EP0443136A1 - Einrichtung zur Einstellung bzw. Ausrichtung einer Mine - Google Patents

Einrichtung zur Einstellung bzw. Ausrichtung einer Mine Download PDF

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Publication number
EP0443136A1
EP0443136A1 EP90124007A EP90124007A EP0443136A1 EP 0443136 A1 EP0443136 A1 EP 0443136A1 EP 90124007 A EP90124007 A EP 90124007A EP 90124007 A EP90124007 A EP 90124007A EP 0443136 A1 EP0443136 A1 EP 0443136A1
Authority
EP
European Patent Office
Prior art keywords
elastic force
active body
reference member
bolt element
force elements
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Withdrawn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
EP90124007A
Other languages
German (de)
English (en)
French (fr)
Inventor
Alfred Eckel
Gerald Rieger
Wolfgang Mosig
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 EP0443136A1 publication Critical patent/EP0443136A1/de
Withdrawn legal-status Critical Current

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Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42BEXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B23/00Land mines ; Land torpedoes
    • F42B23/24Details

Definitions

  • the invention relates to a device for setting or aligning a mine having an active body, the active body being provided in an articulated manner on a reference organ and being adjustable in relation to the reference organ adjacent to the active body.
  • DE-PS 23 36 040 describes a defense system with an accommodated in a container, consisting of several floors, an optical locating part and an actuator Horizontal and vertical gears existing launch unit, in which the individual functions are triggered by a command device.
  • the command device is part of the launch unit and consists of the locating part which can be controlled by a sensor and an evaluating part for evaluating the information supplied by the locating part about a moving object, for adjusting the actuator and for triggering an ignition device.
  • the reference organ is formed by a rod attached to a housing and by a tripod surrounding the rod with a plurality of tripod legs.
  • the articulated connection between the reference member and the multiple-storey active body is provided by the actuator, which has a number of joint parts, so that it is possible to adjust the active body in any desired directional position with respect to the reference member.
  • This defense system has a large number of interacting individual parts and thus has a relatively complex structure.
  • a mine in particular a land mine, which has an acceleration device at the installation site prior to the detonation of the mine explosive charge to ensure that it moves up to a predetermined height level.
  • a rocket engine with a spatially angularly movable connection in the form of a spherical shell joint between the combustion chamber and the thrust nozzle is used as an acceleration device.
  • a swivel device for the thrust nozzle is provided there, which is designed as a mechanical heavy pendulum with two diametrically opposite lever arms, the heavy pendulum engaging with the lever arm remote from the weight in the divergent thrust nozzle section.
  • the swivel device is in particular for aligning the active body Mine provided in the direction of the vertical.
  • a desired setting or alignment to an enemy target or target vehicle to be combated in a direction deviating from the vertical is there only to a limited extent or not possible.
  • this known mine also has a relatively complex structure.
  • the invention has for its object to provide a device of the type mentioned for setting or aligning a mine, which is very simple in design and structure compared to the known devices of the generic type, without thereby affecting the setting or Alignment of a mine provided with this device results.
  • a bolt element protrudes from the active body in the direction of the reference member, that at least two elastic force elements are provided, which are fastened with their one end section to the bolt member and are detachably arranged with their second end section in each case on an associated release part provided on the reference member , wherein the elastic force elements are provided at least approximately evenly distributed in the circumferential direction of the bolt element, and that another release part provided on the reference element is detachably connected to the bolt element.
  • the bolt element is preferably centrally away from the active body in the longitudinal direction thereof.
  • the elastic force elements can be spring elements, for example in the form of helical tension or helical compression springs. Of course, the elastic force elements can also be formed by other spring elements known per se.
  • the associated elastic force element on the bolt element is no longer effective, or only the at least one additional remaining elastic force element on the bolt element is effective, so that the state of equilibrium of the elastic force elements originally given on the bolt element is canceled.
  • the then no longer given state of equilibrium leads to a corresponding deflection of the bolt element in order to in turn form a state of equilibrium of the forces of the remaining elastic force elements on the bolt element after this specific deflection of the bolt element.
  • the elastic force elements are provided at least approximately evenly distributed in the circumferential direction of the bolt element results in a symmetrical distribution of forces on the bolt element both in the original initial state and the advantage that after releasing at least one release part and the resulting elimination of the force component of the associated elastic element Force element a problem-free adjustment of the bolt element and thus the active body of the mine is guaranteed.
  • the further release part detachably connected to the bolt element which is directly and immediately detachably connected to the bolt element without the interposition of an associated elastic force element, results in a good securing of the connection between the active body of the mine and the reference organ until this further release part is detached, which is preferably carried out simultaneously with the detachment of at least one further release part connected to an associated elastic force element, to adjust or align the active body of the mine as desired.
