US1301381A - Incendiary projectile. - Google Patents

Incendiary projectile. Download PDF

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Publication number
US1301381A
US1301381A US17826517A US17826517A US1301381A US 1301381 A US1301381 A US 1301381A US 17826517 A US17826517 A US 17826517A US 17826517 A US17826517 A US 17826517A US 1301381 A US1301381 A US 1301381A
Authority
US
United States
Prior art keywords
bullet
phosphorus
incendiary
filling
projectile
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
US17826517A
Inventor
James Frank Buckingham
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 US17826517A priority Critical patent/US1301381A/en
Application granted granted Critical
Publication of US1301381A publication Critical patent/US1301381A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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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
    • F42B12/36Projectiles, 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
    • F42B12/38Projectiles, 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 tracer type
    • 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

  • the phosphorus there is 1 mixed withthe phosphorus a spongy or jmore'or less finely divided material which serves to conduct the heat rapidly along the interior of the bullet.
  • This substance does not necessarily have any chemical action upon. thecombustible substance of the bullet, but it may be combustible when it issues from the bullet.
  • powdered 0r finely div vided aluminium or other metal may be used.
  • the degree of division depends largely upon the size ofthe bullet or shell. Inthe case of a small bullet the heat conducting substance would be very finely powdered. In a large shell the substance might be in the form of shots or wire. The result in both j cases is that the heat at the rear of the bullet is more quickly conducted along the interior than isotherwise the case. Thus the a phosphorus is caused to be melted more j Gopies of this patent may be obtained for Specification of Letters Patent.
  • a smaller outlet may be employed and instead of obtaining .a large flame directly the cartridge is fired as is the case when a large outlet is used there is a'smaller flame at the commencement and this is more sustained throughout the flight of the bullet.
  • incendiary projectiles have been proposed containing an incendiary composition which includes finely divided metallic substances, but these sub stances were used for their combustible properties and not as heat conductors merely to assist the melting of the remaining contents.

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • General Engineering & Computer Science (AREA)
  • Fireproofing Substances (AREA)

Description

A I No Drawing.
Toall whom it may concern:
Be it lmown that I, JAMES FRANK BUCK- 'INGHAM, a subject of the King of England, residing int-he county of Warwick, England, have invented certain new and useful Improvements in Incendiary Projectiles, of which the following is a specification. This invention relates to incendiary bullets, shells, and the like of the kind in which a hollow bullet or shell case contains phosphorus which, due to the heat of the explosion of the cartridge, melts and flows out through orifices in the back or sides of the bullet. A bullet of this kind is described .I in the specification accompanying my prior T patent application No. 17 8,264. It is the object of the present invention to provide simple means for enabling the heat to be conducted along the interior of the bullet more quickly, so that it operates more rapidly than would otherwise be the case.
' 'elapses afterjfiring of the cartridge before A theflame issues from the bullet. By the present invention this period is reduced and ,i the combustion may be added to.
According to this invention, there is 1 mixed withthe phosphorus a spongy or jmore'or less finely divided material which serves to conduct the heat rapidly along the interior of the bullet. This substance does not necessarily have any chemical action upon. thecombustible substance of the bullet, but it may be combustible when it issues from the bullet. I As an example, powdered 0r finely div vided aluminium or other metal may be used. 1- The degree of division depends largely upon the size ofthe bullet or shell. Inthe case of a small bullet the heat conducting substance would be very finely powdered. In a large shell the substance might be in the form of shots or wire. The result in both j cases is that the heat at the rear of the bullet is more quickly conducted along the interior than isotherwise the case. Thus the a phosphorus is caused to be melted more j Gopies of this patent may be obtained for Specification of Letters Patent.
With. some kinds of bullet a certain period STATES PATENT OFFICE.
INCENDIARY PROJEC'IILE.
Patented Apr. 22, 1919.
Application filed July 2, 1917. Serial No. 178,265.
quickly and starts to issue sooner from the bullet than would otherwise be the case. A smaller outlet may be employed and instead of obtaining .a large flame directly the cartridge is fired as is the case when a large outlet is used there is a'smaller flame at the commencement and this is more sustained throughout the flight of the bullet.
I am aware that incendiary projectiles have been proposed containing an incendiary composition which includes finely divided metallic substances, but these sub stances were used for their combustible properties and not as heat conductors merely to assist the melting of the remaining contents.
What I claim as my invention and desire to secure by Letters Patent is 1. In a hollow projectile of the kind described provided with a discharging orifice, a phosphorus filling and a heat conducting substance mixed with the phosphorus filling.
2. In a hollow projectile of the kind described provided with a discharging orifice,
'a phosphorus filling and a spongy heat conducting substance mixed with the phosphorus filling.
3. In a hollow projectile of the kind described provided with a discharging orifice, a phosphorus filling and a finely divided heat conducting substance mixed with the phosphorus filling.
4. In-a hollow projectile of the kind described provided with a discharging orifice, a phosphorus filling and powdered aluminium mixed with the phosphorus filling.
5. In a hollow! projectile of the kind described, a phosphorus filling and finely divided aluminium mixed with the phosphorus filling.
In testimony whereof I have signed my name to this specification in the presence of two subscribing witnesses.
JAMES FRANK BUOKINGHAM.
Witnesses:
ALBERT BROWN, ANNIE L. WADE.
five cents each, by addressing the "Commissioner of Patents, Washington, D. 0.
US17826517A 1917-07-02 1917-07-02 Incendiary projectile. Expired - Lifetime US1301381A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US17826517A US1301381A (en) 1917-07-02 1917-07-02 Incendiary projectile.

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US17826517A US1301381A (en) 1917-07-02 1917-07-02 Incendiary projectile.

Publications (1)

Publication Number Publication Date
US1301381A true US1301381A (en) 1919-04-22

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Family Applications (1)

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US17826517A Expired - Lifetime US1301381A (en) 1917-07-02 1917-07-02 Incendiary projectile.

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Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3000308A (en) * 1956-03-07 1961-09-19 William E Land High explosive composition
US3022735A (en) * 1957-10-10 1962-02-27 Phillips Petroleum Co Solid rocket propellants
US3109375A (en) * 1956-12-07 1963-11-05 Atlantic Res Corp Propellent grains
US3109374A (en) * 1956-12-07 1963-11-05 Atlantic Res Corp Propellent grains
US3128706A (en) * 1959-04-17 1964-04-14 Atlantic Res Corp Monopropellent grains
US3129562A (en) * 1960-10-21 1964-04-21 United Aircraft Corp Method and means for improving combustion characteristics of solid propellants
US3140663A (en) * 1955-06-09 1964-07-14 Atlantic Res Corp Propellent grains
US3228338A (en) * 1966-01-11 Jpn+pb

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3228338A (en) * 1966-01-11 Jpn+pb
US3140663A (en) * 1955-06-09 1964-07-14 Atlantic Res Corp Propellent grains
US3000308A (en) * 1956-03-07 1961-09-19 William E Land High explosive composition
US3109375A (en) * 1956-12-07 1963-11-05 Atlantic Res Corp Propellent grains
US3109374A (en) * 1956-12-07 1963-11-05 Atlantic Res Corp Propellent grains
US3022735A (en) * 1957-10-10 1962-02-27 Phillips Petroleum Co Solid rocket propellants
US3128706A (en) * 1959-04-17 1964-04-14 Atlantic Res Corp Monopropellent grains
US3129562A (en) * 1960-10-21 1964-04-21 United Aircraft Corp Method and means for improving combustion characteristics of solid propellants

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