EP0187900A2 - 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
EP0187900A2
EP0187900A2 EP85113061A EP85113061A EP0187900A2 EP 0187900 A2 EP0187900 A2 EP 0187900A2 EP 85113061 A EP85113061 A EP 85113061A EP 85113061 A EP85113061 A EP 85113061A EP 0187900 A2 EP0187900 A2 EP 0187900A2
Authority
EP
European Patent Office
Prior art keywords
aircraft
charges
target
drone
projectile
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.)
Granted
Application number
EP85113061A
Other languages
German (de)
English (en)
Other versions
EP0187900B1 (fr
EP0187900A3 (en
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.
  • a missile is known in the manner of a drone for fighting ground targets from the ground.
  • the drone is among other things equipped with a homing head and a detonatable warhead.
  • the drone tackles the target in a dive by hitting the target.
  • a drone in the manner of a missile with a strongly swept structure, in particular delta wings, but without combat charges, is known from OE-OS 32 40 903.
  • DE-PS 27 41 984 proposes a warhead with at least one prong-forming shaped charge.
  • This warhead is part of a grenade or a missile.
  • Spike-forming shaped charges are almost ineffective due to the relatively large combat distance of approx. 100 m.
  • the object of the invention is therefore to combat ground targets, namely light and heavily armored targets, cost-effectively 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 which are arranged in the drone according to the characteristics of the subclaims or 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 in that the charge arrangement consists of two or more P-charges arranged axially parallel, which are ignited simultaneously. This ensures an increased probability of being hit and destroyed, especially for targets that are difficult to fight, such as battle tanks.
  • the effectiveness of the drone can be increased in that multiple targets can be combated by a single drone by providing the drone with at least one submunition that can be fired. After the release of a submunition, the drone stabilizes for the further detection of targets and the release of a second submunition or ignition of the stationary charges.
  • each of the projectile-forming charges carried by an aircraft is provided for a selectively different manner of delivery from the carrier, specifically in the manner of submunition or in the manner of launching 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.
  • 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.
  • a self-sufficient detection device
  • 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 also be arranged in the drone in a stationary or 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 of aerodynamic stabilization of the submunition when it is discharged "upwards".
  • the submunition can therefore be arranged in the drone so that its direction of action is “up” or “down”. With the "up” 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)
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
DE19843438305 DE3438305A1 (de) 1984-10-19 1984-10-19 Unbemanntes fluggeraet fuer die bekaempfung von bodenzielen
DE3438305 1984-10-19

Publications (3)

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

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2658597A1 (fr) * 1990-02-16 1991-08-23 Thomson Brandt Armements Arme sans recul.
GB2317676A (en) * 1989-10-18 1998-04-01 Messerschmitt Boelkow Blohm Ejection and distribition of sub-ammunition

Families Citing this family (2)

* 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
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

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2317676A (en) * 1989-10-18 1998-04-01 Messerschmitt Boelkow Blohm Ejection and distribition of sub-ammunition
GB2317676B (en) * 1989-10-18 1998-07-15 Messerschmitt Boelkow Blohm Ejection and distribution method for sub-ammunition
FR2658597A1 (fr) * 1990-02-16 1991-08-23 Thomson Brandt Armements Arme sans recul.

Also Published As

Publication number Publication date
DE3586945D1 (de) 1993-02-11
IL76632A0 (en) 1986-02-28
EP0187900B1 (fr) 1992-12-30
DE3438305A1 (de) 1986-04-24
IL76632A (en) 1994-05-30
EP0187900A3 (en) 1990-04-18

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