  • a number of elastic force elements are preferably at least approximately evenly spaced from the bolt element in a radial plane.
  • Three, four, six or another number of elastic force elements can be provided.
  • the number of elastic force elements is limited in particular by the reference organ.
  • a particularly simple design of the device results when four elastic force elements are provided.
  • a finer adjustment or alignment of a lead is possible, however, if instead of four uniformly distributed elastic force elements, for example six elastic force elements are provided in a uniformly distributed manner with respect to the bolt element.
  • the reference element for guiding the bolt element has a link with a number of longitudinal recesses corresponding to the number of elastic force elements, which are aligned in the direction of the elastic force elements and form a uniform radiation star.
  • the longitudinal recesses have clear cross-sectional dimensions which are adapted to the transverse dimensions of the bolt element, so that the bolt element, depending on which of the release parts is actuated to release the associated elastic force element, is guided in a linearly movable manner in one or the other longitudinal recess of the link formed in the reference element to adjust or align the active body as desired.
  • a space-saving design of the device is obtained if the elastic force elements are arranged in a radial star-shaped recess in the reference element, which is concentric with the backdrop and conforms to the angle.
  • Such a configuration of the device also results in protected accommodation of the elastic force elements, so that undesired impairment of the elastic force elements by external influences is eliminated.
  • Support arms with joints are preferably provided for the articulated connection of the active body of the mine and the reference element.
  • the support members can be telescopically extendable in at least approximately the radial direction of the reference member, in order in this way to be able to determine the pivoting range of the active body in relation to the reference member as desired.
  • the pivoting range of the active body with respect to the reference member is namely dependent on the length of the support members and on the longitudinal extent of the longitudinal recesses forming the link for the bolt element.
  • the active body of the mine is preferably connected to the supporting organs by means of a cardanic suspension.
  • FIG. 1 shows an active body 10 of a lead 12, drawn in sections, from whose underside 14 a bolt element 16 protrudes centrally in the axial direction.
  • a reference member 18 is provided at a distance from the underside 14 thereof and is connected to the active body 10 by means of support arms 20.
  • Each support arm 20 has a joint 22.
  • the support arms 20 can be made telescopically extendable with respect to the reference member 18.
  • the active body is gimbaled, for example, on a suspension (not shown).
  • the reference member 18 has cutouts 24 in a uniformly distributed manner, in which release parts 26 are arranged.
  • the reference member 18 is formed with a radial star-shaped recess 28, which is used to accommodate elastic force elements 30.
  • These elastic force elements 30 are, for example, coil tension springs.
  • the elastic force elements 30 are detachably connected with their one end section to the associated release parts 26, the second end sections of the elastic force elements 30 are fastened to the bolt element 16, which is cut in FIG. 2 and is therefore shown hatched. As can also be clearly seen from FIG.
  • the reference member 18 has a link 32 with a number of longitudinal recesses 34 corresponding to the number of elastic force elements 30, which are aligned in the direction of the elastic force elements 30 and one Form uniform beam star, which is concentric with the radial recess 28 for the elastic force elements 30 and conforms to the angle.
  • the bolt element 16 protruding from the active body 10 projects into the link 32, the longitudinal recesses 34 serving to linearly guide the bolt element 16 in one direction or the other.
  • the active body 10 of the mine 12 is drawn in the perpendicular "0 °" position. It can be adjusted and aligned with respect to the reference element 18 in one of the number of elastic force elements 30 and thus in a spatial direction corresponding to the number of longitudinal recesses 34 in the link 32.
  • the swivel range i.e. the swivel angle between the active body 10 and the reference member 18 from the position of the attachment, i.e. the pivot point on the active body 10 and thus on the length of the support arms 20 and on the formation of the backdrop, i.e. dependent on the radial longitudinal extent of the longitudinal recesses 34 of the link 32.
  • either one release part or three release parts 26 are pulled.
  • another release part 36 provided on the reference member 18 is pulled, so that on the one hand the connection between the associated one elastic force element 30 or the associated three elastic force element genes 30 and the corresponding release parts 26 and at the same time the connection between the bolt element 16 and the one that forms a fuse Reference organ 18 is canceled.
  • the remaining elastic force elements 30, ie the elastic elements that remain connected to corresponding release parts 26 Force elements 30 or the elastic force element 30 that remains connected leads to the fact that the now freely movable pin element 16 is moved into the appropriate longitudinal recess 34 of the link 32, with a desired pivoting of the active body 10 relative to the reference member 18 into the desired position.
  • At least one of the release parts 26 and the further release part 36 can be activated, for example, by means of an actuating device (not shown) which can be connected to a detector device (not shown) provided on the active body 10.

