US2345619A - Projectile - Google Patents

Projectile Download PDF

Info

Publication number
US2345619A
US2345619A US400042A US40004241A US2345619A US 2345619 A US2345619 A US 2345619A US 400042 A US400042 A US 400042A US 40004241 A US40004241 A US 40004241A US 2345619 A US2345619 A US 2345619A
Authority
US
United States
Prior art keywords
projectile
jacket
core
nose
filler
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
US400042A
Inventor
Wiley T 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.)
Individual
Original Assignee
Individual
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 Individual filed Critical Individual
Priority to US400042A priority Critical patent/US2345619A/en
Application granted granted Critical
Publication of US2345619A publication Critical patent/US2345619A/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
    • F42B12/00Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material
    • F42B12/02Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect
    • F42B12/20Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect of high-explosive type
    • F42B12/201Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect of high-explosive type characterised by target class
    • F42B12/204Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect of high-explosive type characterised by target class for attacking structures, e.g. specific buildings or fortifications, ships or vehicles
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42BEXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B12/00Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material
    • F42B12/02Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect
    • F42B12/36Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect for dispensing materials; for producing chemical or physical reaction; for signalling ; for transmitting information
    • F42B12/44Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect for dispensing materials; for producing chemical or physical reaction; for signalling ; for transmitting information of incendiary type

Definitions

  • This invention relates to explosive or incendiary projectiles.
  • Figure 1 is a longitudinal cross section of a projectile embodying my invention.
  • Figure 2 is a longitudinal cross section of a modified form of my invention.
  • Figure 1 shows a projectile comprising a hollow core I which may conveniently be formed of steel tubing.
  • An end 2 of the core is reduced in diameter and provided with external screw threads.
  • a base filler 3 of lead or other suitable material is provided at the base of the core I and with the core is enclosed in a jacket 4 of gliding metal or the like.
  • the brim of the jacket is crimped or otherwise turned in to form a flange 5 opposing the shoulder 6 formed by the reduced portion of the core.
  • An ogival nose cap 7 formed of a suitable plastic material or of metal is provided with internal screw threads adapted to engage the threaded portion 2 of the hollow core and with an internal bore 8 in alignment with the interior of the hollow core when the nose cap is engaging the threads.
  • This type of construction has several notable advantages in that the main charge may be separately loaded without the presence of a dangerously sensitive priming charge.
  • the nose caps may be specially loaded with any desired type of primer charge. Separate loading in this manner insures that any ing the primers will not be communicated to the main charges with possible loss of life.
  • the nose caps may be assembled to the body portions at any desired time after loading.
  • the flange 5 formed by the brim of the jacket is secured between the rear face of the nose cap and the front face of the core insuring that rotating forces applied to the jacket will be communicated to the core.
  • the nose cap is made of such a length as to extend back to the forward limit of the portion of the projectile which is engaged by the rifiing of the gun securing maximum economy of jacket material.
  • the core I is internally threaded at its nose portion.
  • a base filler 3 is provided as in Figure 1 and the jacket 4 is slipped over the filler and core body and has its brim formed into an inwardly extending flange 5 opposing the front end of the core.
  • An ogival nose cap 9 formed of a suitable plastic material or of metal is provided with a rear portion of reduced diameter It having external threads adapted to cooperate with those formed in the core body.
  • a chamber I I is formed in the nose cap which may be loaded with a suitable primer. This modification may be loaded in a similar manner to the modification shown in Figure 1 and in practice will have the same advantages.
  • plastics of the synthetic resin type are suitable for use as projectile parts presents several advantages not heretofore achieved in practice. For some applications it may be necessary to use fillers of vegetable or mineral fiber to add strength to the plastic compound. It has been discovered that a projectile nose may be formed from plastics which will have ample strength to resist the forces of setback on firing and of centrifugal action during flight. Priming materials are notably sensitive to heat, shock, and vibration all of which are readily transmitted through metallic nose caps. Plastics of suitable strength have been found to be excellent insulators for protecting the priming charge from the heat and shocks incident to firing.
  • plastics enable the bulk of the Weight of the projectile to be concentrated about the explosive charge for more efifective fragmentation without exerting a deleterious effect upon the form factor or stability of the projectile. Further, the use of plastics permits of die-forming with consequent improvements in the cost of production and uniaccidental explosion which might occur in loadformity of the finished product.
  • a projectile comprising a cup-shaped jacket, a filler plate in the base of said jacket, a tubular body portion in said jacket, said body portion having a section of reduced diameter near its front end forming a forwardly facing shoulder, an inwardly extending flange formed in the front end of said jacket in opposition to said shoulder to retain the core in said jacket in contact with.
  • said base filler and a chambered ogival nose cap threadably engaging the portion of reduced di ameter and having a shoulder overlying the said portion in said jacket having its rear end in contact with said filler and having its forward end internally threaded, the front end of said jacket being formed into an inwardly extending flange opposing the forward face of said body portion, and a chambered, ogival nose cap threadably engaging the body portion and having a rearwardly facing shoulder overlying the said flange.
  • a projectile comprising a cup-shaped jacket, a filler in the base of said jacket, a tubular body portion in said jacket having its rear end in contact with said filler, the front end of said jacket being formed into an inwardly extending flange opposing the forward face of said body portion, and a chambered ogival nose cap engaging the body portion and having a rearwardly facing shoulder overlying the said flange.

