EP0143084A2 - Illuminating mixture for illuminating canisters intended to be inserted in artillery projectiles - Google Patents

Illuminating mixture for illuminating canisters intended to be inserted in artillery projectiles Download PDF

Info

Publication number
EP0143084A2
EP0143084A2 EP84830255A EP84830255A EP0143084A2 EP 0143084 A2 EP0143084 A2 EP 0143084A2 EP 84830255 A EP84830255 A EP 84830255A EP 84830255 A EP84830255 A EP 84830255A EP 0143084 A2 EP0143084 A2 EP 0143084A2
Authority
EP
European Patent Office
Prior art keywords
illuminating
mixture
canister
blowing agent
canisters
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.)
Withdrawn
Application number
EP84830255A
Other languages
German (de)
French (fr)
Other versions
EP0143084A3 (en
Inventor
Eugenio Dr. Dall'orto
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.)
Simmel SpA
Original Assignee
Simmel SpA
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 Simmel SpA filed Critical Simmel SpA
Publication of EP0143084A2 publication Critical patent/EP0143084A2/en
Publication of EP0143084A3 publication Critical patent/EP0143084A3/en
Withdrawn legal-status Critical Current

Links

Images

Classifications

    • CCHEMISTRY; METALLURGY
    • C06EXPLOSIVES; MATCHES
    • C06CDETONATING OR PRIMING DEVICES; FUSES; CHEMICAL LIGHTERS; PYROPHORIC COMPOSITIONS
    • C06C15/00Pyrophoric compositions; Flints
    • CCHEMISTRY; METALLURGY
    • C06EXPLOSIVES; MATCHES
    • C06BEXPLOSIVES OR THERMIC COMPOSITIONS; MANUFACTURE THEREOF; USE OF SINGLE SUBSTANCES AS EXPLOSIVES
    • C06B23/00Compositions characterised by non-explosive or non-thermic constituents
    • C06B23/009Wetting agents, hydrophobing agents, dehydrating agents, antistatic additives, viscosity improvers, antiagglomerating agents, grinding agents and other additives for working up

Definitions

  • illuminating canisters to be inserted in artillery projectiles which, once the projecti le has been fired and has reached a predetermined point of its trajectory, are ejected by the use of a suitable explosive charge, which generally has also the purpose of igniting the illuminating mixture con tained in the canister. After the ejection from the projectile the canister descends suspended to a parachute so as to illuminate a surrounding area for a predetermined time depending on its dimensions and the combustion velocity of the illuminating mixture.
  • the prior art illuminating mixtures consist substantially of a metal powder acting as a combustible, an oxidizer acting as a supporter of combustion, and a binder. These mistures are charged in a suitable manner, f.e. by compression or pouring, in a container of a suitable shape and mechanical strength so as to form the so called illuminating canister.
  • the obstruction of the canister mouth reduces the emission surface whereby a decrease of the luminous intensity of the device occurs.
  • an increase of the pressure of the gases inside the canister takes place with a resultant increase of the combustion velocity and as a result a shorter illumination time and the risk that the canister explodes.
  • the ashes by depositing on the underlying mixture cover it so as to prevent its ignition whereby at the end of the combustion a lot of unburnt mixture remains in the canister.
  • the illuminating mixture according to the invention for illuminating canisters intended to be inserted in an artillery projectile is characterized in that it comprises an expander of the type of the blowing agents normally used in the technology of plastics.
  • the expander is simply added in the mixing step of the compounds intended to form the illuminating mixture.
  • Typical classes of compounds usable to this purpose are azo-derivatives such as azo-dicarbonamide or azodiisobutyronitrile (2:2'-azodi-2-methylpropionitrile); sulphonhydrazide-derivatives, such as benzen-m-di- sulphonhydrazide; N-nitroso-derivatives such as N, N' dimethyl-N, N'-dinitroso-terephthalirqide or N, N'-di- nitroso-pentamethylen-tetramine; or other compounds, such as tris-hydrazin-triazin or nitrourea.
  • azo-derivatives such as azo-dicarbonamide or azodiisobutyronitrile (2:2'-azodi-2-methylpropionitrile)
  • sulphonhydrazide-derivatives such as benzen-m-di- sulphonhydrazide
  • Figs. 1 and 2 of the accompanying drawings there are illustrated the graphs of the luminous intensity v. time of two equal compositions including magnesium powder, sodium nitrate and epoxy resin as a binder.
  • the composition is without expander, while in Fig. 2 3% weight of azo-dicarbonamide has been added. It is apparent the improvement obtained in the performance which is due to a substantial reduction in the quanity of ash accumulated in the canister.

