US677527A - Cartridge. - Google Patents

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Publication number
US677527A
US677527A US56651A US1901056651A US677527A US 677527 A US677527 A US 677527A US 56651 A US56651 A US 56651A US 1901056651 A US1901056651 A US 1901056651A US 677527 A US677527 A US 677527A
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United States
Prior art keywords
charge
perforations
sections
cylinders
cells
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Expired - Lifetime
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US56651A
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Hudson Maxim
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Individual
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Individual
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Priority claimed from US72830499A external-priority patent/US694295A/en
Application filed by Individual filed Critical Individual
Priority to US56651A priority Critical patent/US677527A/en
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    • CCHEMISTRY; METALLURGY
    • C06EXPLOSIVES; MATCHES
    • C06BEXPLOSIVES OR THERMIC COMPOSITIONS; MANUFACTURE THEREOF; USE OF SINGLE SUBSTANCES AS EXPLOSIVES
    • C06B45/00Compositions or products which are defined by structure or arrangement of component of product
    • 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

Definitions

  • Fig. 2- is a View similar to Fig. 1, show ing a charge composed of but two'concentrio cylinders having thicker walls.
  • Fig. 3 shows one of the longitudinal sections into which each cylinder is divided, and Fig. ⁇ L is a side elevation of Fig. 1.
  • 1 indicatesa pludivided into longitudinal sections 2, with the joints 3 between the sections soarranged that joints of adjacent cylinders shall not'lie in By this arrangement I break the joints between the sections of the adjacent cylinders.
  • each of the ion- .gitudinal sections 2 is provided with a pin ralityof lateral perforations 4, preferably extending radially through the section, and a plurality of cells 5', also extending, by preference, in a radial direction into but not through the body of the sections 2.
  • Fig. 1 I have shown the radial perforations 4; without the present'i riyenl' rality'of concentric cylinders, each of which is cells, the walls of the several cylinders in this case being so thin that the-adjacent radial perforations are substantially the same dis- 5 tance apart as their inner and outer ends, and hence the cells are not needed.
  • the perforations 4 act not only as lateral vents, but also adord additional burning-surfaces, while the cells 5 act onlyto'increase the burning-surface, Since both the perforations 4 and the cells 5 adord burning-surfaces, it'is desirable that they'should beso arranged with relation to each other a'snot to interferewith thesim'ultaneons completion of combustionthronghout the mass of the charge, and for this reason the cells dand' perforations are uniformly distributed, so as to provide substantially equal thicknesses of material between each cell or perforation and adjacent cells or perforations, For the purpose ⁇ of securing provided 15' tions.
  • a charge formed as 5 herein described will be one of great cornpactness, thereby securing greater density of loading, and that the charge will possess sufificient rigidity to-carry the projectile, if desired.
  • oE concentric tubes of smokeless powder each of which tubes is built up of a plurality of longitudinal sections provided with uniformlyrgdisposed transverse perforations.
  • An exploslve charge having a plurality of concentric tubes ofexplosive material 1 each of which tubes is built up of aplnrality of transversely-perforated longitudinal sec- 20110115.. g I 3.
  • An explosive charge having a plurality the tubes for the flame of ignition, said tubes or cylinders being divided into a plura1ity; 35
  • An explosive charge having a plurality

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  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Crystallography & Structural Chemistry (AREA)
  • Organic Chemistry (AREA)
  • Heterocyclic Carbon Compounds Containing A Hetero Ring Having Oxygen Or Sulfur (AREA)

