US3413923A - Rifle grenade - Google Patents

Rifle grenade Download PDF

Info

Publication number
US3413923A
US3413923A US652826A US65282667A US3413923A US 3413923 A US3413923 A US 3413923A US 652826 A US652826 A US 652826A US 65282667 A US65282667 A US 65282667A US 3413923 A US3413923 A US 3413923A
Authority
US
United States
Prior art keywords
grenade
plate
spherical
tail
rod
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
US652826A
Inventor
Baton Boris
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.)
Anstalt Fuer die Entwicklung von Erfindungen und Gewerblichen Anwendungen ENERGA
Original Assignee
Anstalt Fuer die Entwicklung von Erfindungen und Gewerblichen Anwendungen ENERGA
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 Anstalt Fuer die Entwicklung von Erfindungen und Gewerblichen Anwendungen ENERGA filed Critical Anstalt Fuer die Entwicklung von Erfindungen und Gewerblichen Anwendungen ENERGA
Application granted granted Critical
Publication of US3413923A publication Critical patent/US3413923A/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
    • F42B3/00Blasting cartridges, i.e. case and explosive
    • F42B3/04Blasting cartridges, i.e. case and explosive for producing gas under pressure
    • 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
    • F42B10/02Stabilising arrangements
    • F42B10/04Stabilising arrangements using fixed fins
    • F42B10/06Tail fins
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42BEXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B30/00Projectiles or missiles, not otherwise provided for, characterised by the ammunition class or type, e.g. by the launching apparatus or weapon used
    • F42B30/04Rifle grenades

Definitions

  • a rifle grenade having a body of substantially spherical shape, a tubular tail-rod connected at one pole of the sphere, a tubular nipple disposed at the opposite pole of the sphere, a circular plate of the diameter of the body and fixed to the vnipple, a ballistic cap enclosing a firing device and disposed above the plate, a cylindrical casing supported against the plate, the cylindrical body and the tail-rod, and a closed peripheral space below the plate and between the casing and the spherical body.
  • This invention relates to a rifle grenade.
  • a rifle grenade comprising a steel body of substantially spherical shape, a tubular tail-rod connected thereto at one pole of said sphere, a tubular nipple disposed at the opposite pole of said spherical body, a circular plate of the diameter of said body and fixed to said nipple, a ballistic cap enclosing a firing device and disposed above said plate, a cylindrical casing supported against the plate, the spherical body and the tail-rod, and a closed peripheral space below the plate and between said casing and the spherical body.
  • the plate occupying the entire section defined by the calibre can support a firing device or fuse mechanism, which may, for example, be percussion or inertia operated and the 'diameter of which exceeds the diameter of the nipple through which firing of the explosive is initiated.
  • a firing device or fuse mechanism which may, for example, be percussion or inertia operated and the 'diameter of which exceeds the diameter of the nipple through which firing of the explosive is initiated.
  • the primer of this mechanism can, during storage, be in an eccentric position at a suflicient distance from the axis of the grenade.
  • peripheral space enclosed between the said spherical body and the cylindrical casing may accommodate, if desired, one or more fuse parts.
  • the tubular tail-rod of the grenade has an end wall integral therewith the upper surface of which is in the form of a spherical socket the concavity of which corresponds to the curvature of the spherical body.
  • the spherical body of the grenade is axially fixed to the end wall of the tubular tail-rod by means of a screw passing through the wall of the spherical body.
  • the grenade has a ballistic. cap which encloses a firing device (not shown).
  • the bottom edge of the ballistic cap is supported by the corresponding edge of a plate 1a situated above a spherical steel body 2 comprising two substantially hemispherical shells which are welded together at 2a, the plate 1a having the same diameter as the body 2.
  • tail-rod 3 preferably made of light metal (for example an aluminium alloy), the tail-rod being provided with tail fins 4 near its free end.
  • the steel body 2 of the grenade encloses a detonator 5 which is embedded in a hollow cylindrical cake of explosive 6 in contact with the principal explosive 7 occupying the remainder of free space inside the body 2.
  • a screw 8 passing through an aperture formed in the bottom pole of the body 2 engages a tapped bore of an end wall 9 closing the top end of the tail-rod 3.
  • This end wall which is integral with the tail-rod, has a spherical socket-shaped upper surface in which the concave spherical zone corresponds to the body 2.
  • a thin-walled cylindrical casing 10 bears against the lower edge of the plate 1a, the spherical body 2 (at the location of the weld seam 2a) and an annular shoulder of the tail-rod 3.
  • the spherical body is also formed, at its upper pole, with a cylindrical nipple 11 formed with an internal screw thread into which there is screwed a hollow shank which is integral with the plate 1a and which retains the detonator 5.
  • the acceleration produced when the grenade is shot from the rifle causes this cap 12, due to its inertia, to leave its seating and fall into the peripheral space enclosed between the casing 10 and the body 2.
  • a rifle grenade comprising a steel body of substantially spherical shape, a tubular tail-rod connected thereto at one pole of said sphere, a tubular nipple disposed at the opposite pole of said spherical body, a circular pate of the diameter of said body and fixed to said nipple, a ballistic cap enclosing a firing device and disposed above said plate, a cylindrical casing supported against the plate, the spherical body and the tail-rod, and a closed peripheral space below the plate and between said casing and the spherical body.
  • tubular tail-rod of the grenade has an end wall integral therewith and has a top surface in the form of a spherical socket having a concave spherical zone corresponding to said body.