Landscapes

  • Chemical & Material Sciences (AREA)
  • Organic Chemistry (AREA)
  • Engineering & Computer Science (AREA)
  • Metallurgy (AREA)
  • Non-Portable Lighting Devices Or Systems Thereof (AREA)

Abstract

The illuminating mixture for illuminating canisters intended to be inserted in an artillery projectile comprises an expander of the type of the blowing agents used in the technology of plastics. In this way it is prevented that the ashes accumulate and become compact during the combustion of the illuminating mixture and thus the ejection of the ashes from the canister is facilitated.

Description

  • The present invention relates to illuminating mixtures for illuminating canisters intended to be inserted in an artillery projectile.
  • There are known illuminating canisters to be inserted in artillery projectiles which, once the projecti le has been fired and has reached a predetermined point of its trajectory, are ejected by the use of a suitable explosive charge, which generally has also the purpose of igniting the illuminating mixture con tained in the canister. After the ejection from the projectile the canister descends suspended to a parachute so as to illuminate a surrounding area for a predetermined time depending on its dimensions and the combustion velocity of the illuminating mixture.
  • The prior art illuminating mixtures consist substantially of a metal powder acting as a combustible, an oxidizer acting as a supporter of combustion, and a binder. These mistures are charged in a suitable manner, f.e. by compression or pouring, in a container of a suitable shape and mechanical strength so as to form the so called illuminating canister.
  • One of the major disadvantages which occurs in the course of the combustion consists of the accumulation of ashes along the walls and the mouth of the canister. This phenomenon is much enhanced in the case of projectiles fired by rifled firearms which undergo a spin which can reach speedsup to 18000 r.p.m. In fact, in this case, if the canister is not provided with a sui table aerodynamic braking device, it retains the spin moment it had at the ejection and because of the centrifugal force the ashes are thrown against the walls on which they accumulate and form a hard and compact layer which tends to obstruct the canister mouth.
  • This fact is dangerous for various reasons. Firstly, the obstruction of the canister mouth reduces the emission surface whereby a decrease of the luminous intensity of the device occurs. Secondly, because of the obstruction an increase of the pressure of the gases inside the canister takes place with a resultant increase of the combustion velocity and as a result a shorter illumination time and the risk that the canister explodes. Thirdly, the ashes by depositing on the underlying mixture cover it so as to prevent its ignition whereby at the end of the combustion a lot of unburnt mixture remains in the canister.
  • As stated hereinbefore, in order to attenuate this phenomenon aerodynamic brakes have been provided on the canister which slow down its spin. This method has proved effective but is expensive inasmuch as it involves further manufacturing steps and, in addition, a space is taken up which is necessarily no longer available for the useful load.
  • It is the object of the present invention to elimina te or at least substantially reduce the above mentioned disadvantages of the prior art canisters by acting in a simple and practical manner only on the chemical composition of the illuminating mixture without altering the conventional conformation of the canister and/or the structure of the illuminating body.
  • More particularly, the illuminating mixture according to the invention for illuminating canisters intended to be inserted in an artillery projectile is characterized in that it comprises an expander of the type of the blowing agents normally used in the technology of plastics.
  • The expander is simply added in the mixing step of the compounds intended to form the illuminating mixture.
  • Typical classes of compounds usable to this purpose are azo-derivatives such as azo-dicarbonamide or azodiisobutyronitrile (2:2'-azodi-2-methylpropionitrile); sulphonhydrazide-derivatives, such as benzen-m-di- sulphonhydrazide; N-nitroso-derivatives such as N, N' dimethyl-N, N'-dinitroso-terephthalirqide or N, N'-di- nitroso-pentamethylen-tetramine; or other compounds, such as tris-hydrazin-triazin or nitrourea.
  • These compounds are characterized in that they decompose at a well defined temperature and generate a quan- tity of gas which depends on their chemical formula. The gas developed generates a pressure inside the illuminating mixture downstream the combustion front, along a section in which said mixture has reached, because of the thermal conduction, a temperature equal to or higher than that of the decomposition point of the expander. As a result, at the time of combustion said gas under pressure expands instantaneously, up to the ambient pressure, in the ashes, and causes their disintegration. In this way it is prevented that the ashes accumulate and become compact and it is facilitated their ejection which is further aided by the circumstance that the canister burns with its mouth turned downwards.
  • The choice of the expander and the quantity to be used are no problem for those skilled in the art; however the length of the section whose temperature is higher than that of the point of decomposition of the expander as well as the compatibility with the other compounds of the illuminating mixture must be carefully estimated.
  • As an example, in Figs. 1 and 2 of the accompanying drawings there are illustrated the graphs of the luminous intensity v. time of two equal compositions including magnesium powder, sodium nitrate and epoxy resin as a binder. In Fig. 1 the composition is without expander, while in Fig. 2 3% weight of azo-dicarbonamide has been added. It is apparent the improvement obtained in the performance which is due to a substantial reduction in the quanity of ash accumulated in the canister.

