US229499A - Explosive shell - Google Patents

Explosive shell Download PDF

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Publication number
US229499A
US229499A US229499DA US229499A US 229499 A US229499 A US 229499A US 229499D A US229499D A US 229499DA US 229499 A US229499 A US 229499A
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Prior art keywords
shell
breech
explosive shell
gun
caudal
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Expired - Lifetime
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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42BEXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B10/00Means for influencing, e.g. improving, the aerodynamic properties of projectiles or missiles; Arrangements on projectiles or missiles for stabilising, steering, range-reducing, range-increasing or fall-retarding
    • F42B10/32Range-reducing or range-increasing arrangements; Fall-retarding means
    • F42B10/38Range-increasing arrangements
    • F42B10/42Streamlined projectiles
    • F42B10/44Boat-tails specially adapted for drag reduction

Definitions

  • A represents the body ot' theshell, made in cylindrical form, of the bestlaminated steel or lron.
  • B is the breech or breech-pin, ttting the size of the shell, with heavy screw-threads to prevent explosion in the rear, and in the center ofthe breech is screwed or otherwise fastened a metallic tube, C, for incasing the fuse.
  • a percussion-cap, a is placed o'n the rear end ofthe tubeG, and a iianged cap, D, covers the same, as shown.
  • lln front of the breech B is the powder-chamber E, and in front of. this again a chamber for thcinissiles l?,I which latter should accordv in size with the caliber ofthe gun and the pur vposes for which they are intended.
  • the cap or point G In the front end of the shell is inserted the cap or point G, made in the usual form for elongated shells, and having a neck which lits ,the muzzle of the shell with small screwthreads.
  • a chamber for containing the caudal appendage which consists of two or more telescopic tubular sections, I I, held in the shell by means of an annular ring, d, fastcnedon the shoulder -metal or material. 'to close the rear end mog the shell.
  • I I telescopic tubular sections
  • a sabot, H is then fitted holes or air-passages b, through which theair enters as soon as the projectile leaves themuzzle of the gun, and, acting a ainst thecircumferential flange of the cap ,removes the same from the end of the tube G. It also throws out the sabot H and causes the telescopic caudal appendage to be extended, whi ch, acting as a feather to an arrow, prevents the -shell from turning in 'the air, or, in other words, keeps the point of the shell directly in -frou t.
  • the point G is hollowed out, as shown, formipgwrallambenj, which is to be filled with bucks-hot, adding largely' to the destructive qualities of theprojectile.
  • caudal appendage may be dispensed with and a wooden plugdefining, with a center hole to accommodate the fuse-plug.

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  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Toys (AREA)

Description

fGj.W.TURNER.V Explosive Shell.
`"Patented June 249, 1880.
l UITED STATES PATENT OFFICE.
GEORGE W. TURNER, OF ROONEVILLE, MISSISSIPPI.
ExPL'oslvE SHELL.
SPECIFICATION forming part of Letters Patent ineens, dma June" as, 1880;
Application tiled January 20, 188i).
and it consists in the combination of the bodyf|` of the shell',having'inclined air-inlets, and ai telescopic`tubearranged wit-hin the rear end ofthe shell, to be extended as a caudal append age by the force of the air after the shell leaves the mouth ot' the gun, as will be hereinafter more fully set forth.
In the drawings. Figurelrisa longitudinal Y 'section of my shell with the caudal appendage closed. Fig. 2 is` a similar view, showing the caudal appendage extended. Figs. 3 and 4. are detailed views.
A represents the body ot' theshell, made in cylindrical form, of the bestlaminated steel or lron.
B is the breech or breech-pin, ttting the size of the shell, with heavy screw-threads to prevent explosion in the rear, and in the center ofthe breech is screwed or otherwise fastened a metallic tube, C, for incasing the fuse. A percussion-cap, a, is placed o'n the rear end ofthe tubeG, anda iianged cap, D, covers the same, as shown.
lln front of the breech B is the powder-chamber E, and in front of. this again a chamber for thcinissiles l?,I which latter should accordv in size with the caliber ofthe gun and the pur vposes for which they are intended.
In the front end of the shell is inserted the cap or point G, made in the usual form for elongated shells, and having a neck which lits ,the muzzle of the shell with small screwthreads.
In the rear of the breech B is formed a chamber for containing the caudal appendage, which consists of two or more telescopic tubular sections, I I, held in the shell by means of an annular ring, d, fastcnedon the shoulder -metal or material. 'to close the rear end mog the shell. Directly in'rear of the breech B are inclined herein set forth.
e in the extreme rear end'of the shell. tubes or tubular sections are to be made of galvanized iron, zinc, or other non-corrosive A sabot, H, is then fitted holes or air-passages b, through which theair enters as soon as the projectile leaves themuzzle of the gun, and, acting a ainst thecircumferential flange of the cap ,removes the same from the end of the tube G. It also throws out the sabot H and causes the telescopic caudal appendage to be extended, whi ch, acting as a feather to an arrow, prevents the -shell from turning in 'the air, or, in other words, keeps the point of the shell directly in -frou t.
The point G is hollowed out, as shown, formipgwrallambenj, which is to be filled with bucks-hot, adding largely' to the destructive qualities of theprojectile.
For ride-gunsahe caudal appendage may be dispensed with and a wooden plug putin, with a center hole to accommodate the fuse-plug.
l lAt the rear end ot' the shell are attached two sheet-metal cups, L L, each of which is struck up ot a single piece and has its edges notched. The two cups are placed together, 'so as to have the metal between the notches overlapping. These portions of metal or teeth will spread when the gun is tired and take into the riding, so as to give the rotary or twisting motion to the shell.
These Having thus fully described my invention, l
vwhat ,I claim as new, and desire to secure by Letters Patent, is
ln an elongated shell, the combination of the body A, having inclined air-inlets b, and
In'testimonythat I claim` the foregoing IV have hereunto set .my hand this `16th day ot' January, 1880.
, G. W. TURNER. Witnesses:
` H; AUBEEYTOULMIN,
H. J. ENNIs.
gun, substantially as
US229499D Explosive shell Expired - Lifetime US229499A (en)

