EP1783451B1 - Projectile stabilisé par rotation - Google Patents

Projectile stabilisé par rotation Download PDF

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Publication number
EP1783451B1
EP1783451B1 EP06022695A EP06022695A EP1783451B1 EP 1783451 B1 EP1783451 B1 EP 1783451B1 EP 06022695 A EP06022695 A EP 06022695A EP 06022695 A EP06022695 A EP 06022695A EP 1783451 B1 EP1783451 B1 EP 1783451B1
Authority
EP
European Patent Office
Prior art keywords
projectile
artillery projectile
artillery
elements
target area
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.)
Not-in-force
Application number
EP06022695A
Other languages
German (de)
English (en)
Other versions
EP1783451A2 (fr
EP1783451A3 (fr
Inventor
Karl Kautzsch
Albrecht Reindler
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.)
Junghans Microtec GmbH
Original Assignee
Junghans Microtec GmbH
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 Junghans Microtec GmbH filed Critical Junghans Microtec GmbH
Publication of EP1783451A2 publication Critical patent/EP1783451A2/fr
Publication of EP1783451A3 publication Critical patent/EP1783451A3/fr
Application granted granted Critical
Publication of EP1783451B1 publication Critical patent/EP1783451B1/fr
Not-in-force legal-status Critical Current
Anticipated expiration legal-status Critical

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Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42—AMMUNITION; BLASTING
    • F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B10/00—Means for influencing, e.g. improving, the aerodynamic properties of projectiles or missiles; Arrangements on projectiles or missiles for stabilising, steering, range-reducing, range-increasing or fall-retarding
    • F42B10/32—Range-reducing or range-increasing arrangements; Fall-retarding means
    • F42B10/48—Range-reducing, destabilising or braking arrangements, e.g. impact-braking arrangements; Fall-retarding means, e.g. balloons, rockets for braking or fall-retarding
    • F42B10/50—Brake flaps, e.g. inflatable
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42—AMMUNITION; BLASTING
    • F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B10/00—Means for influencing, e.g. improving, the aerodynamic properties of projectiles or missiles; Arrangements on projectiles or missiles for stabilising, steering, range-reducing, range-increasing or fall-retarding
    • F42B10/60—Steering arrangements
    • F42B10/66—Steering by varying intensity or direction of thrust
    • F42B10/661—Steering by varying intensity or direction of thrust using several transversally acting rocket motors, each motor containing an individual propellant charge, e.g. solid charge

Definitions

  • the invention relates to a spin stabilized artillery projectile according to the preamble of claim 1.
  • Such a spin stabilized artillery projectile is from the DE 101 43 312 C1 and from DE 102 42 588 B4 known.
  • This artillery projectile has in its ogive a radially acting braking device, which serves to reduce the longitudinal shelf of the artillery projectile in a target area. This makes a 1D correction possible.
  • the storage area of an artillery projectile in a target area is elliptical, so it has a longitudinal axis and a transverse axis orthogonal thereto.
  • the longitudinal axis, i. the longitudinal tray is larger than the transverse axis, i. the cross shelf.
  • the braking device of the known spin-stabilized artillery projectile serves to reduce the large lengthwise deposit of the artillery projectile in the target area compared to the crossbeam and thus to improve the accuracy of the target accordingly.
  • the invention has for its object to provide a spin stabilized artillery projectile of the type mentioned, in which reduced by simple means and the cross-placement of the artillery projectile in the target area and thus the accuracy is improved accordingly.
  • the momentum elements can be provided in the ogive of the artillery projectile.
  • the pulse elements may be formed by the pyrotechnic force elements, which are associated with a front annular region of a hood covering the braking device, and by means of which the hood of the ogive of the artillery projectile can be abspengbar.
  • Such impulse elements in the form of pyrotechnic force elements are quoted in the opening paragraph DE 101 43 312 C1 described.
  • the pulse elements are provided on a ring element which is arranged between the projectile fuse and the projectile housing.
  • the impulse elements in the tail section i. in Base Bleed, the artillery projectile.
  • This device can be provided in the artillery projectile, so that there is a self-sufficient device and a self-sufficient artillery projectile. Another possibility is that this device is controlled by satellite.
  • a satellite-based control of a web-corrected spin-stabilized artillery projectile of the type mentioned, ie for the reduction of the longitudinal storage of the artillery projectile in a target area, is in the EP 1 103 779 B1 described, their disclosure content, which concerns the targeted activation of the impulse elements provided at the periphery of the artillery projectile in order to reduce the cross-placement of the artillery projectile in a target area, forms part of the present invention.
  • the web-correctable spin-stabilized artillery projectile according to the invention has the advantage that, with structurally simple means, in addition to the reduction of the longitudinal deposit, a reduction of the transverse placement of the artillery projectile in a target area is realized.
  • the reduction of the cross-shelf, i. the controlled page correction of the artillery projectile, carried out before the activation of the braking device for reducing the longitudinal storage of the artillery projectile in the target area because the page correction is faster in time as the braking device for reducing the longitudinal shelf is effective.
  • FIG. 1 shows longitudinally sectioned the front portion of a formation of the spin-stabilized artillery projectile 10 with a provided in its ogive 12 projectile detonator 14 and a provided in the ogive 12 braking device 16 which is centrifugally force adjustable by pyrotechnic force elements 18, which are associated with a front ring portion 20 of a hood 22.
  • the pyrotechnic force elements 18 form impulse elements 24 of the artillery projectile 10, which are arranged distributed uniformly on the circumference of the artillery projectile.
  • the braking device 16 serves to reduce the longitudinal storage of the artillery projectile 10 in a target area (see the Figures 3 and 4 ).
  • FIG. 4 is the target area 26 elliptical, ie with an elliptical edge 28, illustrated.
  • the limited by the elliptical edge 28 shelf 30 has a longitudinal axis A 0 and a transverse axis B 0 .
  • the braking device 16 results in a reduction of the longitudinal shelf, ie the longitudinal axis A 0 , to an amount A r .
  • a reduction of the transverse axis B 0 is not effected by the braking device 16 of the artillery projectile 10, ie by the braking device 16, the storage surface 30 is reduced to a storage surface 32 which is bounded by the edge line 34.
  • pulse elements 24 is obtained by appropriate activation of the corresponding pulse elements 24 in an artillery projectile 10 with braking device 16, a reduction of the cross-stock of the artillery projectile 10, ie a further reduction of the storage surface 32 to a storage area 36 through the Edge line 38 is limited.
  • the support surface 36 is determined in the x-direction by the longitudinal dimension A r and in the y-direction by the transverse dimension B r , wherein it is preferred if A r and B r are the same size, so that a circular support surface 36 results.
  • FIG. 2 clarifies a training of the artillery projectile 10 in one of FIG. 1 similar cutaway longitudinal sectional view, wherein the pulse elements 24 are provided on a ring member 40 in the circumferential direction uniformly distributed, the is arranged between the projectile fuze 14 and the projectile housing 42.
  • the pyrotechnic force elements 18 are used in this embodiment of the artillery projectile 10 only for blowing off the brake device 16 covering the hood 22nd
  • the impulse elements in the rear part (base bleed) of the artillery projectile 10 may be distributed evenly in the circumferential direction.
  • FIG. 3 is designated reference numeral 50 a Feuerleitrechner.
  • the fire control computer 50 determines the azimuth orientation, the elevation indicated by the double arrow 52, and the propellant power, ie, the theoretical exit velocity 54 for the ballistic trajectory 56 of the artillery projectile 10 into the target area, depending on the pre-enlightened direction and distance 44 from a gun 48 to a target 46 26th