Claims (7)

1. Illuminating mixture for illuminating canisters intended to be inserted in an artillery projectile, cha- racterized in that it comprises an expander of the type of the blowing agents normally used in the technology of plastics.
2. Illumination mixture as claimed in claim 1, characterized in that the blowing agent is an azo-deri vative.
3. Illuminating mixture as claimed in claim 1, characterized in that the blowing agent is a sulphonhydrazide-derivative.
4. Illuminating mixture as claimed in claim 1, characterized in that the blowing agent is a N-nitroso- derivative.
5. Illuminating mixture as claimed in claim 1, characterized in that the blowing agent is tris-hydrozin- triazine.
6. Illuminating mixture as claimed in claim 1, characterized in that the blowing agent is nitrourea.
7. Illuminating mixture as claimed in claim 2, characterized in that the azo-derivative blowing agent is azo-dicarbonamide.
EP84830255A 1983-11-18 1984-09-17 Illuminating mixture for illuminating canisters intended to be inserted in artillery projectiles Withdrawn EP0143084A3 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
IT23768/83A IT1166989B (en) 1983-11-18 1983-11-18 ILLUMINATING MIXTURE FOR ILLUMINATING CANISTERS INTENDED TO BE INSERTED IN ARTILLERY BULLETS
IT2376883 1983-11-18

Publications (2)

Publication Number Publication Date
EP0143084A2 true EP0143084A2 (en) 1985-05-29
EP0143084A3 EP0143084A3 (en) 1985-07-03

Family

ID=11209813

Family Applications (1)

Application Number Title Priority Date Filing Date
EP84830255A Withdrawn EP0143084A3 (en) 1983-11-18 1984-09-17 Illuminating mixture for illuminating canisters intended to be inserted in artillery projectiles

Country Status (2)

Country Link
EP (1) EP0143084A3 (en)
IT (1) IT1166989B (en)

