EP0175914A1 - Projectile pour intercepter des objets en mouvement libre - Google Patents

Projectile pour intercepter des objets en mouvement libre Download PDF

Info

Publication number
EP0175914A1
EP0175914A1 EP85110294A EP85110294A EP0175914A1 EP 0175914 A1 EP0175914 A1 EP 0175914A1 EP 85110294 A EP85110294 A EP 85110294A EP 85110294 A EP85110294 A EP 85110294A EP 0175914 A1 EP0175914 A1 EP 0175914A1
Authority
EP
European Patent Office
Prior art keywords
projectile
sleeve body
shock
sleeve
designed
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Withdrawn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
EP85110294A
Other languages
German (de)
English (en)
Inventor
Heinz Piccolruaz
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.)
Piccolruaz Heinz
Original Assignee
Oerlikon Contraves AG
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 Oerlikon Contraves AG filed Critical Oerlikon Contraves AG
Publication of EP0175914A1 publication Critical patent/EP0175914A1/fr
Withdrawn legal-status Critical Current

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Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41—WEAPONS
    • F41H—ARMOUR; ARMOURED TURRETS; ARMOURED OR ARMED VEHICLES; MEANS OF ATTACK OR DEFENCE, e.g. CAMOUFLAGE, IN GENERAL
    • F41H11/00—Defence installations; Defence devices
    • F41H11/02—Anti-aircraft or anti-guided missile or anti-torpedo defence installations or systems
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41—WEAPONS
    • F41H—ARMOUR; ARMOURED TURRETS; ARMOURED OR ARMED VEHICLES; MEANS OF ATTACK OR DEFENCE, e.g. CAMOUFLAGE, IN GENERAL
    • F41H13/00—Means of attack or defence not otherwise provided for
    • F41H13/0006—Ballistically deployed systems for restraining persons or animals, e.g. ballistically deployed nets