Description

Patenied July 2, l90l.
ATTORNEY MBY H. MAXIM.
CARTRIDGE.
(Application filed'Apr. 19, 1901 TRENORRIS PETERS 5a., wn'snmoran, a. c.
(No Model.)
WITNESSES:
- .nunsonlMAXIM,:orBRooKLYN,--New ORK. i
i ljl SPECIFICATION- fornciing-part o f Letters meab .-e7"7,52,: emissary 2', 1eci-.--
To all whom it'mayc oiwcrrtl 'a new and usef'ullmproi emen tin Cartridges, which inventionv is fully lowing specification? rangement of said lateral vents being such as v to secure the simultaneous completion of combustion throughout'the charge. In the pres cnt invention I form a cartridge charge of a plurality of concentric cylinders, each of which may be provided with lateral ventchannels, affording an escape for the gases in alateral direction, and the additional burning-surfaces, as in the application referred to, and I also divide the cylinder longitudinally,
the lines of division being so arranged as to break joints. With cylinders thus composed of longitudinal sections the internal pressure of the gases of combustion will cause the sections to spread or expand rad ially, thereby openingthe joints between the several sections ofany given cylinder and aifording lateral vents for the gases withinfthe cylinder and exposing the surface of the joints to the flame of ignition; with this construction the necessary lateral venting to avoid disruption of the charge is' secured even in' the absence of lateral perforations, as well as the simultaneous completion of combustion of the entire mass of explosive. It is desirable,'however, to provide such lateral perforations in many instances,
as well as cells or holes in the walls of the,
. r g yl der .i 'h' h' s' Be it known that I, HlIDSQNl/IAXIM, a resident 'of Brooklyn, New York, pers s n e 1 set forth in th'e fol 'in jwhichf- In my application, Serial No. 728304;, filed. August 24, 1809,. of whichthe, prese ntappli rokii'. eti'jdn, cation is a division, I'have descr bed a charge ,the same-radial plane.
It will be apparentthat hikedlint. way thronghthc same.
I t e nr 'n't rf l were mace vario'u's' mechanicalexpressionswneefwhich v I have shown in theaccoinpanying drawings,
.eeaws; e11; Q5 c a ges 'expl sir ma? terial formed according to the tion. Fig. 2- is a View similar to Fig. 1, show ing a charge composed of but two'concentrio cylinders having thicker walls. Fig. 3 shows one of the longitudinal sections into which each cylinder is divided, and Fig. {L is a side elevation of Fig. 1. v
Referring to the drawings, 1 indicatesa pludivided into longitudinal sections 2, with the joints 3 between the sections soarranged that joints of adjacent cylinders shall not'lie in By this arrangement I break the joints between the sections of the adjacent cylinders.
As shown in-Figs. 2 and '3, each of the ion- .gitudinal sections 2 isprovided with a pin ralityof lateral perforations 4, preferably extending radially through the section, and a plurality of cells 5', also extending, by preference, in a radial direction into but not through the body of the sections 2. In Fig. 1 I have shown the radial perforations 4; without the present'i riyenl' rality'of concentric cylinders, each of which is cells, the walls of the several cylinders in this case being so thin that the-adjacent radial perforations are substantially the same dis- 5 tance apart as their inner and outer ends, and hence the cells are not needed. The perforations 4 act not only as lateral vents, but also adord additional burning-surfaces, while the cells 5 act onlyto'increase the burning-surface, Since both the perforations 4 and the cells 5 adord burning-surfaces, it'is desirable that they'should beso arranged with relation to each other a'snot to interferewith thesim'ultaneons completion of combustionthronghout the mass of the charge, and for this reason the cells dand' perforations are uniformly distributed, so as to provide substantially equal thicknesses of material between each cell or perforation and adjacent cells or perforations, For the purpose {of securing provided 15' tions.
the several sectional cylinders assembled as shown in Figs. 1 and 2 they may be bound by cords 6 or secured in any suitable manner.-
It will be obvious that a charge formed as 5 herein described will be one of great cornpactness, thereby securing greater density of loading, and that the charge will possess sufificient rigidity to-carry the projectile, if desired.
oE concentric tubes of smokeless powder each of which tubes is built up of a plurality of longitudinal sections provided with uniformlyrgdisposed transverse perforations.
2. An exploslve charge having a plurality of concentric tubes ofexplosive material 1 each of which tubes is built up of aplnrality of transversely-perforated longitudinal sec- 20110115.. g I 3. In an explosive charge a cylindrical mass of explosive materialdivided by radial planes into longitudinal sections, which sections are 1. An explosive charge having a plurality the tubes for the flame of ignition, said tubes or cylinders being divided into a plura1ity; 35
of transversely-perforated longitudinal sectieus.
; of concentric, laterally-vented tubes or cylininders are divided intofa plurality of. longitudinal sections; l
'In. testimony whereof I have signed this specification in the presence of two subscrib-- ing' witnesses.
. "HUDSON MAXIM. Witncsses: I
with transverse orlateral perfora- EDWARD Lyons, LILIAN MAXIM.
6. An explosive charge having a plurality,
' ders of explosiveni-aterial which tubes orcyl- 4o
US56651A 1899-08-24 1901-04-19 Cartridge. Expired - Lifetime US677527A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US56651A US677527A (en) 1899-08-24 1901-04-19 Cartridge.

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US72830499A US694295A (en) 1899-08-24 1899-08-24 Cartridge.
US56651A US677527A (en) 1899-08-24 1901-04-19 Cartridge.