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Telescopes (AREA)
  • Respiratory Apparatuses And Protective Means (AREA)

Description

Dec. 3, 1968 BATOU 3,413,923
RIFLE GRENADE] Filed July 12, 1967 //v VE/VTOR 3on1? 3a 20 w ,wmfhamg 81M United States Patent 3,413,923 RIFLE GRENADE Boris Baton, Geneva, Switzerland, assignor to Anstalt fur die Entwicklung von Erfindungen und gewerblichen Anwendungen ENERGA, Vaduz, Liechtenstein Filed July 12, 1967, Ser. No. 652,826 Claims priority, application Switzerland, Aug. 29, 1966, 12,566/ 66 3 Claims. (Cl. 10265.2)
ABSTRACT OF THE DISCLOSURE A rifle grenade having a body of substantially spherical shape, a tubular tail-rod connected at one pole of the sphere, a tubular nipple disposed at the opposite pole of the sphere, a circular plate of the diameter of the body and fixed to the vnipple, a ballistic cap enclosing a firing device and disposed above the plate, a cylindrical casing supported against the plate, the cylindrical body and the tail-rod, and a closed peripheral space below the plate and between the casing and the spherical body.
This invention relates to a rifle grenade.
It is an object of the invention to provide a light-weight, compact rifle grenade of simple and economical construction, the efliciency and splinter-producing capabilities of which fulfill the requirements exacted by warfare.
According to the present invention there is provided a rifle grenade, comprising a steel body of substantially spherical shape, a tubular tail-rod connected thereto at one pole of said sphere, a tubular nipple disposed at the opposite pole of said spherical body, a circular plate of the diameter of said body and fixed to said nipple, a ballistic cap enclosing a firing device and disposed above said plate, a cylindrical casing supported against the plate, the spherical body and the tail-rod, and a closed peripheral space below the plate and between said casing and the spherical body.
With the present construction, it is possible to produce, at a relative reduction in missile bulk, an anti-man rifle grenade which is capable of producing a large number of splinters thrown in all directions.
The plate occupying the entire section defined by the calibre can support a firing device or fuse mechanism, which may, for example, be percussion or inertia operated and the 'diameter of which exceeds the diameter of the nipple through which firing of the explosive is initiated. Thus the primer of this mechanism can, during storage, be in an eccentric position at a suflicient distance from the axis of the grenade.
Furthermore the peripheral space enclosed between the said spherical body and the cylindrical casing may accommodate, if desired, one or more fuse parts.
In one particular embodiment of the invention the tubular tail-rod of the grenade has an end wall integral therewith the upper surface of which is in the form of a spherical socket the concavity of which corresponds to the curvature of the spherical body. Thus there is obtained a stable and resistant seating which is capable of withstanding, at the commencement of thrust, the inertia resulting from the acceleration of the body and fuse of the grenade.
In a preferred embodiment of the invention the spherical body of the grenade is axially fixed to the end wall of the tubular tail-rod by means of a screw passing through the wall of the spherical body.