Definitions

  • the invention relates to a projectile with a projectile and deployable element for combating targeted and / or freely moving objects.
  • a towed body is known from US Pat. No. 4,231,311, which is towed by a ship, for example.
  • suitable sensors for detecting torpedoes aimed at the ship, for example in order to achieve a destructive collision and an element arranged in a gathered state, which is ejected from the towed body with suitable means for intercepting the torpedoes and is unfolded and spread out like a parachute.
  • the invention is based, to improve a projectile of the type mentioned in the sense of a variety of uses and for safe and effective combat of targeted shot and / or free-moving objects the task.
  • this object is achieved in that, in order to achieve an intercepting, direction-changing and / or destructive collision of the projectile by a thrust force, it is moved approximately in the direction of the object to be combated and the element is ejected from the sleeve body at a specific distance from the object in such a way that the shock-absorbing organs with the sleeve body or the individual sleeve body parts, the element that is operatively connected is deployed over a large area.
  • a projectile is understood to be any device moved by a thrust in the air, in space or under water, which has a sleeve body designed to receive a deployable element, the projectile being fired from cannon tubes or canisters, for example, or by means of its own suitable means generated thrust can be moved in the direction of the object to be controlled. Furthermore, there is the possibility of directing the projectile directed or unguided, ballistically or aerodynamically or hydrodynamically from a suitable launching device onto the object.
  • FIG. 1 denotes a projectile, shown schematically and in a sectional view, which essentially comprises a sleeve body 15, an ignition element 20 and a base part 25.
  • a propellant charge 30 is arranged in the front area of the projectile 1, which is operatively connected to the ignition element 20 in a manner not shown and is separated from the interior 16 of the sleeve body 15 by a film-like separating element 31.
  • a schematically shown element 40 which can be unfolded over a large area and is shown in the gathered state.
  • the element 40 is at one end via a schematically illustrated, shock-absorbing member 35 and means 36 not shown on the inside 15 'of the sleeve body 15, and at the other end via a tension member 27 and means 26 not shown on the inside 25 'of the bottom part 25 attached.
  • a corresponding predetermined breaking point 28 is provided on the circumference of the projectile 1 in order to separate the base part 25 from the sleeve body 15.
  • a shock-absorbing member 45 which essentially consists of a tension member 46 and is meandered and laid and glued to a set of layers lying parallel to one another and designated 47 in its entirety.
  • the adhesive located between the individual layers and surrounding the complete layer package 47 is denoted by 48 and by the hatching shown.
  • the organ 45 is fastened to the sleeve body 15 or the like with the one tension member end 46 ′ and the means 36 ′ and with the other tension member end 46 ′′ to the deployable element 40 (not shown in more detail).
  • the shock-absorbing member 45 according to FIG 2 when the element 40 is ejected in the direction of the arrow 51 from the sleeve body 15 (not shown in FIG.
  • FIG. 3 according to a first variant, the front section of a floor 2, which differs from the floor 1 according to FIG. 1, is shown and the sleeve body 15, the ignition element 20, the partially shown, expandable element 40 with the shock-absorbing element 35 can be seen as well as the propellant charge 30.
  • the propellant charge 30 is separated from the interior 16 of the sleeve body 15 by a disk-like wall 55 with openings 56, 56 '.
  • the organ 35 which is operatively connected to the element 40, is fastened to the wall 55 with the means 36 ′′ not shown in detail.
  • FIG. 4 shows, on a smaller scale, a projectile 3 according to a second variant and one recognizes the sleeve body 15, the ignition element 20, the deployable element 40 with the shock-absorbing element 35 and the base part 25 with the predetermined breaking point 28.
  • Deviating from the projectile 1 according to FIG Fig. 1 is the floor 3 in this variant provided with an explosive charge 60 in addition to the propellant charge 30 'separated from the interior 16 by a separating element 31'.
  • FIG. 5 shows a projectile 4 according to a third variant and one recognizes the sleeve body 15, the ignition element 20, the propellant charge 30, the partially shown, unfoldable element 40 ', 40 "and a schematically illustrated clamping part 41, 41' with a shock-absorbing element 35, 35 '.
  • the sleeve body 15 is provided on the inside 15' of the interior 16 with a circumferential, schematically illustrated predetermined breaking point 18 by means of which the sleeve body 15 can be separated into two identical sleeve parts 14, 14 ' Variant the element 40 ', 40 "by means of the schematically represented parts 35, 35' and 41, 41 'separately attached to the sleeve part 14 or 14' by means 36 ', 36".
