US2410435A - Cartridge for guns - Google Patents

Cartridge for guns Download PDF

Info

Publication number
US2410435A
US2410435A US445957A US44595742A US2410435A US 2410435 A US2410435 A US 2410435A US 445957 A US445957 A US 445957A US 44595742 A US44595742 A US 44595742A US 2410435 A US2410435 A US 2410435A
Authority
US
United States
Prior art keywords
projectile
cartridge
shank
propulsion surface
case
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
US445957A
Inventor
Jr John O Evans
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 US445957A priority Critical patent/US2410435A/en
Application granted granted Critical
Publication of US2410435A publication Critical patent/US2410435A/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
    • F42B5/00Cartridge ammunition, e.g. separately-loaded propellant charges
    • F42B5/02Cartridges, i.e. cases with charge and missile
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42BEXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B5/00Cartridge ammunition, e.g. separately-loaded propellant charges
    • F42B5/02Cartridges, i.e. cases with charge and missile
    • F42B5/16Cartridges, i.e. cases with charge and missile characterised by composition or physical dimensions or form of propellant charge, with or without projectile, or powder
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10STECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10S102/00Ammunition and explosives
    • Y10S102/70Combustilbe cartridge

Definitions

  • the invention described herein may be manufactured and used by or for tlieGovernment for governmental purposes, without the payment to invention relates to ordnance. Inone' of its aspects it relates to" a 'cartridge, particularly to a; small-arms cartridge; In another of its aspects it relates to a projectile for use in a A special gun.
  • Another ob ect of the invention is to provide asimple cartridge embodying the principles of the invention which is adapted for use in conventional firearms.
  • Another object of the invention is to provide a projectile and gun combination employing separate loading ammunition and embodying the aforesaid principles.
  • Another object of the invention is to provide a separate loading projectile in accordance with the invention.
  • Fig. 1 is a'fragmentary View, partly in section, of a cartridge in accordance with the invention positioned in the chamber of a rifle, and
  • Fig. 2 is a fragmentary View, partly in section, of a gun and projectile embodying the invention.
  • the invention involves in combination with an ordnance piece including a gun tube and a powder chamber receiving a propelling charge, a projectile seated in said ordnance piece, said projectile having a small first propulsion surface initially exposed to pressure generated by said charge and a second propulsion surface subsequently exposed to said pressure.
  • the cartridge embodiment of the invention includes a case providin a powder chamber receiving a propelling charge and having a neck portion providing a relatively small orifice and a projectile seated therein, said projectile having amended April 30, 1928; 370 O. G. 757) a first propulsion surface initially exposed' to pressure generated'by said charge and a second propulsion surface subsequently exposed ,to-said pressure.
  • Fig. 1 which shows' a cartridge in accordancewith the invention resting within the chamber of a riflei 4', 1 indicates a projectile having a head2 and a shank 3,
  • the cartridge case 5, and also the exposed head 2 of the projectile have conventional outside dimensions so that the cartridge is of proper size for conventional use.
  • the neck 6 of the case is much thicker than the neck of the conventional cartridge, thus providing a relatively small cylindrical orifice 1 in which the cylindrical shank of the projectile is seated with a sliding gas-tight fit.
  • the shank may have a slight forward taper, i.
  • the case may also be thickened at the shoulder 8 for reinforcement against rupture at this point.
  • the projectile is provided with two separate and distinct propulsion surfaces against which the propelling gases generated by the propelling charge act to accelerate the projectile.
  • the primary, or first propulsion surface is the base 9 of the shank and the secondary propulsion surface is the rearwardly facing area I! at the base of the projectiles head.
  • gases are rapidly generated by the propellant ll. These gases initially drive the projectile forward by action only upon the relatively small propulsion surface 9.
  • the acceleration takes place relatively slowly due to the small area upon which the gases are eifective.
  • the base 9 of the shank clears the forward end of the orifice 1 thereby giving the gases within the cartridge case egress to the bore of the rifle where they are free to act, not only upon the primary propulsion surface 9, but also, in addition, upon the secondary propulsion surface lB.
  • the accelerating force is thus considerably multiplied and the projectile is rapidly accelerated to the desired velocity.
  • the projectile la is provided with a. head 2a, and a shank 3a.
  • the guntube 4a provides the powder chamber to.
  • a collar 6a is provided for the projectile and is analogous to the thickened neck portion 6 of the cartridge case of Fig. 1.
  • a gas-tight sliding joint is provided between the orifice 1a of the collar and the shank of the projectile.
  • the collar and projectile preferably are loaded into the gun as a unit.
  • a gastight jointitla is p'rovided between the collar and the wallsof the powder chamber.
  • the primary propulsion surface is the base 9a of the shank and the secondary propulsion surface is the rearwardly exposed area Ilia at the base of the head.
  • the powder charge Ila is separately loaded into the chamber.
  • the action of the propelling gases on the projectile in the modification of Fig. 2 is similar to the accelerating action as described in connection with Fig. 1, the propelling gases acting first on the base of the shank and subsequently additionally on the rearwardly facing base of the head.
  • the relative size of shank and head of the projectile are not critical and may be varied within desired limits.
  • the length of the shank may bevaried to give a longer or shorter delay to the full accelerating action of the propelling gases, and the relative areas of the primary and secondary propulsion surfaces may be varied, as the case requires, to regulate the initial acceleration.
  • the area of the primary propulsion surface will be distinctly smaller than the area of the total propulsion surface, being preferably less than three quarters thereof.
  • propulsion surface is intended to means a surface of the projectile upon which propelling gases are eifective for acceleration of the projectile.
  • the area of such a surface will be considered to be the rectilinear projection of said area upon a plane perpendicular to the major axis of the projectile.
  • a cartridge comprising an elongated case providing a powder chamber receiving a propelling charge and having a neck portion at one end, said neck portion having thick walls providing a substantially cylindrical orifice, a projectile having a forwardly tapered shank portion extending inwardly through the said orifice of said case, making a sliding gas-tight joint with the inner surface of said orifice and providing a primary propulsion surface at the end of said shank, said projectile having a head portion providing a sec,- ondary propulsion surface, the outside diameter of the head of said projectile being not greater than the outside diameter of the neck portion of said case.