Description

April 4, 1944. w, MOORE 2,345,619 v PROJECTILE Filed June 27, 1941 Wiiey T MUEI1"E Patented Apr. 4, 1944 PROJECTILE Wiley T. Moore, United States Army Laverne, Okla.
Application June 27, 1941, Serial No. 400,042
(Granted under the act of March 3, 1 883, as
amended April 30, 1928; 370 0. G. 757) 3 Claims.
The invention described herein may be manufactured and used by or for the Government for governmental purposes, without the payment to me of any royalty thereon.
This invention relates to explosive or incendiary projectiles.
In the explosive and incendiary projectiles previously known and used assembly and loading was often difiicult and dangerous owing to the necessity of performing certain assembly operations with sensitive priming charges in place.
It is an object of this invention to simplify the manufacture and assembly of explosive and incendiary projectiles.
It is a further object of this invention to provide a form of projectile which may be safely loaded and handled without reducing the sensitivity of the charge therein.
It is a further object of this invention to provide a projectile having an arrangement of parts whereby the nose cap may be formed of plastics.
The specific nature of the invention as well as other objects and advantages thereof will clearly appear from a description of a preferred embodiment as shown in the accompanying drawing in which:
Figure 1 is a longitudinal cross section of a projectile embodying my invention.
Figure 2 is a longitudinal cross section of a modified form of my invention.
Referring to the drawing by characters of reference, Figure 1 shows a projectile comprising a hollow core I which may conveniently be formed of steel tubing. An end 2 of the core is reduced in diameter and provided with external screw threads. A base filler 3 of lead or other suitable material is provided at the base of the core I and with the core is enclosed in a jacket 4 of gliding metal or the like. The brim of the jacket is crimped or otherwise turned in to form a flange 5 opposing the shoulder 6 formed by the reduced portion of the core. An ogival nose cap 7 formed of a suitable plastic material or of metal is provided with internal screw threads adapted to engage the threaded portion 2 of the hollow core and with an internal bore 8 in alignment with the interior of the hollow core when the nose cap is engaging the threads. This type of construction has several notable advantages in that the main charge may be separately loaded without the presence of a dangerously sensitive priming charge. Similarly the nose caps may be specially loaded with any desired type of primer charge. Separate loading in this manner insures that any ing the primers will not be communicated to the main charges with possible loss of life. The nose caps may be assembled to the body portions at any desired time after loading. When the projectile is completely assembled the flange 5 formed by the brim of the jacket is secured between the rear face of the nose cap and the front face of the core insuring that rotating forces applied to the jacket will be communicated to the core. Preferably the nose cap is made of such a length as to extend back to the forward limit of the portion of the projectile which is engaged by the rifiing of the gun securing maximum economy of jacket material.
In the modification of my invention shown in Figure 2 the core I is internally threaded at its nose portion. A base filler 3 is provided as in Figure 1 and the jacket 4 is slipped over the filler and core body and has its brim formed into an inwardly extending flange 5 opposing the front end of the core. An ogival nose cap 9 formed of a suitable plastic material or of metal is provided with a rear portion of reduced diameter It having external threads adapted to cooperate with those formed in the core body. A chamber I I is formed in the nose cap which may be loaded with a suitable primer. This modification may be loaded in a similar manner to the modification shown in Figure 1 and in practice will have the same advantages.
The discovery that plastics of the synthetic resin type are suitable for use as projectile parts presents several advantages not heretofore achieved in practice. For some applications it may be necessary to use fillers of vegetable or mineral fiber to add strength to the plastic compound. It has been discovered that a projectile nose may be formed from plastics which will have ample strength to resist the forces of setback on firing and of centrifugal action during flight. Priming materials are notably sensitive to heat, shock, and vibration all of which are readily transmitted through metallic nose caps. Plastics of suitable strength have been found to be excellent insulators for protecting the priming charge from the heat and shocks incident to firing. The lower specific gravity of plastics enables the bulk of the Weight of the projectile to be concentrated about the explosive charge for more efifective fragmentation without exerting a deleterious effect upon the form factor or stability of the projectile. Further, the use of plastics permits of die-forming with consequent improvements in the cost of production and uniaccidental explosion which might occur in loadformity of the finished product.
I claim:
-1. A projectile comprising a cup-shaped jacket, a filler plate in the base of said jacket, a tubular body portion in said jacket, said body portion having a section of reduced diameter near its front end forming a forwardly facing shoulder, an inwardly extending flange formed in the front end of said jacket in opposition to said shoulder to retain the core in said jacket in contact with.
said base filler, and a chambered ogival nose cap threadably engaging the portion of reduced di ameter and having a shoulder overlying the said portion in said jacket having its rear end in contact with said filler and having its forward end internally threaded, the front end of said jacket being formed into an inwardly extending flange opposing the forward face of said body portion, and a chambered, ogival nose cap threadably engaging the body portion and having a rearwardly facing shoulder overlying the said flange.
3. A projectile comprising a cup-shaped jacket, a filler in the base of said jacket, a tubular body portion in said jacket having its rear end in contact with said filler, the front end of said jacket being formed into an inwardly extending flange opposing the forward face of said body portion, and a chambered ogival nose cap engaging the body portion and having a rearwardly facing shoulder overlying the said flange.
WILEY T. MOORE.
US400042A 1941-06-27 1941-06-27 Projectile Expired - Lifetime US2345619A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US400042A US2345619A (en) 1941-06-27 1941-06-27 Projectile