  • the predetermined breaking point 18 separable sleeve parts 14, 14 'shown in section along the line VI-VI in Fig.5.
  • the fourth variant of a projectile 5 shown in FIGS. 7 and 8 essentially corresponds to the third variant described with reference to FIGS. 5 and 6.
  • a further predetermined breaking point 19 is provided on the floor 5 according to FIGS. 7 and 8, through which the sleeve body 15 is divided into four sleeve parts 12, 12 'and 13,13 'is separable.
  • the ignition element 20 and the base part 25 are separated from the sleeve body 15 at the predetermined breaking points 28, 28 ', the unfoldable element 140 being shown on the one hand by means of schematically illustrated, shock-absorbing elements 35 Sleeve parts 12, 12 ', 13, 13' and, on the other hand, are fastened to the ignition element 20 and to the base part 25.
  • the predetermined breaking point 19 lying in the sectional plane is not shown.
  • the individual projectile 1, 2, 3, 4 or 5 described above for example, shot down by a gun, not shown, in the direction of an object to be combated.
  • a rocket, a drone or an unmanned aircraft can also be used as a receiving and transport device for the deployable element.
  • the base part 25 is removed from the sleeve body 15 at the predetermined breaking point 28 separated and at the same time the deployable element is ejected or pulled out of the sleeve body 15.
  • the sleeve body 15 is separated into two symmetrical sections together with the base part and the ignition element 20.
  • FIG. 9 shows the projectile 1, 2 or 3 shot in the direction of arrow A and one can see the sleeve body 15, the organ 35 shown in a partially stretched state, the element 40, which is unfolded over a large area by air resistance and parachute-shaped, and the tension member 27 with the fastener attached to it Bottom part 25.
  • FIG. 10 shows, in an oblique view from above, at a short distance above sea or sea level, the sleeve parts 14, 14 'of object 10' of the projectile 4 according to FIG. 10, not shown in FIG. 5, 6 and one recognizes the tennis net-like element 40 'which is fastened at the ends to the respective sleeve part 14, 14' essentially by means of the clamping part 41, 41 'and the shock-absorbing member 35, 35'. Due to the predetermined firing direction and the effect of the propellant charge 30, the two sleeve parts 14, 14 'are steered approximately in the direction indicated by arrows B, B', such that the element 40 'has a relatively large span, as in FIG. 10 in part shown, flying towards the object 10 '.
  • the clamping part 41, 41 'arranged at the ends of the element 40' is designed for the correct, large-area deployment of the element 40 'and essentially comprises a relatively stiff one Bridge 37, 37 'oriented perpendicular to the water surface and ropes labeled 38, 38' and 39, 39 '.
  • the element shown schematically in FIGS. 9 and 10 and designated 40.40 ' consists, for example, of a network 42 formed by linking a large number of wires, ropes, threads or the like, which on the one hand has a low weight and on the other hand has a high tensile strength.
  • the unfolded element 40, 40 ' either totally intercepts or at least deflects the object 10, 10' from the targeted firing direction.
  • 42' denotes the lower edge facing the water surface and 42 "the upper edge of the element 40 'essentially facing the sky. Furthermore, it should be noted that at the inside of the part lying at the top in the drawing plane and the outside of the element 40 'can be seen at the part lying below in the drawing plane.
  • FIG. 12 shows the projectile 3 according to FIG. 4 for combating combat helicopters 12 hovering behind a cover and one can see the element 40, ropes 43 ′′ and the shock-absorbing element 35 in the area of the helicopter 12 braked by means of the parachute-like element Soil-set sleeve body 15.
  • the bottom part 25 (FIG. 4) is blown off the sleeve body 15 so that the element 40, as shown in FIG. 12, spans a large area in the area of the helicopter 12 and hovers in the air and only through the effect of the suction C, C 'caused by the rotor 12' is sucked in the direction of arrow D and wound up by the rotor 12 '.
  • the explosive charge 60 in FIG. 12 not shown
  • the organs 35, 35 '; 81.81 ', 83, 83' and 85.85 ' can also be designed as spring elements, for example as a spiral spring element.
  • the ignition element 20 of the individual projectile 1 to 4 described above is preferably designed as a time fuse which, when approaching the object to be combated, brings about the respective function of the projectile. Furthermore, in the application example according to FIGS. 10 and 11, the spin-stabilized projectile is aligned with respect to the longitudinal axis X-X by means of sensors or the like (not shown) such that the sleeve parts 14, 14 ′ fly apart essentially horizontally.

