FI59873B - MOERSARENS PROJEKTIL - Google Patents
MOERSARENS PROJEKTIL Download PDFInfo
- Publication number
- FI59873B FI59873B FI760872A FI760872A FI59873B FI 59873 B FI59873 B FI 59873B FI 760872 A FI760872 A FI 760872A FI 760872 A FI760872 A FI 760872A FI 59873 B FI59873 B FI 59873B
- Authority
- FI
- Finland
- Prior art keywords
- projectile
- mortar
- pivoted
- timing device
- stern
- Prior art date
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B10/00—Means for influencing, e.g. improving, the aerodynamic properties of projectiles or missiles; Arrangements on projectiles or missiles for stabilising, steering, range-reducing, range-increasing or fall-retarding
- F42B10/60—Steering arrangements
- F42B10/62—Steering by movement of flight surfaces
- F42B10/64—Steering by movement of flight surfaces of fins
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B12/00—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material
- F42B12/02—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect
- F42B12/04—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect of armour-piercing type
- F42B12/10—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect of armour-piercing type with shaped or hollow charge
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B12/00—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material
- F42B12/02—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect
- F42B12/36—Projectiles, 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
- F42B12/56—Projectiles, 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 for dispensing discrete solid bodies
- F42B12/58—Cluster or cargo ammunition, i.e. projectiles containing one or more submissiles
- F42B12/62—Cluster or cargo ammunition, i.e. projectiles containing one or more submissiles the submissiles being ejected parallel to the longitudinal axis of the projectile
- F42B12/625—Cluster or cargo ammunition, i.e. projectiles containing one or more submissiles the submissiles being ejected parallel to the longitudinal axis of the projectile a single submissile arranged in a carrier missile for being launched or accelerated coaxially; Coaxial tandem arrangement of missiles which are active in the target one after the other
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
- Toys (AREA)
Description
|·«Ι»Τ·| ΓΒ] 01ϊ KUULUTUSjULKAISU Γ Q Q n 7 lJ ( } UTLÄGGN I NGSSKRIFT 5)9873 c (4S) /. "j t y 10 ;’J1 ^ (51) Kv.ik?/int.ci.3 F 42 B 13/30 SUOM I—FI N LAN D (21) Pat«nttlh»k»mui-P»t«ntiMei(nlng Τ6θδΤ2 (22) Hik*ml«piiv* — Aniöknlngsdag 01.0^.76 (23) Alkupiiv* — Glltighttsdag 01.0U.T6 (41) Tullut julkiseksi — Bllvlt offentllg 27.10.76| · «Ι» · Τ | Q] 01ϊ ANNOUNCEMENT Γ Q Q n 7 lJ (} UTLÄGGN I NGSSKRIFT 5) 9873 c (4S) /. "jty 10; 'J1 ^ (51) Kv.ik? /int.ci.3 F 42 B 13/30 SUOM I — FI N LAN D (21) Pat« nttlh »k» mui-P »t« n « nlng Τ6θδΤ2 (22) Hik * ml «piiv * - Aniöknlngsdag 01.0 ^ .76 (23) Starting line * - Glltighttsdag 01.0U.T6 (41) Has become public - Bllvlt offentllg 27.10.76
Patentteja rekisterihallitus .... .... . .. , . . ., ,. .Patents Registration Board .... ..... ..,. . .,,. .
. (44) NUitlvIkilpsnon |t kuul.julkalsun pvm.— r Q. (44) Date of publication of the NUitlvIkilpsnon | t Q.
Patent· och registerstyrelsen Aniökan utlagd oeh utl.skriften pubiicend 30.06.01 (32)(33)(31) Pyydetty etuoikeus— Begird prloritet 26.OU.75Patent · och registerstyrelsen Aniökan utlagd oeh utl.skriften pubiicend 30.06.01 (32) (33) (31) Requested privilege— Begird prloritet 26.OU.75
Saksan Liittotasavalta-Förbundsrepubliken Tyskland(DE) P 2518593-7 (71) Firma Diehl, Stephanstr. U9, 8500 Nurnberg, Saksan Liittotasavalta-Förbundsrepubliken Tyskland(DE) (72) Max Rentzsch, Röthenbach/Pegn., Erich Bock, Niimberg, Saksan Liitto-tasavalta-Förbundsrepubliken Tyskland(DE) (7U) Leitzinger Oy (5U) Mörssarin ammus - Morsarens projektilFederal Republic of Germany-Förbundsrepubliken Tyskland (DE) P 2518593-7 (71) Firma Diehl, Stephanstr. U9, 8500 Nurnberg, Federal Republic of Germany-Förbundsrepubliken Tyskland (DE) (72) Max Rentzsch, Röthenbach / Pegn., Erich Bock, Niimberg, Federal Republic of Germany-Förbundsrepubliken Tyskland (DE) (7U) Leitzinger Oy (5U) Mörssarin Morsarens project
Keksinnön kohteena on mörssärin ammus, jossa on rungon sisään sovitettu taistelupanos ja ajopanokset sekä sytytyslaitteen vastaanottava pyrstötuki.The invention relates to a mortar's projectile having a combat charge and propulsion cartridges arranged inside the hull and a tail support receiving the igniter.