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US400042A US2345619A (en) 1941-06-27 1941-06-27 Projectile

Publications (1)

Publication Number Publication Date
US2345619A true US2345619A (en) 1944-04-04

Family

ID=23581990

Family Applications (1)

Application Number Title Priority Date Filing Date
US400042A Expired - Lifetime US2345619A (en) 1941-06-27 1941-06-27 Projectile

Country Status (1)

Country Link
US (1) US2345619A (en)

Cited By (19)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2425418A (en) * 1942-04-18 1947-08-12 Remington Arms Co Inc Ammunition
US2454801A (en) * 1945-04-23 1948-11-30 Harold H Himmer Rotating band
US2938460A (en) * 1956-09-12 1960-05-31 Energa Finned projectile
US2962967A (en) * 1943-12-21 1960-12-06 Harold W Bixby Fuze
US3142256A (en) * 1959-04-03 1964-07-28 Bernhard V Mack Jacketed-cast bullet
US3170405A (en) * 1962-03-17 1965-02-23 Karlsruhe Augsburg Iweka Disintegrating training ammunition for firearms
US3208386A (en) * 1963-12-04 1965-09-28 Ottow W Schneider Strip bullet
US3209650A (en) * 1963-04-30 1965-10-05 Thomas A Andrew Gun perforator and explosive projectile therefor
US3247795A (en) * 1964-04-01 1966-04-26 Abela Michael Frank Spinning projectile for smooth bore guns
US3282216A (en) * 1962-01-30 1966-11-01 Clifford T Calfee Nose cone and tail structures for an air vehicle
US3291048A (en) * 1965-02-24 1966-12-13 Nico Pyrotechnik Practice projectile for sub-calibre barrels
US5728968A (en) * 1989-08-24 1998-03-17 Primex Technologies, Inc. Armor penetrating projectile
US5852255A (en) * 1997-06-30 1998-12-22 Federal Hoffman, Inc. Non-toxic frangible bullet core
US5894645A (en) * 1997-08-01 1999-04-20 Federal Cartridge Company Method of forming a non-toxic frangible bullet core
US20040055501A1 (en) * 2002-09-20 2004-03-25 Hunn David L. Penetrator and method for using same
US20040055502A1 (en) * 2002-09-20 2004-03-25 Lockheed Martin Corporation Penetrator and method for using same
USD813974S1 (en) 2015-11-06 2018-03-27 Vista Outdoor Operations Llc Cartridge with an enhanced ball round
USD848569S1 (en) 2018-01-20 2019-05-14 Vista Outdoor Operations Llc Rifle cartridge
US10551154B2 (en) 2017-01-20 2020-02-04 Vista Outdoor Operations Llc Rifle cartridge with improved bullet upset and separation

