, said band being adapted to be pressed into engagement with said grooves IOO by the wall of a tapering shell-chamber when the gun is discharged, substantially as described.
2. `A projectile having a circumferential groove with undercut front and rear walls and annular inclined supplemental grooves formed in the base of the main groove, and a com pression-band of com paratively soft metal seated Within but not normally filling said main groove, said band being adapted to be pressed into engagement with said main or supplemental grooves by the wall of a tapering shell-chamber when the gu n is discharged, substantially as described.
E M l L GAT H M AN N.
Witnesses: y
M. C. MAssIE, BERTHA L. DANA.
IIO
US70927999A 1899-03-16 1899-03-16 Projectile. Expired - Lifetime US681448A (en)

Priority Applications (2)

Application Number Priority Date Filing Date Title
US70927999A US681448A (en) 1899-03-16 1899-03-16 Projectile.
US35387A US678557A (en) 1899-03-16 1900-11-03 Gun.

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US70927999A US681448A (en) 1899-03-16 1899-03-16 Projectile.

Publications (1)

Publication Number Publication Date
US681448A true US681448A (en) 1901-08-27

Family

ID=2749991

Family Applications (1)

Application Number Title Priority Date Filing Date
US70927999A Expired - Lifetime US681448A (en) 1899-03-16 1899-03-16 Projectile.

Country Status (1)

Country Link
US (1) US681448A (en)

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2922368A (en) * 1953-10-22 1960-01-26 Lyon George Albert Projectile structure
US2996012A (en) * 1955-11-17 1961-08-15 Rex B Butler Rotating band and seat therefor
US3460478A (en) * 1964-10-24 1969-08-12 Rheinmetall Gmbh Projectile with sintered metal driving band
DE1678497B1 (en) * 1963-08-12 1970-05-21 Haut Rhin Manufacture Machines Projectile bodies, especially for small-caliber automatic weapons such as automatic firearms
US4754708A (en) * 1986-11-24 1988-07-05 Ford Aerospace & Communications Corp. Projectile driving band retention system
US5069139A (en) * 1987-10-05 1991-12-03 Denis Jean Pierre Projectile intended to be fired by a fire-arm

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2922368A (en) * 1953-10-22 1960-01-26 Lyon George Albert Projectile structure
US2996012A (en) * 1955-11-17 1961-08-15 Rex B Butler Rotating band and seat therefor
DE1678497B1 (en) * 1963-08-12 1970-05-21 Haut Rhin Manufacture Machines Projectile bodies, especially for small-caliber automatic weapons such as automatic firearms
US3460478A (en) * 1964-10-24 1969-08-12 Rheinmetall Gmbh Projectile with sintered metal driving band
US4754708A (en) * 1986-11-24 1988-07-05 Ford Aerospace & Communications Corp. Projectile driving band retention system
US5069139A (en) * 1987-10-05 1991-12-03 Denis Jean Pierre Projectile intended to be fired by a fire-arm

Similar Documents

Publication Publication Date Title
US1187464A (en) Cartridge-case.
US1355422A (en) Rifle-barrel
US3769912A (en) Spin-stabilized projectiles
US681448A (en) Projectile.
US590428A (en) Thomas g
US1355421A (en) Rifle-barrel
US1072880A (en) Bullet.
US34493A (en) Improvement in projectiles for rifled ordnance
US847149A (en) Bullet.
US1062604A (en) Gun-operating cartridge.
US703839A (en) Cartridge.
US1455354A (en) Projectile
US703840A (en) Gun-cartridge.
US1122738A (en) Target-bullet.
US122014A (en) Improvement in projectiles
US2776621A (en) Projectile
US407890A (en) Lubricating projectile
US132903A (en) Improvement
US998712A (en) Projectile.
US165255A (en) Improvement in projectiles for ordnance
US484012A (en) haskell
US91864A (en) Improvement in ordnance
US2090533A (en) Projectile
US443101A (en) maxim
US214843A (en) Improvement in projectiles for rifled guns