Saksalaisesta kuulutusjulkaisusta 1 703 781 tunnetaan panssarintorjuntaan tarkoitettu mörssärin ammus, joka sisältää useita itsenäisiä ontelopanosammuksia ja on varustettu ulostyöntölaitteella ontelopa-nosammuksia varten ja aikasytyttimellä. Kohdetilassa määrätyllä korkeudella tulevat erillispanokset työnnetyksi ulos suhteellisen pienelle hajonta-alueelle. Tällainen panssarintorjuntatekniikka ei ole kovin tehokas johtuen epävarmasta osumistodennäköisyydestä ja sen aiheuttamasta suuresta ampumatarvikkeiden kulutuksesta sekä yhden tällaisen ontelopanosammuksen suhteellisen pienestä vaikutuksesta panssariin. Korkea osumistodennäköisyys vaatii mörssärin ammuksille ominaisen hajonnan johdosta useampia mörssärin ammuksia maalia kohti.German Offenlegungsschrift No. 1,703,781 discloses a mortar projectile for anti-tank armor, which contains a plurality of independent cavity projectile shells and is equipped with an ejection device for cavity cavity fire extinguishers and a time igniter. At a certain height in the target space, the individual cartridges are pushed out into a relatively small scattering area. Such anti-tank technology is not very effective due to the uncertain probability of impact and the resulting high consumption of ammunition, as well as the relatively small impact of one such cavity charge extinguish on the armor. The high probability of a hit requires more mortar ammunition per target due to the scattering characteristic of mortar ammunition.
US-patenttijulkaisusta 3 041 011 tunnetaan 'rakettiammus, jonka suip-pokärkeen on järjestetty etsinjärjestelmä, joka vaikuttaa pyrstöoh-jauslaitteeseen . Pyrstöohjauslaite on yhdistetty vakainsiipiin.U.S. Pat. No. 3,041,011 discloses a rocket ammunition having a viewfinder system arranged at the tip of the tip that acts on the tail guide device. The tail guide is connected to the stabilizing wing.
Saksalaisesta hakemus julkaisusta 1 950 638 ovat tunnettuja lentokap- 59873 2 paleen käyttölaitteeseen yhdistetyt, ulos käännettävät vakainsii-vekkeet.German application publication 1 950 638 discloses fold-out stabilizing wings connected to an airframe 59873 2-piece actuator.
Keksinnön tarkoituksena on saada aikaan sellainen mörssärin ammus, että osumistodennäköisyys verrattuna saksalaisesta kuulutusjulkaisusta 1 703 781 tunnettuun mörssärin ammukseen olennaisesti lisääntyy. Tämä tarkoitus saavutetaan patenttivaatimuksen 1 tunnusmerkki-osassa esitetyillä tunnusmerkeillä, jolloin patenttisuoja koskee annettujen tunnusmerkkien yhdistelmää.The object of the invention is to provide such a mortar projectile that the probability of impact is substantially increased in comparison with the mortar projectile known from the German publication 1 703 781. This object is achieved by the features set forth in the characterizing part of claim 1, wherein the patent protection relates to a combination of the given features.
Keksinnöllä saavutetaan se, että mörssärin ammus voidaan vakainsii-pien ollessa sisäänkäännettynä ampua tavanomaisesta mörssäristä (= suurikaliiperinen, vain kaariammuntaan soveltuva tykki), samalla kun lentoaika tasaa ympäristövaikutukset kuten erilaiset ilmanvirtaukset, sekä maalin liikkumisen, ja itseohjautunut mörssärin ammus - vaikuttaa maaliin sen runkoon järjestetyllä suurikaliiperisella on-telopanoksella välittömästi vaikuttavana taistelupanoksena.The invention achieves that a mortar projectile can be fired from a conventional mortar (= a large-caliber cannon suitable for archery only) when the vanes are inverted, while the flight time compensates for environmental effects such as different air currents, as well as on-telo bet as an immediate effective combat bet.
