EP0391095A1 - Device for the recovery of unmanned reusable missiles - Google Patents

Device for the recovery of unmanned reusable missiles Download PDF

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Publication number
EP0391095A1
EP0391095A1 EP90104714A EP90104714A EP0391095A1 EP 0391095 A1 EP0391095 A1 EP 0391095A1 EP 90104714 A EP90104714 A EP 90104714A EP 90104714 A EP90104714 A EP 90104714A EP 0391095 A1 EP0391095 A1 EP 0391095A1
Authority
EP
European Patent Office
Prior art keywords
guiding elements
holding
receiving surface
missiles
phase
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Withdrawn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
EP90104714A
Other languages
German (de)
French (fr)
Inventor
Werner Heinzmann
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
Messerschmitt Bolkow Blohm 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 Messerschmitt Bolkow Blohm AG filed Critical Messerschmitt Bolkow Blohm AG
Publication of EP0391095A1 publication Critical patent/EP0391095A1/en
Withdrawn legal-status Critical Current

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    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B63—SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
    • B63B—SHIPS OR OTHER WATERBORNE VESSELS; EQUIPMENT FOR SHIPPING 
    • B63B35/00—Vessels or similar floating structures specially adapted for specific purposes and not otherwise provided for
    • B63B35/50—Vessels or floating structures for aircraft
    • B63B35/52—Nets, slipways or the like, for recovering aircraft from the water

Definitions

  • the invention relates to a device for recovering unmanned reusable missiles (drones) in the return phase, the landing phase being carried out by automatic or remote-controlled control arrangements and additional aids, such as parachute recovery systems.
  • the object of the invention is to provide a simple salvage of generic missiles, which in particular enables use on ships and also ensures the inclusion in unfavorable environmental conditions, such as waves.
  • a flexible surface element from a contracted, folded and / or folded magazine stowed phase is arranged on actuatable holding and guiding elements to form a trampoline-like receiving surface on a vehicle.
  • a favorable embodiment is created in that the flexible surface element is formed from a network.
  • the holding and guiding elements be formed by telescopic arrangements that can be extended.
  • the holding and guiding elements are arranged so that they can be extended and folded out in the lateral and longitudinal directions to form the receiving surface.
  • 1 holding and guiding elements in the form of a telescoping device 2 which can be extended to the rear are arranged in the rear region of a marine vehicle and can additionally be folded into the outer region via struts 3.
  • These elements 2, 3 serve as a holder for a flexible surface element 4 in the form of a network and form a trampoline-like receiving surface 5. It is thus possible, from a magazine-stowed stowage phase of the surface element 4 according to FIGS. 3 and 4 with a small space requirement on the marine vehicle 1, a corresponding one to form large receiving surface 5 and to bring it back into the original position.
  • the receiving surface 5 makes it possible to create a relatively large landing site for a drone 6 in order to take it up by automatic or remote-controlled control arrangements (not shown) and additional aids, such as a parachute, in the recovery phase. Precise landing is therefore not necessary and environmental conditions such as waves and wind can also be controlled.

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  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • Ocean & Marine Engineering (AREA)
  • Toys (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)

Abstract

To create a relatively large landing surface for the recovery of drones, provision is made for a flexible sheet-like element (5) for forming a trampoline-like receiving surface to be arranged in such a way that it can be spread out on a vessel. To this end, the sheet-like element is brought into a spread-out position from a contracted, folded and/or collapsed stored stowage phase via extendable holding and guiding elements. <IMAGE>

Description

Die Erfindung bezieht sich auf eine Vorrichtung zum Bergen von unbemannten wiederverwendbaren Flugkörpern (Drohnen) in der Rückführungsphase, wobei die Lande­phase durch automatische oder ferngesteuerte Steueran­ordnungen und zusätzlicher Hilfsmittel, wie Fall­schirmbergesysteme, erfolgt.The invention relates to a device for recovering unmanned reusable missiles (drones) in the return phase, the landing phase being carried out by automatic or remote-controlled control arrangements and additional aids, such as parachute recovery systems.

Bei der Rückkehr ferngesteuerte, beispielsweise zu Aufklärungszwecken eingesetzter Flugköper, ist es be­kannt, daß die Landung durch einen im Flugkörper mit­geführten Fallschirm realisiert wird. Hierbei sind Me­thoden und Steuerungen bekannt geworden, um unter Be­rücksichtigung der vorliegenden Verhältnisse eine re­lativ gute Landepunktvorhersage zu machen. Es hat. sich aber gezeigt, daß es insbesondere beim Einsatz in Ge­wässern relativ schwierig ist, eine Bergung aus dem Wasser vorzunehmen, da es hierzu erforderlich ist, mit dem Schiff entsprechende Wendekreise zu fahren, die einen großen Zeitaufwand erfordern.When returning remote-controlled missiles, for example used for reconnaissance purposes, it is known that the landing is realized by a parachute carried in the missile. Methods and controls have become known in order to make a relatively good landing point prediction taking into account the existing conditions. It has. it has been shown, however, that it is relatively difficult, particularly when used in water, to recover from the Water, since it is necessary to make appropriate turning circles with the ship, which require a lot of time.

