EP0187900B1 - Avion non équipé pour la lutte contre cibles terrestres - Google Patents

Avion non équipé pour la lutte contre cibles terrestres Download PDF

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Publication number
EP0187900B1
EP0187900B1 EP85113061A EP85113061A EP0187900B1 EP 0187900 B1 EP0187900 B1 EP 0187900B1 EP 85113061 A EP85113061 A EP 85113061A EP 85113061 A EP85113061 A EP 85113061A EP 0187900 B1 EP0187900 B1 EP 0187900B1
Authority
EP
European Patent Office
Prior art keywords
drone
target
projectile
submunition
charge
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
EP85113061A
Other languages
German (de)
English (en)
Other versions
EP0187900A3 (en
EP0187900A2 (fr
Inventor
Klaus Lindstädt
Karl Rudolf
Adolf Weber
Heinrich Lükewille
Wilfried Röll
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.)
Diehl Verwaltungs Stiftung
Original Assignee
Diehl GmbH and Co
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 Diehl GmbH and Co filed Critical Diehl GmbH and Co
Publication of EP0187900A2 publication Critical patent/EP0187900A2/fr
Publication of EP0187900A3 publication Critical patent/EP0187900A3/de
Application granted granted Critical
Publication of EP0187900B1 publication Critical patent/EP0187900B1/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
    • F42B12/36—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
    • F42B12/60—Cluster or cargo ammunition, i.e. projectiles containing one or more submissiles the submissiles being ejected radially
    • 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
    • F42B12/14—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 the symmetry axis of the hollow charge forming an angle with the longitudinal axis of the projectile

Definitions

  • the invention relates to an unmanned aerial vehicle for controlling ground targets according to the preamble of claim 1.
  • DE-A1 25 19 507 discloses an unmanned aerial vehicle, for example a rocket-powered missile, in which at least one projectile-forming charge is provided as a stationary combat charge.
  • the direction of action of the stationary charge selected in relation to a target is directly aimed at the target.
  • the target is fought, the entire missile is inevitably destroyed after the selected stationary charge has been shot down, so that only a single target has to be fought with the direct fire. If several selected targets must therefore be fought, a correspondingly large number of missiles is required.
  • the object of the invention is to combat ground targets, namely light and heavily armored targets, inexpensively and effectively by means of an unmanned aerial vehicle.
  • the stable approach of the aircraft for example a drone, is an ideal weapon platform with the advantages of reliable detection of the targets due to the low speed of the drone of approx. 250 to 300 km / h with an average attack altitude of approx. 70 m.
  • the targets are combated by projectile-forming charges that are stationary in the drone and arranged in the form of ejectable submunitions.
  • a target lies in the direction of action of the stationary charge arrangement, the ignition is possible without prior correction of the flight position. If, on the other hand, the target lies outside the direction of action of the cargo arrangement, a slight correction of the flight position (e.g. by rolling motion) is sufficient to combat the target.
  • the effectiveness of the drone is increased by the charge arrangement consisting of two or more axially ignitable P charges arranged in parallel. This ensures an increased likelihood of being hit and destroyed, especially for targets that are difficult to fight, such as battle tanks.
  • targets can be combated by a single drone by providing the drone with at least one "ammunition" that can be launched. After the release of one submunition, the drone is stabilized for the further detection of targets and the release of a second submunition or ignition of the stationary charges.
  • the drone Due to the "upwards" submunition, the drone has a high probability of acquisition at very low altitude. Due to the longer time span for the aerodynamic stabilization of the submunition with subsequent detection with a larger usable search radius and the triggering of the projectile-forming charge, the required probability of a hit is present.
  • the deployment area of armored units or other unmanned aerial vehicles can be combated cost-effectively by flying several drones in strips over the target area.
  • the multiple combat of a single target by several drones is largely excluded in a simple manner.
  • each of the projectile-forming charges carried by an aircraft is intended for a selectively different manner of delivery from the carrier, namely in the manner of submunition or in the manner with firing from the aircraft.
  • the choice of the type of delivery of the loads as submunition includes, in the presence of several loads, delivery combinations according to which the delivery is effected individually or in groups with time intervals or all loads at the same time.
  • a drone 1 with delta wings 2, 3 has a multi-part fuselage 4. 2 to 5 projectile-forming charges 35 in the form of stationary charges 6 to 8 and ejectable submunitions 9 to 11 are arranged in a bow section 5.
  • a detection device (not shown) for detecting a detection corridor 16 is accommodated in a subsequent section 15.
  • the upwardly ejectable submunition 9 is arranged in a central section 20 with the center of gravity 21.
  • a battle tank 30 is identified by the detection device with corresponding target data.
  • the submunition 9 is ejected from a container 32 via an ejection charge 31 and stabilized via a parachute 33. In a known manner, the submunition 9 executes a circular movement while hanging on the parachute 33.
  • An autonomous detection device of the submunition 9 triggers the projectile-forming charge 35 when the target is detected.
  • a target 40 which is subsequently detected, is combated by the projectile-forming charge 10.
  • a subsequently detected third target 45 is combated by the projectile-forming charge 6 arranged stationary in the drone.
  • the drone 1 is rotated about its main axis 46 by appropriate control maneuvers of the drone in the direction of arrow 47 to such an extent that the target 45 lies within the effective range of the projectile-forming charge 6.
  • the path of the projectile is designated 48.
  • the projectile-forming charges 6 to 8 are shown in the bow section 5 in a schematic representation.
  • Shock wave-reflecting insulating layers 51, 52 are arranged between said charges 6 to 8. This ensures that with simultaneous detonation of the projectile-forming charges 6 to 8, there is no mutual influence which could interfere with the projectile formation. With these charges it is provided that a target is combated by charges 6 to 8 at the same time. The detonation of the charges leads to the destruction of the bow section 5, which then leads to the drone 1 crashing.
  • the submunitions 9, which can be ejected downwards are arranged.
  • the underside of the drone 1 is designated 53 and the top 54.
  • the stationary charge 6 and the ejectable submunition 10 are accommodated in the bow section 5.
  • the ejectable submunition 9 is arranged in the fuselage section 4 in the area of the center of gravity 21.
  • the directions of action of the charge 6 and the submunition 10 are designated 41, 42.
  • ejectable submunitions 9 to 11 are arranged in the bow section 5 of the drone 1 and in the fuselage section 4.
  • two targets are to be combated, in that the first target is to be combated with the submunition 9 and the second target is to be combated simultaneously with the stationary charges 6 and 7.
  • a single charge can be arranged in the drone in a stationary and ejectable manner.
  • the stationary charges in the drone - viewed in the direction of flight - can also be arranged transversely at an angle to the vertical longitudinal plane.
  • the ejectable submunition can also be fired directly in the manner of a stationary charge.
  • the arrangement of the submunition in the drone with respect to the direction of action of the submunition depends on the type "aerodynamic" of the type of aerodynamic stabilization of the ejected submunition.
  • the submunition can therefore be arranged in the drone so that its direction of action is “upwards” or “downwards”. With the "upward” direction of action, the drone can also be used against helicopters by flying underneath the target and firing the submunition directly. Instead of submunition, an "upward" stationary charge of the drone must also be provided.