Lisäksi on vakainsiipien uloskääntämiseen saakka ballistisena kulkevan mörssärin ammuksen lentoradan perusteella mörssärin paikantaminen vastustajan puolelta vaikeutunut. Vakainsiipien uloskääntämisen jälkeen on mörssärin ammus nopeasti ja tehokkaasti ohjailtavissa suunnilleen painopisteen kohdalle järjestettyjen vakainsiipien ympäri. Seuraavassa selostetaan keksinnön erästä suoritusesimerkkiä viittaamalla oheisiin piirustuksiin, joissa kuvio 1 esittää mörssärinammusta maalilennossa.In addition, based on the flight path of the ballistic projectile projectile, which extends as a ballistic projector, it is more difficult to locate the mortal on the opponent's side. After the stabilizing wings are folded out, the mortar's projectile can be guided quickly and efficiently around the stabilizing wings arranged approximately at the center of gravity. An embodiment of the invention will now be described with reference to the accompanying drawings, in which Figure 1 shows mortar munitions in a target flight.
Kuvio 2 esittää kuvion 1 mukaisen mörssärinammuksen rakennetta.Figure 2 shows the structure of the mortar projectile according to Figure 1.
Kuvion 2 mukaan mörssärsinammuksen 1 muodostaa useat kotelonosat 2-7 ja pyrsöputki 8 siihen sovitettuine ajopanoksineen 9 ja kään-nettävine peräsimineen 10.According to Figure 2, the mortar projectile 1 is formed by a plurality of housing parts 2-7 and a tailpipe 8 with drive cartridges 9 and a reversible rudder 10 fitted thereon.
Suippokärjen muotoiseen kotelonosaan 2 on sovitettu etsinjärjestelmä 11. Tähän liittyvät iskukytkin 12 elektronisine aikalaitteineen 13, energiakappale 14 ja pyrotekniUinen moottori 15 kotelonosan 5 sisään-käännettyjen vakainsiipien 16 uloskääntamiseksi. Vakainsiipien 16 välissä kotelonosassa 5 on toistensa alapuolelle yhdistetyt elektroniset ohjauskappaleet 17.A viewfinder system 11 is arranged in the tapered housing-shaped housing part 2. Associated with this are an impact switch 12 with electronic timing devices 13, an energy piece 14 and a pyrotechnic motor 15 for unfolding the inverted stabilizing wings 16 of the housing part 5. Between the stabilizing wings 16, the housing part 5 has electronic control pieces 17 connected below each other.
3 598733 59873
Teräsputki 18 kotelonosaan 6 sovitettua ontelopanosta 19 varten on kiinnitetty keskeisesti kahteen kotelon levyyn 20, 21. Ontelopanok-sessa 19 on metallisuppilo 22, sirpaleita muodostava vaippa 23 ja sytytyspanos 24.The steel tube 18 for the cavity cartridge 19 fitted to the housing part 6 is fixed centrally to the two housing plates 20, 21. The cavity cartridge 19 has a metal funnel 22, a fragment-forming jacket 23 and an ignition cartridge 24.
Kotelonosassa 7 on peräsimen moottori 25 merkintälähettimineen 26, ohjaustangosto 27 ja sytytyslaite 28 käyttölatauksia 9 varten. Peräsimet 10 ovat tunnettuun tapaan jousivoimaa vastaan perusasennossa.The housing part 7 has a rudder motor 25 with a marking transmitter 26, a handlebar 27 and an ignition device 28 for drive charges 9. The rudders 10 are in a known position against the spring force in the basic position.
Välittömästi mörssärin ammuksen 1 ampumisen jälkeen tavallisella mörssärillä tapahtuu jousivoimalla peräsimen 10 asetus. Lentoradan lakipisteen saavuttamisen jälkeen käännetään ennen ampumista säädetyn aikalaitteen 13 ja moottorin 15 välityksellä vakainsiivet 16 ulos. Sen jälkeen käynnistetään aikalaitteen 13 välityksellä ener-giakappale 14, ohjauskappaleet 17, etsinjärjestelmä 11 ja peräsimen asetusmoottori 25.Immediately after firing the mortar's projectile 1 with a normal mortar, the setting of the rudder 10 takes place by spring force. After reaching the orbital point of the flight path, the stabilizing wings 16 are turned out by means of a time device 13 and a motor 15 adjusted before firing. The energy piece 14, the guide pieces 17, the viewfinder system 11 and the rudder setting motor 25 are then started via the time device 13.
Etsinjärjestelmästä lähtevä ohjausmerkki siirretään peräsimen ase-tusmoottorin 25 ja merkintälähettimen 26 välityksellä peräsimiin 10.The control signal from the viewfinder system is transmitted to the rudders 10 via the rudder setting motor 25 and the marking transmitter 26.
Mörssärin ammuksen 1 iskiessä kohteeseen tapahtuu iskukytkimen 12 välityksellä ontelopanoksen sytytys.When the mortar projectile 1 strikes the target, the hollow charge is ignited via the impact switch 12.