Die Aufgabe der Erfindung ist es, eine einfache Bergung von gattungsgemäßen Flugkörpern zu schaffen, die ins­besondere einen Einsatz auf Schiffen ermöglicht und auch die Aufnahme bei ungünstigen Umweltbedingungen, wie Wellengang, gewährleistet.The object of the invention is to provide a simple salvage of generic missiles, which in particular enables use on ships and also ensures the inclusion in unfavorable environmental conditions, such as waves.

Die Lösung dieser Aufgabe erfolgt erfindungsgemäß da­durch, daß an einem Fahrzeug ein flexibles Flächenele­ment aus einer zusammengezogenen, gefalteten und/oder geklappten magazinierten Stauphase über betätigbare Halte- und Führungselemente zur Bildung einer trampo­linartiger Aufnahmefläche aufspannbar angeordnet ist.This object is achieved according to the invention in that a flexible surface element from a contracted, folded and / or folded magazine stowed phase is arranged on actuatable holding and guiding elements to form a trampoline-like receiving surface on a vehicle.

Hierdurch ist es möglich, eine relativ große Aufnahme­fläche zu bilden, die während des normalen Einsatzes des Fahrzeuges keine Beeinträchtigung darstellt. Durch die trampolinartige Aufnahmefläche ist auch eine Erhö­hung der Auftreffgeschwindigkeiten durchführbar und somit auch eine gezielte Ansteuerung des Landepunktes besser realisierbar.This makes it possible to form a relatively large receiving area, which does not constitute an impairment during normal use of the vehicle. Due to the trampoline-like receiving surface, an increase in the impact speeds can also be carried out and thus a targeted control of the landing point can be realized more effectively.

Ein besonderer Vorteil ergibt sich beim Einsatz auf Schiffen, da hierbei eine genaue Ausrichtung durch Wellengang nicht gewährleistet ist.A particular advantage arises when used on ships, since precise alignment due to waves is not guaranteed.

Eine günstige Ausgestaltung wird dadurch geschaffen, daß das flexible Flächenelement aus einem Netzwerk ge­bildet ist.A favorable embodiment is created in that the flexible surface element is formed from a network.

Um eine einfache Handhabung zu ermöglichen wird vorge­schlagen, daß die Halte- und Führungselemente durch ausfahrbare Teleskopanordnungen gebildet sind.In order to enable simple handling, it is proposed that the holding and guiding elements be formed by telescopic arrangements that can be extended.

Eine den Platzbedarf auf dem Fahrzeug nicht beein­trächtigende Anordnung wird dadurch geschaffen, daß für die Anordnung auf Schiffen die Halte- und Führungsele­mente in den über das Heck hinausgehenden Bereich aus­fahrbar sind.An arrangement which does not impair the space required on the vehicle is created in that the holding and guiding elements can be extended into the area beyond the stern for the arrangement on ships.

Um eine große Aufnahmefläche zu schaffen, wird vorge­schlagen, daß die Halte- und Führungselemente in Seiten- und Längsrichtung zur Ausbildung der Aufnahme­fläche ausfahrbar und ausklappbar angeordnet sind.In order to create a large receiving surface, it is proposed that the holding and guiding elements are arranged so that they can be extended and folded out in the lateral and longitudinal directions to form the receiving surface.

In der Zeichnung ist ein Ausführungsbeispiel der Er­findung schematisch dargestellt. Es zeigen:

  • Fig. 1 eine Seitenansicht eines Marinefahrzeuges mit einer ausgefahrenen Aufnahmefläche,
  • Fig. 2 eine Teildraufsicht gemäß Fig. 1,
  • Fig. 3 eine Seitenansicht auf eine gestaute Aufnahmefläche,
  • Fig. 4 eine Draufsicht gemäß Fig. 3.
In the drawing, an embodiment of the invention is shown schematically. Show it:
  • 1 is a side view of a marine vehicle with an extended receiving surface,
  • 2 is a partial plan view of FIG. 1,
  • 3 is a side view of a stowed receiving surface,
  • 4 is a top view according to FIG. 3.

Bei der dargestellten Ausbildung sind im Heckbereich eines Marinefahrzeuges 1 Halte- und Führungselemente in Form einer nach hinten ausfahrbaren teleskopierenden Einrichtung 2 angeordnet, die zusätzlich über Streben 3 in den Außenbereich klappbar sind. Diese Elemente 2, 3 dienen als eine Halterung für ein flexibles Flächen­element 4 in Form eines Netzes und bilden eine trampo­linartige Aufnahmefläche 5 .
Somit ist es möglich, aus einer magazinierten Stauphase des Flächenelementes 4 gemäß Fig. 3 und 4 mit geringem Platzbedarf auf dem Marinefahrzeug 1 eine entsprechende große Aufnahmefläche 5 zu bilden und diese wieder in die ursprüngliche Lage zurückzubringen.In the illustrated embodiment, 1 holding and guiding elements in the form of a telescoping device 2 which can be extended to the rear are arranged in the rear region of a marine vehicle and can additionally be folded into the outer region via struts 3. These elements 2, 3 serve as a holder for a flexible surface element 4 in the form of a network and form a trampoline-like receiving surface 5.
It is thus possible, from a magazine-stowed stowage phase of the surface element 4 according to FIGS. 3 and 4 with a small space requirement on the marine vehicle 1, a corresponding one to form large receiving surface 5 and to bring it back into the original position.

