EP0691519A1 - Dispositif de combat non-mortelle contre des avions - Google Patents

Dispositif de combat non-mortelle contre des avions Download PDF

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Publication number
EP0691519A1
EP0691519A1 EP95106519A EP95106519A EP0691519A1 EP 0691519 A1 EP0691519 A1 EP 0691519A1 EP 95106519 A EP95106519 A EP 95106519A EP 95106519 A EP95106519 A EP 95106519A EP 0691519 A1 EP0691519 A1 EP 0691519A1
Authority
EP
European Patent Office
Prior art keywords
aircraft
bodies
interfering bodies
interfering
change
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
EP95106519A
Other languages
German (de)
English (en)
Other versions
EP0691519B1 (fr
Inventor
Ulrich Dipl. Ing. Rieger
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.)
Airbus Defence and Space GmbH
Original Assignee
Daimler Benz Aerospace 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 Daimler Benz Aerospace AG filed Critical Daimler Benz Aerospace AG
Publication of EP0691519A1 publication Critical patent/EP0691519A1/fr
Application granted granted Critical
Publication of EP0691519B1 publication Critical patent/EP0691519B1/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
    • F42B12/66—Chain-shot, i.e. the submissiles being interconnected by chains or the like

Definitions

  • the invention relates to a device for the non-lethal combat of aircraft according to the preamble of claim 1.
  • US Pat. No. 5,249,527 discloses disposable flexible, inflatable and shaping IR active bodies, which, however, are not able to force an aircraft to land.
  • DE 37 22 420 A1 discloses a projectile for combating a helicopter, which is shot roughly in the direction of the aircraft and is intended to enclose it with a net and cause it to crash.
  • an interception device for flying objects in which activatable, aerodynamic resistance bodies are incorporated, which completely or partially enclose the flying object and after a certain time destroy themselves by an integrated device.
  • this device is relatively complex, in particular due to the integrated self-destruct device.
  • the present invention has for its object to provide an active agent of the type mentioned, which is able to force unauthorized aircraft to turn or reliably land without thereby endangering the life of the occupants.
  • the first phase of the non-lethal combat of all types and sizes of aircraft provides for a target-seeking or self-guiding missile, which is provided with a detonator or proximity detonator and is densely filled with interfering objects to bring the aircraft to be forced to land and to bring the missile to an explosion such that the aircraft in question is enclosed by a dense cloud of interfering bodies.
  • these bodies are pressed close to the stagnation point of the aerodynamic surfaces and thus generate disturbances in the air flow in the most aerodynamically sensitive area, which lead to a considerable deterioration in flight behavior and cause vibrations, resistance increases and loss of lift . This inevitably leads to limited maneuverability, a loss of flight range and ultimately uncertainty for the pilot.
  • the interfering bodies In order to enable the aircraft to land properly, without restriction, the interfering bodies must be designed in such a way that their interference during landing approaches is or is reduced to such an extent that the landing can be carried out absolutely safely. To a large extent this will be achievable simply by reducing the cruising speed to the landing speed, since a large part of the interfering bodies will fall off by themselves, for example.
  • the shape, design and size of the individual interfering bodies can be produced in a variety of ways. They should have a length of 5 to about 20 cm and a thickness of a few tenths of a millimeter up to about 2 to 3 centimeters. Different embodiments are illustrated in FIGS. 2 to 4 of the drawing.
  • the embodiment of FIG. 2 consists of resilient material which is forced into a flat shape with the application of force during the so-called packing process. After ejection - i.e. in the state of suspension - the interfering bodies take on a clearly spatially extended shape in order to adapt to the contour of the aerodynamic surfaces and to get caught. it is - as shown in FIG. 2 - a narrow, resilient steel strip is twisted in its longitudinal direction and individual partial areas are spread apart.
  • the interfering bodies consist of chains of small, essentially flat bodies made of metal or plastic which are connected to one another by a thread and are designed in such a way that they face up to the flow when they flow against them, for example as a cone or correspondingly attached disks, polygonal plates etc. .
  • each envelope contains an inflating agent which is slightly increased Pressure is liquid and is gaseous under atmospheric or dynamic pressure (the so-called butane lighter principle). These interfering active bodies are kept under increased pressure for transport.
  • the interfering active bodies consist of foam and are only generated when they are deployed.
  • a specific storage supply of foam-forming material is to be transported here, together with a generator, for example a strand-forming mixing and chopping device to form the interfering bodies.
  • a generator for example a strand-forming mixing and chopping device to form the interfering bodies.
  • These are preferably elongated, but also ring-shaped, chain-shaped with or without barbs, noses or friction surfaces, etc.
  • the various interfering active bodies are designed in such a way that, after a certain time, they automatically assume a flat shape or fall off or disintegrate. This ensures that the interference effect is at least reduced so that a safe, largely optimal landing is guaranteed.
  • the interfering active bodies assume a flat shape or disintegrate again due to external radiation. Examples of this are active bodies which consist partially or entirely of a material which decomposes when irradiated with laser light, microwaves, etc.
  • This embodiment has the advantage that the impairment of the aircraft can be removed immediately if it can be seen that it is following the instructions.