In order to enable the invention to be more readily understood, reference Will now be made to the accompanying drawing, which illustrated diagrammatically and 3,413,923 Patented Dec. 3, 1968 ICC by way of example a partial longitudinal section through a rifle grenade according to the invention.
Referring now to the drawing, the grenade has a ballistic. cap which encloses a firing device (not shown). The bottom edge of the ballistic cap is supported by the corresponding edge of a plate 1a situated above a spherical steel body 2 comprising two substantially hemispherical shells which are welded together at 2a, the plate 1a having the same diameter as the body 2.
Below the bottom pole of the spherical body there is disposed a tubular tail-rod 3, preferably made of light metal (for example an aluminium alloy), the tail-rod being provided with tail fins 4 near its free end.
The steel body 2 of the grenade encloses a detonator 5 which is embedded in a hollow cylindrical cake of explosive 6 in contact with the principal explosive 7 occupying the remainder of free space inside the body 2. A screw 8 passing through an aperture formed in the bottom pole of the body 2 engages a tapped bore of an end wall 9 closing the top end of the tail-rod 3. This end wall, which is integral with the tail-rod, has a spherical socket-shaped upper surface in which the concave spherical zone corresponds to the body 2.
A thin-walled cylindrical casing 10 bears against the lower edge of the plate 1a, the spherical body 2 (at the location of the weld seam 2a) and an annular shoulder of the tail-rod 3. The spherical body is also formed, at its upper pole, with a cylindrical nipple 11 formed with an internal screw thread into which there is screwed a hollow shank which is integral with the plate 1a and which retains the detonator 5.
Finally, a cap 12, passing through the plate 1a and projecting below it, keeps the firing device in a safe condition during storage and before the commencement of thrust. The acceleration produced when the grenade is shot from the rifle causes this cap 12, due to its inertia, to leave its seating and fall into the peripheral space enclosed between the casing 10 and the body 2.
What I claim is:
1. A rifle grenade, comprising a steel body of substantially spherical shape, a tubular tail-rod connected thereto at one pole of said sphere, a tubular nipple disposed at the opposite pole of said spherical body, a circular pate of the diameter of said body and fixed to said nipple, a ballistic cap enclosing a firing device and disposed above said plate, a cylindrical casing supported against the plate, the spherical body and the tail-rod, and a closed peripheral space below the plate and between said casing and the spherical body.
2. A rifle grenade as claimed in claim 1, wherein the tubular tail-rod of the grenade has an end wall integral therewith and has a top surface in the form of a spherical socket having a concave spherical zone corresponding to said body.
3. A rifle grenade as claimed in claim 2, wherein the spherical body of the grenade is axially fixed to the end wall of said tubular tail-rod by means of a screw passing through the wall of said body.
References Cited UNITED STATES PATENTS 2,408,486 10/ 1946 Shinkle 102-64 2,420,661 5/ 1947 Fox 102-65.2
FOREIGN PATENTS 79,873 6/1919 Germany. 717,204 5/1931 France.
BENJAMIN A. BORCHELT, Primary Examiner, J. FOX, Assistant Examiner.
US652826A 1966-08-29 1967-07-12 Rifle grenade Expired - Lifetime US3413923A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CH1256666A CH457197A (en) 1966-08-29 1966-08-29 Rifle grenade

