BE827381A - PROJECTILE FOR OBUSIER - Google Patents

PROJECTILE FOR OBUSIER

Info

Publication number
BE827381A
BE827381A BE154947A BE154947A BE827381A BE 827381 A BE827381 A BE 827381A BE 154947 A BE154947 A BE 154947A BE 154947 A BE154947 A BE 154947A BE 827381 A BE827381 A BE 827381A
Authority
BE
Belgium
Prior art keywords
projectile
emi
tip
shell
breaking
Prior art date
Application number
BE154947A
Other languages
French (fr)
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 filed Critical
Priority to BE154947A priority Critical patent/BE827381A/en
Publication of BE827381A publication Critical patent/BE827381A/en

Links

Classifications

    • 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
    • F42B30/08Ordnance projectiles or missiles, e.g. shells

Landscapes

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

Description

       

  "Projectile pour obusier"

  
La présente invention est relative à un projectile ou obus pour obusier , constitué par un corps , une queue avec des ailettes de stabilisation et un embout de fusée. 

  
Il est courant de réaliser le corps du projectile sous une forme renflée à son extrémité avant , de telle sorte qu'il apparaisse entre l'embout de fusée et l'extrémité avant du corps , un gradin et la surface d'embout de fusée se raccorde



  "Howitzer projectile"

  
The present invention relates to a projectile or shell for a howitzer, consisting of a body, a tail with stabilization fins and a rocket tip.

  
It is common to make the body of the projectile in a shape swollen at its front end, so that between the rocket tip and the front end of the body appears a step and the rocket tip surface is connects


    

Claims (1)

<EMI ID=1.1> <EMI ID = 1.1> de l'amélioration des caractéristiques de trajectoire de tels projectiles. Suivant L'invention ceci est obtenu grâce-.au fait improving the trajectory characteristics of such projectiles. According to the invention this is obtained thanks to the fact <EMI ID=2.1> <EMI ID = 2.1> tinue et sans brisure à celle du corps de l'obus.. tinny and without breaking to that of the shell body. <EMI ID=3.1> <EMI ID = 3.1> ressortiront de la description ci-après , donnée à titre d'exemple non limitatif et en se référant au dessin annexé , dont la figure unique est une vue en élévation d'un projectile. will emerge from the following description, given by way of non-limiting example and with reference to the appended drawing, the single figure of which is an elevational view of a projectile. L'obus du projectile désigné dans son ensemble par-la référence 1 est constitué par un corps 2, une queue 3 avec-des..ailettes de stabilisation 4 et un embout de fusée 5, muni d'une fusée percutante 6. L'enveloppe 7 de l'embout de fus&#65533;e The shell of the projectile designated as a whole by the reference 1 consists of a body 2, a tail 3 with stabilizing fins 4 and a fuse tip 5, fitted with a percussion fuze 6. The shell 7 of the spindle tip 5 se raccorde en 8 de manière continue et sans brisure à l'enveloppe 9 du corps d'obus 2. 5 is connected at 8 continuously and without breaking to the casing 9 of the shell body 2. Il s'est révélé d'une manière surprenante que cette continuité des enveloppes améliore la précision de tir du projectile pour obusier . It has surprisingly been found that this continuity of envelopes improves the firing accuracy of the howitzer projectile. Il doit être entendu que la présente invention n'est en aucune façon limitée aux formes de réalisation ci-avant It should be understood that the present invention is in no way limited to the above embodiments. et que bien des modifications peuvent y être apportées sans sortir du cadre du présente brevet. and that many modifications can be made to it without departing from the scope of the present patent. REVENDICATIONS 1. Projectile pour obusier , constitué par un 1. Projectile for howitzer, consisting of a corps, une queue avec des ailettes de stabilisation et un embout body, a tail with stabilizing fins and a tip de fusée , caractérisé en ce que la surface de l'embout de fusée rocket, characterized in that the surface of the rocket tip se raccorde de manière continue et sans brisure à celle du corps connects continuously and without breaking to that of the body du projectile. of the projectile. <EMI ID=4.1> <EMI ID = 4.1> avant ou conforme au dessin annexé. before or in accordance with the attached drawing.
BE154947A 1975-03-28 1975-03-28 PROJECTILE FOR OBUSIER BE827381A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
BE154947A BE827381A (en) 1975-03-28 1975-03-28 PROJECTILE FOR OBUSIER

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
BE154947A BE827381A (en) 1975-03-28 1975-03-28 PROJECTILE FOR OBUSIER
BE827381 1975-03-28

Publications (1)

Publication Number Publication Date
BE827381A true BE827381A (en) 1975-07-16

Family

ID=25648492

Family Applications (1)

Application Number Title Priority Date Filing Date
BE154947A BE827381A (en) 1975-03-28 1975-03-28 PROJECTILE FOR OBUSIER

Country Status (1)

Country Link
BE (1) BE827381A (en)

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Legal Events

Date Code Title Description
RE Patent lapsed

Owner name: BRUDER ASSMANN

Effective date: 19870331