US1042176A - Artillery-projectile. - Google Patents

Artillery-projectile. Download PDF

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Publication number
US1042176A
US1042176A US69114612A US1912691146A US1042176A US 1042176 A US1042176 A US 1042176A US 69114612 A US69114612 A US 69114612A US 1912691146 A US1912691146 A US 1912691146A US 1042176 A US1042176 A US 1042176A
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Prior art keywords
head
projectile
shell
artillery
shrapnel
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Expired - Lifetime
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US69114612A
Inventor
Karl Voeller
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Individual
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Priority to US69114612A priority Critical patent/US1042176A/en
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    • 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
    • F42B12/20Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect of high-explosive type
    • F42B12/22Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect of high-explosive type with fragmentation-hull construction
    • F42B12/32Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect of high-explosive type with fragmentation-hull construction the hull or case comprising a plurality of discrete bodies, e.g. steel balls, embedded therein or disposed around the explosive charge

Definitions

  • the head of the projectile as a grenade as well as providing it with an incendiary composition
  • the additional result is gained as compared with the invention disclosed by the before noted application for patent, that in consequence of the explosive action of the head of the shell, anair ship will be hit and destroyed by some part ofv the projectile, although it may not be hit by the whole projectile or by the detached head.
  • FIG. 1 is a vertical longitudinal sectional view.
  • Fig. 2 is a cross-section on line 2 2
  • Fig. l is a diagrammatic view
  • Fig. 4 is a diagrammatic view illustrating the flight and explosion.
  • the main bodyo of the shell is construct ed as in the before noted application for patent as a shrapnel containing chamber, whose charge will be ignited by the time fuse b at a certain point of the path by means of the priming channels c and d. This causes the shrapnel bullets to be expelled in a'comparatively narrow cone, and the head of the projectile continues its flight, as shown diagrammatically in Fig. 4.
  • the inflammable composition e At the rear or inner end of the head Z of the shell is the inflammable composition e, which, as shown in Fig. 2, is pressed into an annular shape and is connected with the channel c by a small cross passage f.' As soon as the shrapnel explodes and the detachable head continues its flight, the inflammable composition e is ignited and burns during the further flight of the head Z of the shell, leaving behind a trail of smoke of predetermined length, by which it is more easily seen and range calculated. In the head besides the incendiary material e there is also the ⁇ explosive charge z'. This is detonated as soon as the inflammable material e is burnt away.
  • An artillery projectile adapted for firing at airships comprising, in combination with a shell containing shrapnel, a separable portion, inflammable smoke-producing material extending over a comparatively extended area within the separable portion, and an explosive charge in said separable portion which is designed to be ignited by said inflammable material.
  • An artillery pro'ectlle adapted for firing at airships, comprising, in combination with a shell containingshrapnel, a separable portion having a groove extending substantially around its axis, inlammablesmoketially around lts axis, an inammable smoke producing material located v'vithin said groove, an explosive charge 1n said separable portion designed to be ignited by said inflammable material, and a smoke generator 1n said separable portion for indicating the. moment of the explosion of the separable 1b portion.