Landscapes

  • Engineering & Computer Science (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • General Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
EP85110294A 1984-09-25 1985-08-17 Projectile pour intercepter des objets en mouvement libre Withdrawn EP0175914A1 (fr)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
CH458184 1984-09-25
CH4581/84 1984-09-25

Publications (1)

Publication Number Publication Date
EP0175914A1 true EP0175914A1 (fr) 1986-04-02

Family

ID=4278769

Family Applications (1)

Application Number Title Priority Date Filing Date
EP85110294A Withdrawn EP0175914A1 (fr) 1984-09-25 1985-08-17 Projectile pour intercepter des objets en mouvement libre

Country Status (2)

Country Link
EP (1) EP0175914A1 (fr)
IL (1) IL76404A0 (fr)

Cited By (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2617956A1 (fr) * 1987-07-07 1989-01-13 Saint Louis Inst Projectile anti-helicoptere
DE4409424C1 (de) * 1994-03-18 1995-08-10 Daimler Benz Aerospace Ag Abfangvorrichtung für Flugobjekte
EP0856141A1 (fr) * 1995-10-17 1998-08-05 Foster-Miller Inc. Filet d'immobilisation a deploiement balistique
DE19601756C1 (de) * 1996-01-19 2000-12-28 Diehl Stiftung & Co Verfahren und Einrichtung zum Schutz gegen die Einwirkung eines schnellen Projektiles
US6626077B1 (en) 2002-10-16 2003-09-30 Mark David Gilbert Intercept vehicle for airborne nuclear, chemical and biological weapons of mass destruction
EP1752730A3 (fr) * 2005-08-10 2007-02-21 Rheinmetall Waffe Munition GmbH Dispositif et procédé de protection de véhicules contre des munitions, en particulier contre des charges creuses
DE19711823B3 (de) * 1997-03-21 2007-08-09 Diehl Stiftung & Co.Kg Sprenggranate
DE102009016147A1 (de) * 2009-04-03 2010-10-07 Rheinmetall Soldier Electronics Gmbh Zerlegendes Geschoss
EP2213975A3 (fr) * 2009-01-28 2013-09-04 Krauss-Maffei Wegmann GmbH & Co. KG Projectile cargo
RU2495359C1 (ru) * 2012-05-15 2013-10-10 Николай Валерьевич Чистяков Устройство уничтожения дистанционно пилотируемых (беспилотных) летательных аппаратов (дпла)
US8881638B2 (en) 2006-01-17 2014-11-11 Amsafe Bridport Limited Textile armour
DE102012000893B4 (de) * 2012-01-18 2014-12-24 Bundesrepublik Deutschland, vertreten durch das Bundesministerium der Verteidigung, dieses vertreten durch das Bundesamt für Ausrüstung, Informationstechnik und Nutzung der Bundeswehr Retardierend zerlegende Geschosshülle
CN104792227A (zh) * 2015-04-09 2015-07-22 从宏锦 拦截器
DE102015011058A1 (de) * 2015-08-27 2017-03-02 Rheinmetall Waffe Munition Gmbh System zur Abwehr von Bedrohungen
WO2018099603A1 (fr) 2016-12-02 2018-06-07 Rheinmetall Air Defence Ag Corps volant destiné à intercepter des drones ennemis
WO2020201391A1 (fr) * 2019-04-02 2020-10-08 Droptec Gmbh Filet d'interception avec dispositif d'absorption pour intercepter des drones

Citations (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB103500A (en) * 1916-01-22 1917-01-22 Herbert Mitchell Improvements in and connected with Shot for the Destruction of Entanglements or other Objects.
US1377467A (en) * 1920-11-13 1921-05-10 William A Crawford-Frost Torpedo-obstructing projectile
FR782097A (fr) * 1934-05-23 1935-05-27 Dispositif de protection anti-aérienne
GB493313A (en) * 1937-04-20 1938-10-06 Erich Bickel Improvements in and relating to anti-aircraft projectiles
FR859282A (fr) * 1939-05-04 1940-12-14 Projectile à filet
DE1175117B (de) * 1958-07-08 1964-07-30 Boelkow Entwicklungen Kg Geschoss
FR1465264A (fr) * 1965-03-10 1967-01-06 Dornier System Gmbh Amortisseur pour ensembles de remorquage de cibles aériennes
DE2206403A1 (de) * 1972-02-11 1973-08-16 Messerschmitt Boelkow Blohm Gefechtskopf mit mehreren sprengkoerpern, insbesondere zur bekaempfung von flugzielen
GB1508728A (en) * 1977-10-11 1978-04-26 Welham L Low flying aircraft defence system
US4262595A (en) * 1978-10-12 1981-04-21 The Singer Company Anti torpedo device
US4327644A (en) * 1979-05-01 1982-05-04 Stahan Corporation Projectile deployed cable weapons system

Patent Citations (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB103500A (en) * 1916-01-22 1917-01-22 Herbert Mitchell Improvements in and connected with Shot for the Destruction of Entanglements or other Objects.
US1377467A (en) * 1920-11-13 1921-05-10 William A Crawford-Frost Torpedo-obstructing projectile
FR782097A (fr) * 1934-05-23 1935-05-27 Dispositif de protection anti-aérienne
GB493313A (en) * 1937-04-20 1938-10-06 Erich Bickel Improvements in and relating to anti-aircraft projectiles
FR859282A (fr) * 1939-05-04 1940-12-14 Projectile à filet
DE1175117B (de) * 1958-07-08 1964-07-30 Boelkow Entwicklungen Kg Geschoss
FR1465264A (fr) * 1965-03-10 1967-01-06 Dornier System Gmbh Amortisseur pour ensembles de remorquage de cibles aériennes
DE2206403A1 (de) * 1972-02-11 1973-08-16 Messerschmitt Boelkow Blohm Gefechtskopf mit mehreren sprengkoerpern, insbesondere zur bekaempfung von flugzielen
GB1508728A (en) * 1977-10-11 1978-04-26 Welham L Low flying aircraft defence system
US4262595A (en) * 1978-10-12 1981-04-21 The Singer Company Anti torpedo device
US4327644A (en) * 1979-05-01 1982-05-04 Stahan Corporation Projectile deployed cable weapons system