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)

Description

Nov. 5, 1946. J. o. EVANS, JR 0 3 CARTRIDGE FOR GUNS Filed June 5, 1942 awe/W600 John ELEvans, Jr.
Patented Nov. 5, 1946 UNETED? stares PATNT OFFICE "Washington, D. 0.
Application June 5, 1942, Seria lNo. 445,957
ioia'im. (01.102-38) "(Granted under the act of March 3, 1883, s
The invention described herein may be manufactured and used by or for tlieGovernment for governmental purposes, without the payment to invention relates to ordnance. Inone' of its aspects it relates to" a 'cartridge, particularly to a; small-arms cartridge; In another of its aspects it relates to a projectile for use in a A special gun.
mizes recoil because of a smoother acceleration of the projectile and, at the same time, permits extremely accurate engraving of the .projectile or its rotating band with concomitant high efficiency.
Another ob ect of the invention is to provide asimple cartridge embodying the principles of the invention which is adapted for use in conventional firearms.
Another object of the invention is to provide a projectile and gun combination employing separate loading ammunition and embodying the aforesaid principles.
Another object of the invention is to provide a separate loading projectile in accordance with the invention.
Still further objects and advantages of the invention will be apparent from the following description taken in connection with the accompanying drawing in which:
Fig. 1 is a'fragmentary View, partly in section, of a cartridge in accordance with the invention positioned in the chamber of a rifle, and
Fig. 2 is a fragmentary View, partly in section, of a gun and projectile embodying the invention.
The invention involves in combination with an ordnance piece including a gun tube and a powder chamber receiving a propelling charge, a projectile seated in said ordnance piece, said projectile having a small first propulsion surface initially exposed to pressure generated by said charge and a second propulsion surface subsequently exposed to said pressure.
The cartridge embodiment of the invention includes a case providin a powder chamber receiving a propelling charge and having a neck portion providing a relatively small orifice and a projectile seated therein, said projectile having amended April 30, 1928; 370 O. G. 757) a first propulsion surface initially exposed' to pressure generated'by said charge and a second propulsion surface subsequently exposed ,to-said pressure. j
Referring now to Fig. 1, which shows' a cartridge in accordancewith the invention resting within the chamber of a riflei 4', 1 indicates a projectile having a head2 and a shank 3, The cartridge case 5, and also the exposed head 2 of the projectile, have conventional outside dimensions so that the cartridge is of proper size for conventional use. However, the neck 6 of the case is much thicker than the neck of the conventional cartridge, thus providing a relatively small cylindrical orifice 1 in which the cylindrical shank of the projectile is seated with a sliding gas-tight fit. The shank may have a slight forward taper, i. e., it diminishes in size from rear to front, so as to maintain the joint at the orifice gas-tight as the projectile moves forward after firing and, also, to retain the bullet in the case during shipment and handling. The case may also be thickened at the shoulder 8 for reinforcement against rupture at this point.
The projectile is provided with two separate and distinct propulsion surfaces against which the propelling gases generated by the propelling charge act to accelerate the projectile. The primary, or first propulsion surface, is the base 9 of the shank and the secondary propulsion surface is the rearwardly facing area I!) at the base of the projectiles head.