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US677527A true US677527A (en) 1901-07-02

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Cited By (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2575871A (en) * 1947-01-06 1951-11-20 Ici Ltd Granular smokeless propellant powders
US2953971A (en) * 1954-10-04 1960-09-27 Dresser Ind Gun perforator
US3010400A (en) * 1957-10-14 1961-11-28 Phillips Petroleum Co Propellant charge
US3017836A (en) * 1958-08-28 1962-01-23 Phillips Petroleum Co Rocket motor
US3017743A (en) * 1956-01-20 1962-01-23 Phillips Petroleum Co Rocket and propellant charge therefor
US3054353A (en) * 1958-09-23 1962-09-18 Norman L Rumpp Segment grain
US3961581A (en) * 1970-01-27 1976-06-08 Office National D'etudes Et De Recherches Aerospatiales (O.N.E.R.A.) Ignitor element for a generator of hot gas
WO2002083602A1 (en) 2001-04-02 2002-10-24 Nexplo Bofors Ab Propellant and a method and device for producing the same
WO2005057123A1 (en) 2003-12-09 2005-06-23 Eurenco Bofors Ab Progressive propellant charge with high charge density
WO2005057124A1 (en) * 2003-12-09 2005-06-23 Eurenco Bofors Ab Method and arrangement for producing propellant for charges with high charge density and high progressivity
WO2009123528A1 (en) 2008-04-01 2009-10-08 Bae Systems Bofors Ab Method for electrical flashover ignition and combustion of propellent charge, as well as propellent charge and ammunition shot in accordance therewith

Cited By (26)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2575871A (en) * 1947-01-06 1951-11-20 Ici Ltd Granular smokeless propellant powders
US2953971A (en) * 1954-10-04 1960-09-27 Dresser Ind Gun perforator
US3017743A (en) * 1956-01-20 1962-01-23 Phillips Petroleum Co Rocket and propellant charge therefor
US3010400A (en) * 1957-10-14 1961-11-28 Phillips Petroleum Co Propellant charge
US3017836A (en) * 1958-08-28 1962-01-23 Phillips Petroleum Co Rocket motor
US3054353A (en) * 1958-09-23 1962-09-18 Norman L Rumpp Segment grain
US3961581A (en) * 1970-01-27 1976-06-08 Office National D'etudes Et De Recherches Aerospatiales (O.N.E.R.A.) Ignitor element for a generator of hot gas
WO2002083602A1 (en) 2001-04-02 2002-10-24 Nexplo Bofors Ab Propellant and a method and device for producing the same
US20040216823A1 (en) * 2001-04-02 2004-11-04 Johan Dahlberg Propellant and a method and device for producing the same
US20090148549A1 (en) * 2001-04-02 2009-06-11 Eurenco Bofors Ab Propellant and a method and device for producing the same
US7507308B2 (en) * 2001-04-02 2009-03-24 Eurenco Bofors Ab Propellant and a method and device for producing the same
US20080047453A1 (en) * 2003-12-09 2008-02-28 Eurenco Bofors Ab Progressive Propellant Charge With High Charge Density
JP4657220B2 (en) * 2003-12-09 2011-03-23 ユーレンコ ボフォース アーベー Progressive propellant charge with high charge density
US20080282926A1 (en) * 2003-12-09 2008-11-20 Eurenco Bofors Ab Method and Arrangement For Producing Propellant For Charges With High Charge Density and High Progressivity
WO2005057124A1 (en) * 2003-12-09 2005-06-23 Eurenco Bofors Ab Method and arrangement for producing propellant for charges with high charge density and high progressivity
WO2005057123A1 (en) 2003-12-09 2005-06-23 Eurenco Bofors Ab Progressive propellant charge with high charge density
CN1914478B (en) * 2003-12-09 2013-11-06 尤伦科伯福斯股份公司 Method and arrangement for producing propellant for charges with high charge density and high progressivity
AU2004297496B2 (en) * 2003-12-09 2010-07-15 Eurenco Bofors Ab Progressive propellant charge with high charge density
JP2007514126A (en) * 2003-12-09 2007-05-31 ユーレンコ ボフォース アーベー Method and apparatus for producing a propellant for a charge with high charge density and high graduality
US7918163B2 (en) * 2003-12-09 2011-04-05 Eurenco Bofors Ab Progressive propellant charge with high charge density
US7921777B2 (en) 2003-12-09 2011-04-12 Eurenco Bofors Ab Method and arrangement for producing propellant for charges with high charge density and high progressivity
US8544387B2 (en) 2003-12-09 2013-10-01 Eurenco Bofors Ab Progressive propellant charge with high charge density
CN1914477B (en) * 2003-12-09 2012-06-13 尤伦科伯福斯股份公司 Progressive propellant charge with high charge density
US20110174184A1 (en) * 2008-04-01 2011-07-21 Ola Stark Method for electrical flashover ignition and combustion of propellent charge, as well as propellent charge and ammunition shot in accordance therewith
WO2009123528A1 (en) 2008-04-01 2009-10-08 Bae Systems Bofors Ab Method for electrical flashover ignition and combustion of propellent charge, as well as propellent charge and ammunition shot in accordance therewith
US8607704B2 (en) 2008-04-01 2013-12-17 Bae Systems Bofors Ab Method for electrical flashover ignition and combustion of propellent charge, as well as propellent charge and ammunition shot in accordance therewith

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