Cited By (22)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2425418A (en) * 1942-04-18 1947-08-12 Remington Arms Co Inc Ammunition
US2962967A (en) * 1943-12-21 1960-12-06 Harold W Bixby Fuze
US2454801A (en) * 1945-04-23 1948-11-30 Harold H Himmer Rotating band
US2938460A (en) * 1956-09-12 1960-05-31 Energa Finned projectile
US3142256A (en) * 1959-04-03 1964-07-28 Bernhard V Mack Jacketed-cast bullet
US3282216A (en) * 1962-01-30 1966-11-01 Clifford T Calfee Nose cone and tail structures for an air vehicle
US3170405A (en) * 1962-03-17 1965-02-23 Karlsruhe Augsburg Iweka Disintegrating training ammunition for firearms
US3209650A (en) * 1963-04-30 1965-10-05 Thomas A Andrew Gun perforator and explosive projectile therefor
US3208386A (en) * 1963-12-04 1965-09-28 Ottow W Schneider Strip bullet
US3247795A (en) * 1964-04-01 1966-04-26 Abela Michael Frank Spinning projectile for smooth bore guns
US3291048A (en) * 1965-02-24 1966-12-13 Nico Pyrotechnik Practice projectile for sub-calibre barrels
US5728968A (en) * 1989-08-24 1998-03-17 Primex Technologies, Inc. Armor penetrating projectile
US5852255A (en) * 1997-06-30 1998-12-22 Federal Hoffman, Inc. Non-toxic frangible bullet core
US5894645A (en) * 1997-08-01 1999-04-20 Federal Cartridge Company Method of forming a non-toxic frangible bullet core
US20040055501A1 (en) * 2002-09-20 2004-03-25 Hunn David L. Penetrator and method for using same
US20040055502A1 (en) * 2002-09-20 2004-03-25 Lockheed Martin Corporation Penetrator and method for using same
US6843179B2 (en) 2002-09-20 2005-01-18 Lockheed Martin Corporation Penetrator and method for using same
USD813974S1 (en) 2015-11-06 2018-03-27 Vista Outdoor Operations Llc Cartridge with an enhanced ball round
USD884821S1 (en) 2015-11-06 2020-05-19 Vista Outdoor Operations Llc Enhanced ball round
US10551154B2 (en) 2017-01-20 2020-02-04 Vista Outdoor Operations Llc Rifle cartridge with improved bullet upset and separation
US11280595B2 (en) 2017-01-20 2022-03-22 Vista Outdoor Operations Llc Rifle cartridge with improved bullet upset and separation
USD848569S1 (en) 2018-01-20 2019-05-14 Vista Outdoor Operations Llc Rifle cartridge

Similar Documents

Publication Publication Date Title
US2345619A (en) Projectile
US3482516A (en) Caseless cartridges having the projectile housed in the propellant charge
US3507221A (en) Armor piercing,sabot shells
US2764092A (en) Impact fuze for projectiles
US4096804A (en) Plastic/mischmetal incendiary projectile
US4004516A (en) Fuze
US2426997A (en) Projectile
US2083665A (en) Ammunition and ordnance device
US3283720A (en) Molded plastic shotshell
US5148750A (en) Unitary projectile
FR2343987A1 (en) Tubular primer for artillery ammunition propellant - has axial bore and side vents through combustible ensuring uniform ignition
US2401380A (en) Projectile cap
US3212440A (en) Molded caseless small arms ammunition
US3216356A (en) Projectile
US2996007A (en) Explosive train
US2398287A (en) Incendiary bullet
GB1063965A (en) Improvements in or relating to propellent cartridges for projectiles
US2703531A (en) Fuze for projectiles
US2269316A (en) Ammunition for small arms
US2364643A (en) Explosive projectile
US2992612A (en) Projectile
US2459175A (en) Explosive bullet
US3710716A (en) Ram pressure standoff extension and safe/arm mechanism for self-arming munitions
US2441388A (en) Projectile
US2475632A (en) Bullet