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Manipulator (AREA)
  • Orthopedics, Nursing, And Contraception (AREA)
  • Particle Accelerators (AREA)
EP90124007A 1990-02-21 1990-12-13 Einrichtung zur Einstellung bzw. Ausrichtung einer Mine Withdrawn EP0443136A1 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE4005403 1990-02-21
DE19904005403 DE4005403A1 (de) 1990-02-21 1990-02-21 Einrichtung zur einstellung bzw. ausrichtung einer mine

Publications (1)

Publication Number Publication Date
EP0443136A1 true EP0443136A1 (de) 1991-08-28

Family

ID=6400631

Family Applications (1)

Application Number Title Priority Date Filing Date
EP90124007A Withdrawn EP0443136A1 (de) 1990-02-21 1990-12-13 Einrichtung zur Einstellung bzw. Ausrichtung einer Mine

Country Status (2)

Country Link
EP (1) EP0443136A1 (enrdf_load_stackoverflow)
DE (1) DE4005403A1 (enrdf_load_stackoverflow)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE4220640C2 (de) * 1992-06-24 1994-06-01 Deutsche Aerospace Automatische Elevationsverstellung bei Richtminen
DE4220902C2 (de) * 1992-06-25 1994-07-07 Deutsche Aerospace Abwehrsystem mit einem Zielsensor zur Erfassung und Feuerleitung auf ein Ziel

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE263512C (enrdf_load_stackoverflow) *
DE3509281A1 (de) * 1985-03-15 1986-09-25 Messerschmitt-Bölkow-Blohm GmbH, 8012 Ottobrunn Vorrichtung zur ausrichtung eines wirkkoerpers
DE3517826A1 (de) * 1985-03-15 1987-01-22 Messerschmitt Boelkow Blohm Vorrichtung zur ausrichtung eines wirkkoerpers

Family Cites Families (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2336040C3 (de) * 1973-07-14 1980-06-19 Messerschmitt-Boelkow-Blohm Gmbh, 8000 Muenchen Abwehrsystem mit mehreren Geschossen
DE3509282C2 (de) * 1985-03-15 1987-01-15 Messerschmitt-Bölkow-Blohm GmbH, 8012 Ottobrunn Mine mit vertikaler oder horizontaler Wirkrichtung

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE263512C (enrdf_load_stackoverflow) *
DE3509281A1 (de) * 1985-03-15 1986-09-25 Messerschmitt-Bölkow-Blohm GmbH, 8012 Ottobrunn Vorrichtung zur ausrichtung eines wirkkoerpers
DE3517826A1 (de) * 1985-03-15 1987-01-22 Messerschmitt Boelkow Blohm Vorrichtung zur ausrichtung eines wirkkoerpers

Also Published As

Publication number Publication date
DE4005403C2 (enrdf_load_stackoverflow) 1991-12-12
DE4005403A1 (de) 1991-08-22

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