EP0293295B1 - Perfectionnements apportés aux projectiles perforants - Google Patents

Perfectionnements apportés aux projectiles perforants Download PDF

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Publication number
EP0293295B1
EP0293295B1 EP88401272A EP88401272A EP0293295B1 EP 0293295 B1 EP0293295 B1 EP 0293295B1 EP 88401272 A EP88401272 A EP 88401272A EP 88401272 A EP88401272 A EP 88401272A EP 0293295 B1 EP0293295 B1 EP 0293295B1
Authority
EP
European Patent Office
Prior art keywords
projectile
auxiliary
explosive
main
bore
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 - Lifetime
Application number
EP88401272A
Other languages
German (de)
English (en)
French (fr)
Other versions
EP0293295A1 (fr
Inventor
Serge Ladriere
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.)
Individual
Original Assignee
Individual
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
Priority to IN388/CAL/88A priority Critical patent/IN168917B/en
Application filed by Individual filed Critical Individual
Priority to AT88401272T priority patent/ATE54364T1/de
Publication of EP0293295A1 publication Critical patent/EP0293295A1/fr
Application granted granted Critical
Publication of EP0293295B1 publication Critical patent/EP0293295B1/fr
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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Classifications

    • 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
    • F42B12/16—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 in combination with an additional projectile or charge, acting successively on the target
    • 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
    • F42B12/44—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 of incendiary type
    • 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
    • F42B12/06—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 hard or heavy core; Kinetic energy penetrators
    • 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

Definitions

  • the invention relates to piercing projectiles comprising, as described in patent FR-A 477 375, a main projectile of the caliber of the weapon and in which is formed at least one axial bore open towards the front, and, housed in said bore, an auxiliary projectile with the caliber of said bore, a propellant charge being disposed between the bottom of this bore and said auxiliary projectile.
  • a triggering device is provided for igniting the propellant charge in order to cause the firing of the auxiliary projectile before or at the time of the impact of the main projectile on its aim.
  • a proximity detonating fuse triggering device is well known (see in particular the patent GB-A 2 110 799).
  • Such piercing projectiles the piercing effect of which is therefore caused, on the one hand by the auxiliary projectile and on the other hand by the main projectile, are known and the invention aims to give them additional destructive properties, in particular by as regards explosive and / or incendiary effects, which are known and which are described in particular in patent FR-A 2 356 906.
  • the main projectile comprises on the one hand at least an explosive and / or incendiary charge located in the main projectile in front of the auxiliary projectile firing thereof, and on the other hand means for firing this explosive and / or incendiary charge designed to fire automatically as soon as the auxiliary projectile has been fired.
  • these means for igniting the explosive and / or incendiary charge are sensitive to the passage of the auxiliary projectile in the axial bore formed in the main projectile.
  • Such firing means can then be constituted by at least one channel connecting the axial bore formed in the main projectile to the explosive and / or incendiary charge.
  • the axial bore may include scratches whose pitch is such that the angular velocity generated on the auxiliary projectile is added to the angular velocity communicated by the main projectile to said auxiliary projectile.
  • securing means to make the auxiliary projectile, before firing, integral in rotation with the main projectile, such securing means may be constituted by a self-tightening conical fitting.
  • This self-locking conical fitting between the auxiliary projectile and the main projectile also plays the role of temporary retention means of the auxiliary projectile in the axial bore and allows an optimization of the setting in speed (axial speed and rotational speed) of the auxiliary projectile during of the firing of the propellant charge.
  • the invention consists, apart from the arrangements just mentioned, of certain arrangements which are preferably used at the same time and which will be more explicitly described below.
  • a triggering device is provided for igniting the propellant charge 4 in order to cause the firing of the auxiliary projectile 3 before or at the time of the impact of the main projectile 1 on its goal.
  • the aforesaid rear shoe 7 and the aforesaid front cover 8 are connected to each other at a junction plane P, the outside diameter of the projectile being Ion the invention at this junction plane P being less than the outer diameter of the rear shoe 7 at its annular bulge area 7b and the outer diameter of the front cap 8 at its annular bulge area 8b, and this in such proportions that the hollow connecting the two aforesaid annular bulging zones is not in contact with the barrel by which the projectile according to the invention is fired.
  • the axial bore 2 of such a projectile is therefore formed in the central core 6 which has at its front a mouth 9 covered by the tip 10 of the front cap 8 which, at this mouth 9, has a small thickness.
  • the main projectile 1 comprises one or preferably several explosive and / or incendiary charges 11 located in the main projectile 1, in front of the auxiliary projectile 3 before firing, means for igniting this explosive and / or incendiary charge 11 generally designated by the reference numeral 12 being provided and arranged to fire automatically as soon as the auxiliary projectile 3 has been drawn.
  • recesses 13 are regularly spaced circumferentially, and formed in the central core 6, each of these recesses 13 containing an explosive and / or incendiary substance and being closed by the inner wall of the front cover 8.
  • the means 12 for firing these explosive and / or incendiary charges 11 are advantageously produced so as to be sensitive to the passage of the auxiliary projectile 3 in the bore 2.
  • At least one channel 14 is provided connecting the axial bore 2 to each explosive and / or incendiary charge 11 housed in its housing 13.
  • the firing of the propellant charge 4 causes the auxiliary projectile 3 to fire and, as soon as this auxiliary projectile 3 has passed the outlet of the channels 14 in the bore 2, the hot gases penetrate the channels 14 and ignite the Explosive and / or incendiary charges housed in the accommodation 13.
  • the axial bore 2 may include scratches 15 whose pitch is such that the angular speed generated on the auxiliary projectile 3 is added to the angular speed communicated by the main projectile 1 to said auxiliary projectile 3.
  • securing means to make the auxiliary projectile 3, before firing, integral in rotation with the central core 6 of the main projectile 1; such means are formed by self-locking conical engagement 16 between the rear part of the auxiliary projectile 3 and the bottom of the axial bore 2 and formed in the central core 6.
  • This self-locking conical engagement 16 between the auxiliary projectile 3 and the central core 6 also plays the role of temporary retaining means of the auxiliary projectile 3 in the axial bore 2 and allows an optimization of the speed setting (axial speed and rotational speed ) of the auxiliary projectile 3 when the propellant charge is fired.
  • a projectile in accordance with the invention can be produced in all calibers.
  • any caliber less than the 12.7 mm (.50) caliber, without being excluded from the field of application of the invention can be ruled out at least in the first stage.
  • the architecture of the projectile according to the invention could be designed more freely given the dimensions that it would then be possible to give to the constituents of the projectile.
EP88401272A 1987-05-27 1988-05-25 Perfectionnements apportés aux projectiles perforants Expired - Lifetime EP0293295B1 (fr)