Etsinjärjestelmää varten soveltuvat esimerkiksi optiset kuin myös lämpösäteily- tai tutkajärjestelmät.For example, optical as well as thermal radiation or radar systems are suitable for the search system.
Mörssäriä varten järjestetyn ammuksen 1 ohella se on sovitettavissa myöskin kantojärjestelmiä, kuten raketteja varten.In addition to the projectile 1 for mortars, it can also be adapted for launch systems such as rockets.
Claims (3)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE2518593A DE2518593C3 (en) | 1975-04-26 | 1975-04-26 | Mortar projectile |
DE2518593 | 1975-04-26 |
Publications (3)
Publication Number | Publication Date |
---|---|
FI760872A FI760872A (en) | 1976-10-27 |
FI59873B true FI59873B (en) | 1981-06-30 |
FI59873C FI59873C (en) | 1981-10-12 |
Family
ID=5945049
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FI760872A FI59873C (en) | 1975-04-26 | 1976-04-01 | MOERSARENS PROJEKTIL |
Country Status (7)
Country | Link |
---|---|
DE (1) | DE2518593C3 (en) |
DK (1) | DK137817C (en) |
FI (1) | FI59873C (en) |
FR (1) | FR2308903A1 (en) |
IL (1) | IL49443A (en) |
IT (1) | IT1060226B (en) |
NL (1) | NL184295C (en) |
Families Citing this family (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE2904749C2 (en) * | 1979-02-08 | 1984-01-05 | Messerschmitt-Bölkow-Blohm GmbH, 8000 München | Missile in the manner of a drone |
FR2552871B1 (en) * | 1981-04-28 | 1986-11-07 | France Etat Armement | ANTICHAR PROJECTILE ACTING AT SCROLLING SPEED |
SE8106719L (en) * | 1981-11-12 | 1983-05-13 | Foerenade Fabriksverken | PROJECTILE |
EP0091860A1 (en) * | 1982-04-02 | 1983-10-19 | Thomson-Brandt | Armour-piercing hollow charge |
FR2534370B1 (en) * | 1982-10-11 | 1986-12-19 | Luchaire Sa | DEVICE INTENDED FOR ATTACKING OVER OBJECTIVES SUCH AS ESPECIALLY ARMORED |
GB2208017B (en) * | 1983-11-25 | 1989-07-05 | British Aerospace | Guidance systems |
DE3432614A1 (en) * | 1984-09-05 | 1986-03-13 | Rheinmetall GmbH, 4000 Düsseldorf | MISSILE |
FR2587476B1 (en) * | 1985-09-13 | 1989-06-09 | France Etat Armement | VERY SHORT RANGE ANTICHAR PROJECTILE |
DE3606835C2 (en) * | 1986-03-03 | 1997-03-27 | Diehl Gmbh & Co | Steering device for projectiles |
FR2622966B1 (en) * | 1987-11-06 | 1993-05-07 | Thomson Brandt Armements | GYROSCOPIC STABILIZATION DEVICE FOR A PROJECTILE HANDLING MEMBER |
FR2624597B1 (en) * | 1987-12-11 | 1993-05-07 | Thomson Brandt Armements | SUB-PROJECTILE GROUND-TO-AIR GUIDE VECTOR |
-
1975
- 1975-04-26 DE DE2518593A patent/DE2518593C3/en not_active Expired
-
1976
- 1976-03-26 DK DK136076A patent/DK137817C/en not_active IP Right Cessation
- 1976-04-01 FI FI760872A patent/FI59873C/en not_active IP Right Cessation
- 1976-04-05 NL NLAANVRAGE7603512,A patent/NL184295C/en not_active IP Right Cessation
- 1976-04-14 FR FR7610943A patent/FR2308903A1/en active Granted
- 1976-04-19 IL IL49443A patent/IL49443A/en unknown
- 1976-04-22 IT IT22542/76A patent/IT1060226B/en active
Also Published As
Publication number | Publication date |
---|---|
NL184295C (en) | 1989-06-01 |
DK136076A (en) | 1976-10-27 |
NL7603512A (en) | 1976-10-28 |
DK137817C (en) | 1978-10-16 |
IL49443A0 (en) | 1976-08-31 |
FI760872A (en) | 1976-10-27 |
IT1060226B (en) | 1982-07-10 |
DE2518593C3 (en) | 1979-12-06 |
FI59873C (en) | 1981-10-12 |
FR2308903B3 (en) | 1979-07-13 |
NL184295B (en) | 1989-01-02 |
DE2518593A1 (en) | 1976-11-11 |
FR2308903A1 (en) | 1976-11-19 |
DE2518593B2 (en) | 1979-03-29 |
DK137817B (en) | 1978-05-08 |
IL49443A (en) | 1982-12-31 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
MM | Patent lapsed |
Owner name: FIRMA DIEHL |