Die Aufnahmefläche 5 ermöglicht es, einen relativ großen Landeplatz für eine Drohne 6 zu schaffen, um diese durch nicht näher dargestellte automatische oder ferngesteuerte Steueranordnungen und zusätzliche Hilfsmittel, wie einen Fallschirm, in der Bergungsphase aufzunehmen. Es ist somit keine punktgenaue Landung erforderlich und auch die Umweltbedingungen, wie Wel­lengang und Wind, können damit beherrscht werden.The receiving surface 5 makes it possible to create a relatively large landing site for a drone 6 in order to take it up by automatic or remote-controlled control arrangements (not shown) and additional aids, such as a parachute, in the recovery phase. Precise landing is therefore not necessary and environmental conditions such as waves and wind can also be controlled.

Claims (5)

1. Vorrichtung zum Bergen von unbemannten wiederver­wendbaren Flugkörpern (Drohnen) in der Rückfüh­rungsphase, wobei die Landephase durch automatische oder ferngesteuerte Steueranordnungen und zusätz­licher Hilfsmittel, wie Fallschirmbergesysteme, erfolgt, dadurch gekennzeichnet, daß an einem Fahrzeug (1) ein flexibles Flächenelement (4) aus einer zusammengezogenen, gefalteten und/oder ge­klappten magazinierten Stauphase über betätigbare Halte- und Führungselemente (2,3) zur Bildung einer trampolinartiger Aufnahmefläche (5) aufspannbar angeordnet ist.1. Device for recovering unmanned reusable missiles (drones) in the return phase, the landing phase being carried out by automatic or remote-controlled control arrangements and additional aids, such as parachute recovery systems, characterized in that a flexible surface element (4) is provided on a vehicle (1) a contracted, folded and / or folded magazine stowed phase is arranged so that it can be stretched over actuatable holding and guiding elements (2, 3) to form a trampoline-like receiving surface (5). 2. Vorrichtung nach Anspruch 1, dadurch gekennzeich­net, daß das flexible Flächenelement (4) aus einem Netzwerk gebildet ist.2. Device according to claim 1, characterized in that the flexible surface element (4) is formed from a network. 3. Vorrichtung nach Anspruch 1 oder 2, dadurch ge­kennzeichnet, daß die Halte- und Führungs­elemente (2,3) durch ausfahrbare Teleskopanord­nungen gebildet sind.3. Apparatus according to claim 1 or 2, characterized in that the holding and guiding elements (2, 3) are formed by extendable telescopic arrangements. 4. Vorrichtung nach einem der Ansprüche 1 bis 3, da­durch gekennzeichnet, daß für die Anordnung auf Schiffen die Halte- und Führungselemente (2,3) in den über das Heck hinausgehenden Bereich ausfahrbar angeordnet sind.4. Device according to one of claims 1 to 3, characterized in that for the arrangement on ships, the holding and guiding elements (2, 3) are arranged so that they can be extended into the area beyond the stern. 5. Vorrichtung nach einem der Ansprüche 1 bis 4, da­durch gekennzeichnet, daß die Halte- und Führungs­elemente (2,3) in Seiten- und Längsrichtung zur Ausbildung der Aufnahmefläche ausfahrbar und aus­klappbar angeordnet sind.5. Device according to one of claims 1 to 4, characterized in that the holding and guiding elements (2, 3) are arranged to be extendable and foldable in the lateral and longitudinal direction to form the receiving surface.
EP90104714A 1989-04-01 1990-03-13 Device for the recovery of unmanned reusable missiles Withdrawn EP0391095A1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE3910621A DE3910621A1 (en) 1989-04-01 1989-04-01 DEVICE FOR RECOVERING UNMANNED REUSABLE AIRCRAFT
DE3910621 1989-04-01

Publications (1)

Publication Number Publication Date
EP0391095A1 true EP0391095A1 (en) 1990-10-10

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EP90104714A Withdrawn EP0391095A1 (en) 1989-04-01 1990-03-13 Device for the recovery of unmanned reusable missiles

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US (1) US5109788A (en)
EP (1) EP0391095A1 (en)
DE (1) DE3910621A1 (en)
IL (1) IL93641A0 (en)

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IT201900006955A1 (en) * 2019-05-17 2020-11-17 Enzo Manca TELESCOPIC STRUCTURE FOR SUPPORTING AN ELASTIC OR SIMILAR NET FOR USE IN BOATS OR SIMILAR

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Also Published As

Publication number Publication date
IL93641A0 (en) 1990-12-23
DE3910621C2 (en) 1992-01-09
US5109788A (en) 1992-05-05
DE3910621A1 (en) 1990-10-04

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