Priority Applications (2)

Application Number Priority Date Filing Date Title
IN388/CAL/88A IN168917B (zh) 1987-05-27 1988-05-13
AT88401272T ATE54364T1 (de) 1987-05-27 1988-05-25 Durchdringendes geschoss.

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR8707487 1987-05-27
FR8707487A FR2615937B1 (fr) 1987-05-27 1987-05-27 Perfectionnements apportes aux projectiles perforants

Publications (2)

Publication Number Publication Date
EP0293295A1 EP0293295A1 (fr) 1988-11-30
EP0293295B1 true EP0293295B1 (fr) 1990-07-04

Family

ID=9351523

Family Applications (1)

Application Number Title Priority Date Filing Date
EP88401272A Expired - Lifetime EP0293295B1 (fr) 1987-05-27 1988-05-25 Perfectionnements apportés aux projectiles perforants

Country Status (16)

Country Link
US (1) US4932326A (zh)
EP (1) EP0293295B1 (zh)
JP (1) JPH0672759B2 (zh)
KR (1) KR890701982A (zh)
CN (1) CN1019143B (zh)
AU (1) AU596749B2 (zh)
BR (1) BR8807074A (zh)
CA (1) CA1311150C (zh)
DE (1) DE3860293D1 (zh)
DK (1) DK164527C (zh)
ES (1) ES2015612B3 (zh)
FI (1) FI890357A0 (zh)
FR (1) FR2615937B1 (zh)
GR (1) GR3000624T3 (zh)
OA (1) OA08977A (zh)
WO (1) WO1988009477A1 (zh)