Cited By (22)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2617956A1 (fr) * 1987-07-07 1989-01-13 Saint Louis Inst Projectile anti-helicoptere
DE4409424C1 (de) * 1994-03-18 1995-08-10 Daimler Benz Aerospace Ag Abfangvorrichtung für Flugobjekte
EP0674149A1 (fr) * 1994-03-18 1995-09-27 Daimler-Benz Aerospace Aktiengesellschaft Dispositif d'arrêt pour objets volants
US5583311A (en) * 1994-03-18 1996-12-10 Daimler-Benz Aerospace Ag Intercept device for flying objects
EP0856141A1 (fr) * 1995-10-17 1998-08-05 Foster-Miller Inc. Filet d'immobilisation a deploiement balistique
EP0856141A4 (fr) * 1995-10-17 1998-11-18 Foster Miller Inc Filet d'immobilisation a deploiement balistique
DE19601756C1 (de) * 1996-01-19 2000-12-28 Diehl Stiftung & Co Verfahren und Einrichtung zum Schutz gegen die Einwirkung eines schnellen Projektiles
DE19711823B3 (de) * 1997-03-21 2007-08-09 Diehl Stiftung & Co.Kg Sprenggranate
US6626077B1 (en) 2002-10-16 2003-09-30 Mark David Gilbert Intercept vehicle for airborne nuclear, chemical and biological weapons of mass destruction
EP1752730A3 (fr) * 2005-08-10 2007-02-21 Rheinmetall Waffe Munition GmbH Dispositif et procédé de protection de véhicules contre des munitions, en particulier contre des charges creuses
US8881638B2 (en) 2006-01-17 2014-11-11 Amsafe Bridport Limited Textile armour
US9310169B2 (en) 2006-01-17 2016-04-12 Amsafe Bridport Limited Textile armour
EP2213975A3 (fr) * 2009-01-28 2013-09-04 Krauss-Maffei Wegmann GmbH & Co. KG Projectile cargo
DE102009016147A1 (de) * 2009-04-03 2010-10-07 Rheinmetall Soldier Electronics Gmbh Zerlegendes Geschoss
DE102012000893B4 (de) * 2012-01-18 2014-12-24 Bundesrepublik Deutschland, vertreten durch das Bundesministerium der Verteidigung, dieses vertreten durch das Bundesamt für Ausrüstung, Informationstechnik und Nutzung der Bundeswehr Retardierend zerlegende Geschosshülle
RU2495359C1 (ru) * 2012-05-15 2013-10-10 Николай Валерьевич Чистяков Устройство уничтожения дистанционно пилотируемых (беспилотных) летательных аппаратов (дпла)
CN104792227A (zh) * 2015-04-09 2015-07-22 从宏锦 拦截器
DE102015011058A1 (de) * 2015-08-27 2017-03-02 Rheinmetall Waffe Munition Gmbh System zur Abwehr von Bedrohungen
WO2018099603A1 (fr) 2016-12-02 2018-06-07 Rheinmetall Air Defence Ag Corps volant destiné à intercepter des drones ennemis
WO2018099604A1 (fr) 2016-12-02 2018-06-07 Rheinmetall Air Defence Ag Dispositif de lancement conçu pour un missile pour intercepter des drones étrangers
AU2017369210B2 (en) * 2016-12-02 2021-04-15 Rheinmetall Air Defence Ag Missile for intercepting alien drones
WO2020201391A1 (fr) * 2019-04-02 2020-10-08 Droptec Gmbh Filet d'interception avec dispositif d'absorption pour intercepter des drones

Also Published As

Publication number Publication date
IL76404A0 (en) 1986-01-31

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