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3986907A (en) * 1975-03-07 1976-10-19 Thiokol Corporation Illuminating flare composition containing tetranitrocarbazole
FR2316204A1 (en) * 1975-07-03 1977-01-28 Poudres & Explosifs Ste Nale A LIGHTING PYROTECHNICAL COMPOSITION GENERATING GAS
FR2332966A1 (en) * 1975-11-28 1977-06-24 Poudres & Explosifs Ste Nale Porous powders, esp. of nitrocellulose - obtd. by addn. of porogenic agents and leaching out with water esp. useful in prepn. of more active gun powders
GB1500679A (en) * 1964-09-18 1978-02-08 Dynamit Nobel Ag Hybrid rocket fuels

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1500679A (en) * 1964-09-18 1978-02-08 Dynamit Nobel Ag Hybrid rocket fuels
US3986907A (en) * 1975-03-07 1976-10-19 Thiokol Corporation Illuminating flare composition containing tetranitrocarbazole
FR2316204A1 (en) * 1975-07-03 1977-01-28 Poudres & Explosifs Ste Nale A LIGHTING PYROTECHNICAL COMPOSITION GENERATING GAS
FR2332966A1 (en) * 1975-11-28 1977-06-24 Poudres & Explosifs Ste Nale Porous powders, esp. of nitrocellulose - obtd. by addn. of porogenic agents and leaching out with water esp. useful in prepn. of more active gun powders

Also Published As

Publication number Publication date
EP0143084A3 (en) 1985-07-03
IT8323768A1 (en) 1985-05-18
IT1166989B (en) 1987-05-06
IT8323768A0 (en) 1983-11-18

Similar Documents

Publication Publication Date Title
US3865035A (en) Multi-use munition
US4237787A (en) Incendiary projectile
US6257146B1 (en) Noise making projectile
US3771451A (en) Low pressure ballistic system
US2445312A (en) Incendiary bomb mixture
US4130061A (en) Gun fired projectile having reduced drag
ATE80221T1 (en) SMOKING PROJECTILE AND AMMUNITION CONTAINING SUCH PROJECTILE.
GB1517630A (en) Projectile
ES548171A0 (en) DEVICE TO REDUCE AERODYNAMIC RESISTANCE OF AMMUNITIONS SUCH AS ARTILLERY PROJECTILES.
JPH01164789A (en) Signal projictile composition and signal projectile containing this composition
US4438700A (en) White smoke spotting composition for training ammunition
US3750585A (en) Tracer projectiles
US3942443A (en) Rocket assisted projectile
EP0143084A2 (en) Illuminating mixture for illuminating canisters intended to be inserted in artillery projectiles
US3754511A (en) Fuel and fuel igniter for ram jet and rocket
US3959041A (en) Illumination and incendiary composition for explosive munitions
US4402705A (en) Incendiary composition containing a group IVB metallic fuel
US2476370A (en) Electric initiator device and ignition composition
US3667391A (en) Detonator and igniter for explosives
US2363863A (en) Priming composition
US4015529A (en) Illuminative and incendiary explosive munitions
EP1166033B1 (en) Electronically and mechanically-operated ignition delay for cartridge-type pyrotechnic decoy flare ammunition
US2359777A (en) Fuse
GB2218414A (en) High-duty smoke-producing bodies and projectile
US1025500A (en) Projectile for firing at airships.

Legal Events

Date Code Title Description
PUAI Public reference made under article 153(3) epc to a published international application that has entered the european phase

Free format text: ORIGINAL CODE: 0009012

PUAL Search report despatched

Free format text: ORIGINAL CODE: 0009013

AK Designated contracting states

Designated state(s): AT BE CH DE FR GB LI LU NL SE

AK Designated contracting states

Designated state(s): AT BE CH DE FR GB LI LU NL SE

17P Request for examination filed

Effective date: 19850907

17Q First examination report despatched

Effective date: 19860924

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: THE APPLICATION IS DEEMED TO BE WITHDRAWN

18D Application deemed to be withdrawn

Effective date: 19870205

RIN1 Information on inventor provided before grant (corrected)

Inventor name: DALL'ORTO, EUGENIO, DR.