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Cited By (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2426239A (en) * 1942-12-28 1947-08-26 Henry M Renner Rocket shell
US3412962A (en) * 1967-04-10 1968-11-26 Claud R. Killian Retractable air drag reducing aircraft attachment
US4674706A (en) * 1986-02-21 1987-06-23 Hall Robert C Projectile with an extendable boattail
US4882996A (en) * 1987-10-30 1989-11-28 Diehl Gmbh & Co. Explosive projectile assembly with a projectile body
US6657174B1 (en) * 1999-11-10 2003-12-02 Bofors Defence Ab Method and design for increasing the firing range of artillery shells
US20050173588A1 (en) * 2002-11-08 2005-08-11 Giat Industries Method of correcting the trajectory of a spin-stabilised projectile and projectile implementing one such method
US20050224631A1 (en) * 2004-03-05 2005-10-13 The Boeing Company Mortar shell ring tail and associated method
US20070006768A1 (en) * 2005-07-06 2007-01-11 Rafael-Armament Development Authority Ltd. Mushroom warhead
US20110024549A1 (en) * 2009-07-31 2011-02-03 Raytheon Company, General Dynamics Ordnance and Tactical Systems (OTS) Deployable fairing and method for reducing aerodynamic drag on a gun-launched artillery shell
US20230221101A1 (en) * 2022-01-11 2023-07-13 Raytheon Company Effector having morphing airframe and method

Cited By (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2426239A (en) * 1942-12-28 1947-08-26 Henry M Renner Rocket shell
US3412962A (en) * 1967-04-10 1968-11-26 Claud R. Killian Retractable air drag reducing aircraft attachment
US4674706A (en) * 1986-02-21 1987-06-23 Hall Robert C Projectile with an extendable boattail
US4882996A (en) * 1987-10-30 1989-11-28 Diehl Gmbh & Co. Explosive projectile assembly with a projectile body
US6657174B1 (en) * 1999-11-10 2003-12-02 Bofors Defence Ab Method and design for increasing the firing range of artillery shells
US20050173588A1 (en) * 2002-11-08 2005-08-11 Giat Industries Method of correcting the trajectory of a spin-stabilised projectile and projectile implementing one such method
US20050224631A1 (en) * 2004-03-05 2005-10-13 The Boeing Company Mortar shell ring tail and associated method
US7262394B2 (en) * 2004-03-05 2007-08-28 The Boeing Company Mortar shell ring tail and associated method
US20070006768A1 (en) * 2005-07-06 2007-01-11 Rafael-Armament Development Authority Ltd. Mushroom warhead
US20110024549A1 (en) * 2009-07-31 2011-02-03 Raytheon Company, General Dynamics Ordnance and Tactical Systems (OTS) Deployable fairing and method for reducing aerodynamic drag on a gun-launched artillery shell
US8312813B2 (en) * 2009-07-31 2012-11-20 Raytheon Company Deployable fairing and method for reducing aerodynamic drag on a gun-launched artillery shell
US20230221101A1 (en) * 2022-01-11 2023-07-13 Raytheon Company Effector having morphing airframe and method
US11796291B2 (en) * 2022-01-11 2023-10-24 Raytheon Company Effector having morphing airframe and method

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