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GB164697A - New type of cannon with high initial velocity - Google Patents

New type of cannon with high initial velocity

Info

Publication number
GB164697A
GB164697A GB15906/21A GB1590621A GB164697A GB 164697 A GB164697 A GB 164697A GB 15906/21 A GB15906/21 A GB 15906/21A GB 1590621 A GB1590621 A GB 1590621A GB 164697 A GB164697 A GB 164697A
Authority
GB
United Kingdom
Prior art keywords
cannon
new type
main barrel
initial velocity
high initial
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
Application number
GB15906/21A
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.)
CHEVALIER GERVASIO GENTINI
Original Assignee
CHEVALIER GERVASIO GENTINI
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 CHEVALIER GERVASIO GENTINI filed Critical CHEVALIER GERVASIO GENTINI
Publication of GB164697A publication Critical patent/GB164697A/en
Expired legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41—WEAPONS
    • F41A—FUNCTIONAL FEATURES OR DETAILS COMMON TO BOTH SMALLARMS AND ORDNANCE, e.g. CANNONS; MOUNTINGS FOR SMALLARMS OR ORDNANCE
    • F41A1/00—Missile propulsion characterised by the use of explosive or combustible propellant charges
    • F41A1/02—Hypervelocity missile propulsion using successive means for increasing the propulsive force, e.g. using successively initiated propellant charges arranged along the barrel length; Multistage missile propulsion

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • General Engineering & Computer Science (AREA)
  • Filling Or Discharging Of Gas Storage Vessels (AREA)

Abstract

164,697. Gentini, C. G. June 10, 1920, [Convention date]. Void [Published under Sect. 91 of the Act]. Ordnance, multicharge. - Auxiliary barrels d, e, f are provided, communicating by ports with the main barrel a and containing charges which are automatically and successively ignited by the gases in the main barrel after the projectile l has passed the respective ports. The auxiliary barrels may be symmetrically disposed or inclined with respect to the main barrel. To prevent escape of the auxiliary charge gases, a double checkring is provided, at the front of the projectile.
GB15906/21A 1920-06-10 1921-06-09 New type of cannon with high initial velocity Expired GB164697A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
IT164697X 1920-06-10

Publications (1)

Publication Number Publication Date
GB164697A true GB164697A (en) 1921-09-22

Family

ID=11148894

Family Applications (1)

Application Number Title Priority Date Filing Date
GB15906/21A Expired GB164697A (en) 1920-06-10 1921-06-09 New type of cannon with high initial velocity

Country Status (2)

Country Link
FR (1) FR536387A (en)
GB (1) GB164697A (en)

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1056968B (en) * 1955-08-19 1959-05-06 Boelkow Entwicklungen Kg Barrel with several propellants distributed over the length of the barrel
DE1082834B (en) * 1955-08-19 1960-06-02 Boelkow Entwicklungen Kg Propellant charge to accelerate a projectile
US2986072A (en) * 1952-11-19 1961-05-30 Colin M Hudson Liquid fuel catapult
DE1116111B (en) * 1958-03-29 1961-10-26 Busch Jaeger Duerener Metall Missile launcher
US6089139A (en) * 1998-08-20 2000-07-18 Russell; Ronnie David Porous nozzle projectile barrel
FR2792399A1 (en) * 1999-04-19 2000-10-20 Giat Ind Sa Projectile launcher with multiple charges uses controlled time delay between charges to determine exact speed of launch
WO2004070308A2 (en) * 2003-02-10 2004-08-19 Salvatore Tedde Firearm with supplementary firing chamber

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2986072A (en) * 1952-11-19 1961-05-30 Colin M Hudson Liquid fuel catapult
DE1056968B (en) * 1955-08-19 1959-05-06 Boelkow Entwicklungen Kg Barrel with several propellants distributed over the length of the barrel
DE1082834B (en) * 1955-08-19 1960-06-02 Boelkow Entwicklungen Kg Propellant charge to accelerate a projectile
DE1116111B (en) * 1958-03-29 1961-10-26 Busch Jaeger Duerener Metall Missile launcher
US6089139A (en) * 1998-08-20 2000-07-18 Russell; Ronnie David Porous nozzle projectile barrel
FR2792399A1 (en) * 1999-04-19 2000-10-20 Giat Ind Sa Projectile launcher with multiple charges uses controlled time delay between charges to determine exact speed of launch
WO2004070308A2 (en) * 2003-02-10 2004-08-19 Salvatore Tedde Firearm with supplementary firing chamber
WO2004070308A3 (en) * 2003-02-10 2004-11-25 Salvatore Tedde Firearm with supplementary firing chamber

Also Published As

Publication number Publication date
FR536387A (en) 1922-05-01

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