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • General Engineering & Computer Science (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Geophysics And Detection Of Objects (AREA)

Claims (3)

  1. Missile (1) téléguidé, tel que drones, conteneurs d'agents NBC, fusées, pour combattre des objectifs au sol (40), avec une tête chercheuse et au moins une charge de combat (6) fixe, pouvant exploser, dont la direction d'action (42) par rapport au missile (1) en position horizontale, est, en option, dirigée "vers le bas" et qui est conçue comme une charge formant projectile (6 à 10), caractérisé en ce qu'il est prévu en supplément au moins une charge formant projectile en tant que sous-munition (9, 10) combattant de manière autonome l'objectif (30, 40, 45) et qui par rapport à la position horizontale du missile (1) peut être éjectée, en option, "vers le haut".
  2. Missile selon la revendication 1, caractérisé en ce que les charges fixes (6 à 8) sont séparées par des couches d'isolation (51, 52), absorbant les ondes de choc.
  3. Missile selon la revendication 1, caractérisé en ce que les sous-munitions (9) éjectables sont placées dans la zone du centre de gravité (21), dans la région du fuselage (20) du missile (1).
EP85113061A 1984-10-19 1985-10-15 Avion non équipé pour la lutte contre cibles terrestres Expired - Lifetime EP0187900B1 (fr)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE3438305 1984-10-19
DE19843438305 DE3438305A1 (de) 1984-10-19 1984-10-19 Unbemanntes fluggeraet fuer die bekaempfung von bodenzielen

Publications (3)

Publication Number Publication Date
EP0187900A2 EP0187900A2 (fr) 1986-07-23
EP0187900A3 EP0187900A3 (en) 1990-04-18
EP0187900B1 true EP0187900B1 (fr) 1992-12-30

Family

ID=6248271

Family Applications (1)

Application Number Title Priority Date Filing Date
EP85113061A Expired - Lifetime EP0187900B1 (fr) 1984-10-19 1985-10-15 Avion non équipé pour la lutte contre cibles terrestres

Country Status (3)

Country Link
EP (1) EP0187900B1 (fr)
DE (2) DE3438305A1 (fr)
IL (1) IL76632A (fr)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3924352C1 (de) * 1989-07-22 1997-01-30 Diehl Gmbh & Co Flugkörper zur Bekämpfung von Bodenzielen
GB9014653D0 (en) * 1989-10-18 1997-11-05 Messerschmitt Boelkow Blohm Auswerfen und verteilen von submunition
FR2658597B1 (fr) * 1990-02-16 1994-05-27 Thomson Brandt Armements Arme sans recul.
DE102019109360A1 (de) * 2019-04-09 2020-10-15 Rheinmetall Air Defence Ag Inventionssystem zur Abwehr von RAM-Zielen und/oder UAVs sowie Verfahren zur Abwehr von RAM-Zielen und/oder UAVs

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2519507A1 (de) * 1975-05-02 1976-11-18 Messerschmitt Boelkow Blohm Munition zur bekaempfung von zielen, insbesondere flugzielen im vorbeiflug
DE2904749C2 (de) * 1979-02-08 1984-01-05 Messerschmitt-Bölkow-Blohm GmbH, 8000 München Flugkörper nach Art einer Drohne
DE3244708A1 (de) * 1982-12-03 1984-06-07 Diehl GmbH & Co, 8500 Nürnberg Einrichtung zur erzeugung eines zuendsignals fuer ueberflug-flugkoerper
DE3127674A1 (de) * 1981-07-14 1983-02-24 Rheinmetall GmbH, 4000 Düsseldorf Verfahren und vorrichtung zum belegen einer zielflaeche mit munition
DE3219535C2 (de) * 1982-05-25 1984-04-05 Messerschmitt-Bölkow-Blohm GmbH, 8000 München Flugkörper zum Absetzen von Streumunition
DE3306659A1 (de) * 1983-02-25 1984-08-30 Rheinmetall GmbH, 4000 Düsseldorf Wirkkoerpereinheit

Also Published As

Publication number Publication date
IL76632A0 (en) 1986-02-28
EP0187900A3 (en) 1990-04-18
EP0187900A2 (fr) 1986-07-23
DE3438305A1 (de) 1986-04-24
DE3586945D1 (de) 1993-02-11
IL76632A (en) 1994-05-30

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