Publications (1)

Publication Number Publication Date
US3413923A true US3413923A (en) 1968-12-03

Family

ID=4384217

Family Applications (1)

Application Number Title Priority Date Filing Date
US652826A Expired - Lifetime US3413923A (en) 1966-08-29 1967-07-12 Rifle grenade

Country Status (9)

Country Link
US (1) US3413923A (en)
AT (1) AT280104B (en)
BE (1) BE699161A (en)
CH (1) CH457197A (en)
DE (1) DE1578066A1 (en)
ES (1) ES344554A1 (en)
GB (1) GB1138926A (en)
NL (1) NL6709943A (en)
NO (1) NO122173B (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4016816A (en) * 1975-06-20 1977-04-12 Forenade Fabriksverken Shell especially for mortars
FR2371666A1 (en) * 1976-11-23 1978-06-16 Alsetex Stabilising fins for mortar fired grenade - has tube carrying fins bolted to explosive head with gun barrel seal between

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
SE7906604L (en) * 1978-09-22 1980-03-23 Sarmac Sa GEVERSGRANAT
CN111211021B (en) * 2020-01-09 2022-03-25 四川蓝狮科技有限公司 Miniature gas generator of quick fusing device

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE79873C (en) *
FR717204A (en) * 1930-05-20 1932-01-05 Grenade and Grenade Launcher
US2408486A (en) * 1945-03-28 1946-10-01 Edward M Shinkle Hand grenade and fuse therefor
US2420661A (en) * 1945-07-03 1947-05-20 Fox William Mervin Grenade adapter

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE79873C (en) *
FR717204A (en) * 1930-05-20 1932-01-05 Grenade and Grenade Launcher
US2408486A (en) * 1945-03-28 1946-10-01 Edward M Shinkle Hand grenade and fuse therefor
US2420661A (en) * 1945-07-03 1947-05-20 Fox William Mervin Grenade adapter

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4016816A (en) * 1975-06-20 1977-04-12 Forenade Fabriksverken Shell especially for mortars
FR2371666A1 (en) * 1976-11-23 1978-06-16 Alsetex Stabilising fins for mortar fired grenade - has tube carrying fins bolted to explosive head with gun barrel seal between

Also Published As

Publication number Publication date
DE1578066A1 (en) 1971-09-30
BE699161A (en) 1967-11-03
GB1138926A (en) 1969-01-01
NO122173B (en) 1971-05-24
CH457197A (en) 1968-05-31
NL6709943A (en) 1968-03-01
ES344554A1 (en) 1968-10-16
AT280104B (en) 1970-03-25

Similar Documents

Publication Publication Date Title
US3134330A (en) Projectile
US2426997A (en) Projectile
US5979332A (en) Fragmentation body for a fragmentation projectile
US4899661A (en) Projectile containing a fragmentation jacket
NO316339B1 (en) Br degree no degree stainless, ballistic blasting projectile
US3413923A (en) Rifle grenade
NO884373L (en) Post for warhead.
US20020011173A1 (en) Pyrotechnic impact fuse
US2672094A (en) Fuze
US2441388A (en) Projectile
US3430568A (en) Delay actuator
GB625333A (en) Improvements in or relating to projectiles
US4428294A (en) Finless gun-fired practice round
KR870002026B1 (en) Rifle grenade
US2455603A (en) Fuse
CA1071020A (en) Explosive projectile
RU2001115648A (en) Head fuse
US3292543A (en) Projectile
NO168836B (en) DRILL BASKET ADDITIVE CONTAINING XANTAN WITH 5 - 9% WEIGHT PYRODRUIC ACID
US2436378A (en) Fuze
EP0084095A2 (en) Ballistic propulsion system for rifle grenades and similar projectiles
US3427975A (en) Anti-pillaring white phosphorus projectile
US3537398A (en) Rifle grenade
GB2134231A (en) A hollow-charge warhead
US1172636A (en) Projectile.