When the piece is fired, gases are rapidly generated by the propellant ll. These gases initially drive the projectile forward by action only upon the relatively small propulsion surface 9.
The acceleration takes place relatively slowly due to the small area upon which the gases are eifective.. When the projectile has advanced in the bore of the rifle a distance equal to the length of the shank, the base 9 of the shank clears the forward end of the orifice 1 thereby giving the gases within the cartridge case egress to the bore of the rifle where they are free to act, not only upon the primary propulsion surface 9, but also, in addition, upon the secondary propulsion surface lB. The accelerating force is thus considerably multiplied and the projectile is rapidly accelerated to the desired velocity.
The principles of the invention as applied to a large gun using separate loading ammunition will be explained with referenceto Fig. 2 of the drawing. The projectile la is provided with a. head 2a, and a shank 3a. The guntube 4a provides the powder chamber to. A collar 6a is provided for the projectile and is analogous to the thickened neck portion 6 of the cartridge case of Fig. 1. A gas-tight sliding joint is provided between the orifice 1a of the collar and the shank of the projectile. The collar and projectile preferably are loaded into the gun as a unit. A gastight jointitla is p'rovided between the collar and the wallsof the powder chamber. The primary propulsion surface is the base 9a of the shank and the secondary propulsion surface is the rearwardly exposed area Ilia at the base of the head. The powder charge Ila is separately loaded into the chamber.
The action of the propelling gases on the projectile in the modification of Fig. 2 is similar to the accelerating action as described in connection with Fig. 1, the propelling gases acting first on the base of the shank and subsequently additionally on the rearwardly facing base of the head.
After firing the gun, it will be necessary to remove the collar 61: before reloading, V
The relative size of shank and head of the projectile are not critical and may be varied within desired limits. The length of the shank may bevaried to give a longer or shorter delay to the full accelerating action of the propelling gases, and the relative areas of the primary and secondary propulsion surfaces may be varied, as the case requires, to regulate the initial acceleration. In general, however, the area of the primary propulsion surface will be distinctly smaller than the area of the total propulsion surface, being preferably less than three quarters thereof.
The term propulsion surface is intended to means a surface of the projectile upon which propelling gases are eifective for acceleration of the projectile. The area of such a surface will be considered to be the rectilinear projection of said area upon a plane perpendicular to the major axis of the projectile.
I claim:
A cartridge comprising an elongated case providing a powder chamber receiving a propelling charge and having a neck portion at one end, said neck portion having thick walls providing a substantially cylindrical orifice, a projectile having a forwardly tapered shank portion extending inwardly through the said orifice of said case, making a sliding gas-tight joint with the inner surface of said orifice and providing a primary propulsion surface at the end of said shank, said projectile having a head portion providing a sec,- ondary propulsion surface, the outside diameter of the head of said projectile being not greater than the outside diameter of the neck portion of said case.
JOHN O. EVANS, JR.
US445957A 1942-06-05 1942-06-05 Cartridge for guns Expired - Lifetime US2410435A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US445957A US2410435A (en) 1942-06-05 1942-06-05 Cartridge for guns