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • General Engineering & Computer Science (AREA)
  • Vibration Dampers (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Details Of Aerials (AREA)
EP95106519A 1994-06-06 1995-04-29 Dispositif de combat non-mortelle contre des avions Expired - Lifetime EP0691519B1 (fr)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE4419788 1994-06-06
DE4419788A DE4419788C2 (de) 1994-06-06 1994-06-06 Vorrichtung zur nichtletalen Bekämpfung von Flugzeugen

Publications (2)

Publication Number Publication Date
EP0691519A1 true EP0691519A1 (fr) 1996-01-10
EP0691519B1 EP0691519B1 (fr) 1997-04-09

Family

ID=6519937

Family Applications (1)

Application Number Title Priority Date Filing Date
EP95106519A Expired - Lifetime EP0691519B1 (fr) 1994-06-06 1995-04-29 Dispositif de combat non-mortelle contre des avions

Country Status (3)

Country Link
US (1) US5814753A (fr)
EP (1) EP0691519B1 (fr)
DE (2) DE4419788C2 (fr)

Families Citing this family (23)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6381894B1 (en) 2000-08-29 2002-05-07 The United States Of America As Represented By The Secretary Of The Navy Bola launcher
US6782790B2 (en) * 2002-12-20 2004-08-31 Bae Systems Information And Electronic Systems Integration Inc. Method for deflecting fast projectiles
FR2887327B1 (fr) * 2005-06-17 2007-08-24 Thales Sa Procede de protection antimissiles de vehicules et dispositif de mise en oeuvre
DE102015011058A1 (de) * 2015-08-27 2017-03-02 Rheinmetall Waffe Munition Gmbh System zur Abwehr von Bedrohungen
US10107599B2 (en) 2016-03-25 2018-10-23 Wrap Technologies, Inc. Entangling projectiles and systems for their use
US10036615B2 (en) * 2016-03-25 2018-07-31 Wrap Technologies, Inc. Entangling projectile deployment system
US10438494B1 (en) * 2016-10-10 2019-10-08 Amazon Technologies, Inc. Generation of flight plans for aerial vehicles
CA3049793A1 (fr) * 2017-01-10 2018-07-19 AIRSHARE, Inc. Systeme et procede de communication avec un uav
DE102017109874A1 (de) * 2017-05-08 2018-11-08 Rheinmetall Waffe Munition Gmbh Abwehrsystem gegen leichte Flugkörper, wie Drohnen
US10634461B2 (en) 2017-06-24 2020-04-28 Wrap Technologies, Inc. Entangling projectiles and systems for their use
USD822785S1 (en) 2017-09-29 2018-07-10 Wrap Technologies, Inc. Projectile casing
USD820940S1 (en) 2017-09-29 2018-06-19 Wrap Technologies, Inc. Projectile launcher
US10724831B1 (en) * 2017-10-16 2020-07-28 Leidos, Inc. Fibrous occlusive interruption of lift
WO2019079288A1 (fr) 2017-10-18 2019-04-25 Wrap Technologies, Inc. Systèmes et procédés de génération de faisceaux de ciblage
US10852114B2 (en) 2018-07-03 2020-12-01 Wrap Technologies, Inc. Adhesive-carrying entangling projectiles and systems for their use
US11371810B2 (en) 2018-07-03 2022-06-28 Wrap Technologies, Inc. Seal-carrying entangling projectiles and systems for their use
US10890419B2 (en) 2018-09-11 2021-01-12 Wrap Technologies, Inc. Systems and methods for non-lethal, near-range detainment of subjects
US11835320B2 (en) 2018-09-11 2023-12-05 Wrap Technologies, Inc. Systems and methods for non-lethal, near-range detainment of subjects
US10948269B2 (en) 2018-12-04 2021-03-16 Wrap Technologies Inc. Perimeter security system with non-lethal detainment response
US11156432B1 (en) 2020-08-31 2021-10-26 Wrap Techologies, Inc. Protective coverings and related methods for entangling projectiles
US11761737B2 (en) 2021-02-18 2023-09-19 Wrap Technologies, Inc. Projectile launching systems with anchors having dissimilar flight characteristics
US11555673B2 (en) 2021-02-18 2023-01-17 Wrap Technologies, Inc. Projectile launching systems with anchors having dissimilar flight characteristics
US11852439B2 (en) 2021-11-24 2023-12-26 Wrap Technologies, Inc. Systems and methods for generating optical beam arrays