Description

K. VO'LLBR. ARTILLERY FROJBCTILE. APPLICATION FILED, APBl, 1912 Patented Oct. 22, 1912.
2 SHEETS-SHEET 1,
K. VLLER. ARTILLERY PROJEGTILB.
APPLICATION PILEDIAPB. 16, 1912.
1,042,176. Patented o@t.22,1912.
2 SHEETS-SHEET 2.
'mix/ENTE R VJITESSE wei/ KARL VLLER, OF DUSSELDRF, GERMANY.
ABTILLERY-PRUJECTILE.
Specication of Letters Patent.
Patented Oct/22, 1912.
Application filed April 16,1212. Serial No. 691,146.
To all whom it ma'y concern: 0
Be it known that l', KARL VLLER, engineer, a subject of the German Emperor, residing at Dusseldorf, 1`2 Scharnhorststrasse, Germany, Yhave invented certain new and useful Improvements in Artillery-Projec tile's; and I do hereby declare the following to be a full, clear, and exact descriptionof the invention, such as will enable others skilled in the art to which it appertains to make and use the same.
An incendiary shell is described in the patent application Ser. No. 484,518 in which a rocket charge is placed in front of the part of .the shell containing the shrapnel bullets, which charge is ignited by the explosion produced by the time or percussion fuse. In
firing at air ships the flames would only be transmitted to the air ship by a projectile of this kind, if it actually hit the target, or at least passed very close to it; otherwise the head which is emitting sparks and flames would have no destructive action on the air ship.
In order to heighten the effect of the shell and more partioularlyt increase the area of its lateral action, the head of the projectile, in front of the shrapnel containing port1on,
vwhich head gives rise to the incendiary effeet, is provided, not only with an inflammable composition, but also with a filling of explosive material, which is alreadyl known i of the explosive material.
in connection with combined high explosive and shrapnel shells. According to the present invention, by constructing the head of the projectile as a grenade as well as providing it with an incendiary composition, the additional result is gained as compared with the invention disclosed by the before noted application for patent, that in consequence of the explosive action of the head of the shell, anair ship will be hit and destroyed by some part ofv the projectile, although it may not be hit by the whole projectile or by the detached head.
A'construction according to the invention is shown in the accompanying drawings, wherein- A Figure 1 is a vertical longitudinal sectional view. Fig. 2 is a cross-section on line 2 2, Fig. l. Fig. 3 is a diagrammatic view Fig. 4 is a diagrammatic view illustrating the flight and explosion. f
The main bodyo of the shell is construct ed as in the before noted application for patent as a shrapnel containing chamber, whose charge will be ignited by the time fuse b at a certain point of the path by means of the priming channels c and d. This causes the shrapnel bullets to be expelled in a'comparatively narrow cone, and the head of the projectile continues its flight, as shown diagrammatically in Fig. 4.
At the rear or inner end of the head Z of the shell is the inflammable composition e, which, as shown in Fig. 2, is pressed into an annular shape and is connected with the channel c by a small cross passage f.' As soon as the shrapnel explodes and the detachable head continues its flight, the inflammable composition e is ignited and burns during the further flight of the head Z of the shell, leaving behind a trail of smoke of predetermined length, by which it is more easily seen and range calculated. In the head besides the incendiary material e there is also the `explosive charge z'. This is detonated as soon as the inflammable material e is burnt away. The fire strikes then through the channel g to the detonator 7L contained in the head of the shell, and explodes this, thereby causing the explosion of the high explosive charge and the disruption of the head. A smoke generator c in the head of the shell serves to make the moment of the explosion of the grenade head more easily observed. l By the detonation of the explosive charge pieces of the head are scattered in all directions and the effective zone of the whole projectileis very large and much more extended, than that of the incendiary material of the above noted ap-v plication for patent.
Having now particularly described and ascertained the nature of my said invention and in what manner the same is to be per-A formed, Iv declare that what I claim is 1. An artillery projectile adapted for firing at airships, comprising, in combination with a shell containing shrapnel, a separable portion, inflammable smoke-producing material extending over a comparatively extended area within the separable portion, and an explosive charge in said separable portion which is designed to be ignited by said inflammable material.
2. An artillery pro'ectlle adapted for firing at airships, comprising, in combination with a shell containingshrapnel, a separable portion having a groove extending substantially around its axis, inlammablesmoketially around lts axis, an inammable smoke producing material located v'vithin said groove, an explosive charge 1n said separable portion designed to be ignited by said inflammable material, and a smoke generator 1n said separable portion for indicating the. moment of the explosion of the separable 1b portion. n
In testimony whereof, I have signed this specification in the presence of two subscrib- 4 ing witnesses.
KARL VLLER.
Witnesses:
PETER N OLFGARTEN. YV. TACK.
US69114612A 1912-04-16 1912-04-16 Artillery-projectile. Expired - Lifetime US1042176A (en)

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US69114612A US1042176A (en) 1912-04-16 1912-04-16 Artillery-projectile.

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US69114612A US1042176A (en) 1912-04-16 1912-04-16 Artillery-projectile.

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Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6279482B1 (en) 1996-07-25 2001-08-28 Trw Inc. Countermeasure apparatus for deploying interceptor elements from a spin stabilized rocket
US20080223246A1 (en) * 2007-03-13 2008-09-18 Dindl Frank J Burping projectile
US8056481B2 (en) * 2007-03-13 2011-11-15 Dindl Frank J Controlled deceleration projectile
US20160258727A1 (en) * 2015-03-02 2016-09-08 Nostromo Holdings, Llc Low collateral damage bi-modal warhead assembly

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6279482B1 (en) 1996-07-25 2001-08-28 Trw Inc. Countermeasure apparatus for deploying interceptor elements from a spin stabilized rocket
US20080223246A1 (en) * 2007-03-13 2008-09-18 Dindl Frank J Burping projectile
US8056481B2 (en) * 2007-03-13 2011-11-15 Dindl Frank J Controlled deceleration projectile
US20160258727A1 (en) * 2015-03-02 2016-09-08 Nostromo Holdings, Llc Low collateral damage bi-modal warhead assembly
US9759533B2 (en) * 2015-03-02 2017-09-12 Nostromo Holdings, Llc Low collateral damage bi-modal warhead assembly

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