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US445957A US2410435A (en) 1942-06-05 1942-06-05 Cartridge for guns

Publications (1)

Publication Number Publication Date
US2410435A true US2410435A (en) 1946-11-05

Family

ID=23770809

Family Applications (1)

Application Number Title Priority Date Filing Date
US445957A Expired - Lifetime US2410435A (en) 1942-06-05 1942-06-05 Cartridge for guns

Country Status (1)

Country Link
US (1) US2410435A (en)

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2678804A (en) * 1944-06-09 1954-05-18 Schlumberger Well Surv Corp Sample taking projectile
US3602086A (en) * 1968-12-09 1971-08-31 Victor Comptometer Corp Air ignition system ammunition
US4448130A (en) * 1982-07-15 1984-05-15 General Dynamics, Pomona Division Packaging kit for pyrotechnic materials loading
US5063848A (en) * 1990-10-16 1991-11-12 Olin Corporation Igniter bag
US5180883A (en) * 1990-12-22 1993-01-19 Rheinmetall Gmbh Ammunition
US20070056461A1 (en) * 2005-06-10 2007-03-15 Diehl Bgt Defence Gmbh & Co., Kg Weapon system with caseless ammunition

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2678804A (en) * 1944-06-09 1954-05-18 Schlumberger Well Surv Corp Sample taking projectile
US3602086A (en) * 1968-12-09 1971-08-31 Victor Comptometer Corp Air ignition system ammunition
US4448130A (en) * 1982-07-15 1984-05-15 General Dynamics, Pomona Division Packaging kit for pyrotechnic materials loading
US5063848A (en) * 1990-10-16 1991-11-12 Olin Corporation Igniter bag
US5180883A (en) * 1990-12-22 1993-01-19 Rheinmetall Gmbh Ammunition
US20070056461A1 (en) * 2005-06-10 2007-03-15 Diehl Bgt Defence Gmbh & Co., Kg Weapon system with caseless ammunition

Similar Documents

Publication Publication Date Title
US5492063A (en) Reduced energy cartridge
US3485173A (en) Variable centroid projectile
US5677505A (en) Reduced energy cartridge
US5359937A (en) Reduced energy cartridge
US3490330A (en) Firearm,particularly light antitank weapon
US3169333A (en) Projectile for firing a leakproof caseless round
US3062145A (en) Slug for a shotgun shell
US3815503A (en) Self-propelling ballistic projectiles
US3318033A (en) Grenade launching arrangement
US3245350A (en) Rocket propelled device for straightline payload transport
US3185094A (en) Cartridge case extension piece for use with projectiles
US2410435A (en) Cartridge for guns
US2681619A (en) Rocket projectile
US3348484A (en) Flame cartridge
US3326128A (en) Rockets and combinations of rockets and cases
US3618250A (en) Launching arrangement for sub-caliber projectiles
US2654318A (en) Subcaliber adapter
US3619924A (en) Self-obturating gas-operated launcher
US2494562A (en) Rocket projectile
US3307283A (en) Firearm grenade launcher
US20070272111A1 (en) Low Energy Training Cartridge
US3059367A (en) Compensating means in barrel chamber for low and high powered cartridges
US11346621B2 (en) Recoilless apparatus for guns
US10996036B1 (en) Sabot and projectile with improved coupling for better torque transfer
US2579323A (en) Rocket projectile