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE318027C (fr) *
GB100753A (en) * 1915-06-16 1900-01-01 Wilbur Carrier James An Improvement in Projectiles in reference to their Loading.
CH210356A (de) * 1939-06-13 1940-07-15 Carl Dr Meyer Geschoss für Flugzeugabwehr.
FR858712A (fr) * 1939-04-29 1940-12-02 Petits Fils Francois Wendel Bombe plus particulièrement utilisable pour la défense contre aéronefs et usages aanalogues
DE1209838B (de) * 1963-04-16 1966-01-27 American Chain & Cable Co Wicklung aus sich selbsttaetig abspulendem Band sowie ein Verfahren und eine Einrichtung zu ihrer Herstellung
DE3800879A1 (de) * 1988-01-14 1988-09-01 Gerd Rienks Waffenbremse

Family Cites Families (21)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1309530A (en) * 1919-07-08 Aircraft-projectile
US1312764A (en) * 1919-08-12 straub
US1171152A (en) * 1914-05-07 1916-02-08 Joseph A Steinmetz Capturing or destroying aircraft.
US1211001A (en) * 1914-12-08 1917-01-02 Joseph A Steinmetz Ordnance-projectile.
US1488182A (en) * 1921-11-17 1924-03-25 Gordon T Whelton Ordnance projectile
US1759912A (en) * 1925-11-11 1930-05-27 William H Mount Antiaircraft offensive and defensive means
US1744233A (en) * 1927-01-11 1930-01-21 Locori Pietro Projectile for antiaircraft fire
US1757788A (en) * 1928-03-05 1930-05-06 Erasmus G West Antiaircraft shell
US2322624A (en) * 1939-10-06 1943-06-22 John D Forbes Chain shot
US2285789A (en) * 1940-03-01 1942-06-09 Ace W Woolley Airplane trap
US2373364A (en) * 1940-11-15 1945-04-10 Welleome Hubert Bolas projectile
US2283065A (en) * 1941-06-05 1942-05-12 Hunter Thurman Hawkins Chain shot
US2374261A (en) * 1941-09-05 1945-04-24 Ames Blanche Ames Propeller snare
US2339921A (en) * 1942-06-17 1944-01-25 Walter B Fraser Antiaircraft projectile
US2368587A (en) * 1942-09-17 1945-01-30 Wise Edward Brooks Antiaircraft shell
US2360096A (en) * 1942-12-21 1944-10-10 John W Aydelotte Shell body
DE3327043A1 (de) * 1983-07-27 1985-02-07 Technisch-Mathematische Studiengesellschaft mbH, 5300 Bonn Vorrichtung zum ausstreuen elektromagnetischen scheinzielmaterials, insbesondere aus einer rakete
DE3437594A1 (de) * 1984-10-13 1986-04-17 Diehl GmbH & Co, 8500 Nürnberg Hubschrauberabwehrgeschoss
DE3722420A1 (de) * 1987-07-07 1989-01-26 Deutsch Franz Forsch Inst Geschoss zur bekaempfung eines hubschraubers
DE3735426A1 (de) * 1987-10-20 1989-05-03 Hans Dipl Ing Simon Geschoss mit entfaltbarem element zur bekaempfung freibeweglicher objekte, vorzugsweise flugkoerpern
US5249527A (en) * 1992-07-01 1993-10-05 Westinghouse Electric Corp. High speed, inflating bag infrared countermeasure

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE318027C (fr) *
GB100753A (en) * 1915-06-16 1900-01-01 Wilbur Carrier James An Improvement in Projectiles in reference to their Loading.
FR858712A (fr) * 1939-04-29 1940-12-02 Petits Fils Francois Wendel Bombe plus particulièrement utilisable pour la défense contre aéronefs et usages aanalogues
CH210356A (de) * 1939-06-13 1940-07-15 Carl Dr Meyer Geschoss für Flugzeugabwehr.
DE1209838B (de) * 1963-04-16 1966-01-27 American Chain & Cable Co Wicklung aus sich selbsttaetig abspulendem Band sowie ein Verfahren und eine Einrichtung zu ihrer Herstellung
DE3800879A1 (de) * 1988-01-14 1988-09-01 Gerd Rienks Waffenbremse

Also Published As

Publication number Publication date
DE4419788C2 (de) 1996-05-30
US5814753A (en) 1998-09-29
DE4419788A1 (de) 1995-12-07
EP0691519B1 (fr) 1997-04-09
DE59500172D1 (de) 1997-05-15

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