Families Citing this family (25)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE19535218C1 (de) * 1995-09-22 1997-02-27 Diehl Gmbh & Co Ballistisches Geschoß
DE19600167C1 (de) * 1996-01-04 2003-07-17 Diehl Stiftung & Co Penetrator
US6408762B1 (en) 1997-12-11 2002-06-25 Lockheed Martin Corporation Clamp assembly for shrouded aerial bomb
DK1038152T3 (da) * 1997-12-11 2004-12-13 Lockheed Corp Beklædt flyvemaskinebombe
US6389977B1 (en) 1997-12-11 2002-05-21 Lockheed Martin Corporation Shrouded aerial bomb
US6105505A (en) * 1998-06-17 2000-08-22 Lockheed Martin Corporation Hard target incendiary projectile
US6374744B1 (en) 2000-05-25 2002-04-23 Lockheed Martin Corporation Shrouded bomb
ES2190317B1 (es) * 2000-11-22 2004-11-16 Candelaria Codoñer Gomez Proyectil mejorado contra dobles blindajes.
US8661980B1 (en) 2003-05-08 2014-03-04 Lone Star Ip Holdings, Lp Weapon and weapon system employing the same
US7530315B2 (en) 2003-05-08 2009-05-12 Lone Star Ip Holdings, Lp Weapon and weapon system employing the same
FR2871226B1 (fr) * 2004-06-08 2006-08-18 Tda Armements Sas Soc Par Acti Projectile, notamment bombe de penetration anti- infrastructure et procede de penetration d'un tel projectile a travers une paroi
US7690304B2 (en) 2005-09-30 2010-04-06 Lone Star Ip Holdings, Lp Small smart weapon and weapon system employing the same
US7895946B2 (en) 2005-09-30 2011-03-01 Lone Star Ip Holdings, Lp Small smart weapon and weapon system employing the same
US8541724B2 (en) 2006-09-29 2013-09-24 Lone Star Ip Holdings, Lp Small smart weapon and weapon system employing the same
US8117955B2 (en) 2006-10-26 2012-02-21 Lone Star Ip Holdings, Lp Weapon interface system and delivery platform employing the same
SE533168C2 (sv) * 2008-06-11 2010-07-13 Norma Prec Ab Projektil för skjutvapen
US9068803B2 (en) 2011-04-19 2015-06-30 Lone Star Ip Holdings, Lp Weapon and weapon system employing the same
CN102654470A (zh) * 2012-04-19 2012-09-05 江苏亚洲气体设备有限公司 一种热导式动态参比气气体分析仪
PL220109B1 (pl) * 2012-05-07 2015-08-31 Jan Olszewski Pocisk kulowy do broni o lufie gwintowanej
US9389052B2 (en) * 2013-09-18 2016-07-12 The United States Of America As Represented By The Secretary Of The Army Jacketed bullet
KR102548318B1 (ko) * 2017-05-30 2023-06-28 테크벤쳐 인베스트먼트스 피티와이 엘티디 단일 밀봉형 발사체
WO2019048914A1 (de) * 2017-09-09 2019-03-14 Ruag Ammotec Ag Vollmantel-sicherheitsgeschoss, insbesondere für mehrzweckanwendungen
CN110906806A (zh) * 2019-11-17 2020-03-24 长沙深蓝未来智能技术有限公司 外弹道末段底爆增速侵彻穿甲弹
US11573068B1 (en) * 2020-06-19 2023-02-07 The United States Of America As Represented By The Secretary Of The Army Payload protection and deployment mechanism
US11867487B1 (en) * 2021-03-03 2024-01-09 Wach Llc System and method for aeronautical stabilization

Family Cites Families (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR477375A (zh) * 1900-01-01
FR494445A (zh) * 1917-01-16
FR864439A (fr) * 1939-12-12 1941-04-26 Obus à balles multiples dirigées
FR917369A (fr) * 1945-11-14 1947-01-06 Dispositif spécial de lancement des projectiles d'arme à feu
LU44772A1 (zh) * 1963-11-07 1965-05-07
US3418878A (en) * 1967-06-02 1968-12-31 James A. Stricklin Method and means for augmenting hypervelocity flight
FR2202585A5 (zh) * 1972-10-10 1974-05-03 France Etat
DE2439304C2 (de) * 1974-08-16 1986-02-27 Mauser-Werke Oberndorf Gmbh, 7238 Oberndorf Brandgeschoß, insbesondere panzerbrechendes Geschoß
JPS51113400A (en) * 1975-03-31 1976-10-06 Tech Res & Dev Inst Of Japan Def Agency Armored plate shooting bullet
NO137297C (no) * 1976-07-01 1978-02-01 Raufoss Ammunisjonsfabrikker Prosjektil.
DE2948542A1 (de) * 1979-12-03 1984-04-12 Rheinmetall GmbH, 4000 Düsseldorf Geschoss zum bekaempfen mehrlagiger, vorzugsweise aktiver panzerungen
US4648323A (en) * 1980-03-06 1987-03-10 Northrop Corporation Fragmentation munition
PT77697B (fr) * 1982-11-24 1986-02-12 Ladriere Serge Projectile perfectionne destine a etre decharge par des armes a feu
US4648324A (en) * 1985-10-01 1987-03-10 Olin Corporation Projectile with enhanced target penetrating power

Also Published As

Publication number Publication date
EP0293295A1 (fr) 1988-11-30
KR890701982A (ko) 1989-12-22
GR3000624T3 (en) 1991-09-27
FI890357A (fi) 1989-01-25
DK33489A (da) 1989-01-26
OA08977A (fr) 1990-11-30
DE3860293D1 (de) 1990-08-09
JPH0672759B2 (ja) 1994-09-14
CA1311150C (en) 1992-12-08
DK164527C (da) 1992-11-23
AU596749B2 (en) 1990-05-10
CN1019143B (zh) 1992-11-18
FR2615937B1 (fr) 1989-09-08
BR8807074A (pt) 1989-10-31
CN1038157A (zh) 1989-12-20
DK164527B (da) 1992-07-06
FR2615937A1 (fr) 1988-12-02
FI890357A0 (fi) 1989-01-25
DK33489D0 (da) 1989-01-26
AU1943688A (en) 1988-12-21
ES2015612B3 (es) 1990-09-01
US4932326A (en) 1990-06-12
JPH01503402A (ja) 1989-11-16
WO1988009477A1 (fr) 1988-12-01

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