Landscapes

  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Braking Arrangements (AREA)
  • Organic Low-Molecular-Weight Compounds And Preparation Thereof (AREA)
  • Steroid Compounds (AREA)

Claims (4)

  1. Projectile d'artillerie (10) à stabilisation gyroscopique comprenant une amorce de projectile (14) prévue dans son ogive (12) et un dispositif de freinage (16) prévu dans l'ogive (12) et exposé dans le sens radial pour réduire la déviation longitudinale (A0 ; Ar) du projectile d'artillerie (10) dans une région visée (26), caractérisé en ce que
    a) le projectile d'artillerie (10) présente un certain nombre d'éléments d'impulsion (24) distribués sur son pourtour, lesquels sont prévus pour réduire la déviation transversale (B0 ; Br) du projectile d'artillerie (10) dans la région visée (26),
    b) un élément d'impulsion (24) adapté pour réduire la déviation transversale (B0 ; Br) pouvant être activé de manière ciblée par le biais d'un dispositif qui interagit avec les éléments d'impulsion (24), lequel permet de déterminer la position angulaire rotative temporelle respective du projectile d'artillerie (10) et ainsi des éléments d'impulsion (24) espacés les uns des autres dans le sens du pourtour et
    c) les éléments d'impulsion (24) étant prévus sur un élément annulaire (40) qui est disposé entre l'amorce de projectile (14) et le boîtier de projectile (42).
  2. Projectile d'artillerie (10) selon la revendication 1, caractérisé en ce que les éléments d'impulsion (24) sont distribués régulièrement sur le pourtour de l'élément annulaire (40).
  3. Projectile d'artillerie (10) selon la revendication 1 ou 2, caractérisé en ce que le dispositif est prévu dans le projectile d'artillerie (10).
  4. Projectile d'artillerie (10) selon l'une des revendications précédentes, caractérisé en ce que le dispositif est commandé avec une assistance satellitaire.
EP06022695A 2005-11-03 2006-10-31 Projectile stabilisé par rotation Not-in-force EP1783451B1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE102005052474A DE102005052474B3 (de) 2005-11-03 2005-11-03 Drallstbilisiertes Artillerieprojektil

Publications (3)

Publication Number Publication Date
EP1783451A2 EP1783451A2 (fr) 2007-05-09
EP1783451A3 EP1783451A3 (fr) 2007-08-29
EP1783451B1 true EP1783451B1 (fr) 2008-12-17

Family

ID=37697820

Family Applications (1)

Application Number Title Priority Date Filing Date
EP06022695A Not-in-force EP1783451B1 (fr) 2005-11-03 2006-10-31 Projectile stabilisé par rotation

Country Status (5)

Country Link
US (1) US7360490B2 (fr)
EP (1) EP1783451B1 (fr)
AT (1) ATE418059T1 (fr)
DE (2) DE102005052474B3 (fr)
ES (1) ES2317401T3 (fr)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3035205B1 (fr) * 2015-04-20 2018-10-05 Roxel France Dispositif de correction de trajectoire d'un projectile et procede de correction de trajectoire
CN115358638A (zh) * 2022-10-19 2022-11-18 中国兵器科学研究院 一种火力分配方法、装置、电子设备及存储介质

Family Cites Families (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2809281C2 (de) * 1978-03-03 1984-01-05 Emile Jean Versailles Stauff Steuervorrichtung für ein Geschoß mit Eigendrehung
DE3546269C1 (de) * 1985-12-28 1987-08-13 Deutsche Forsch Luft Raumfahrt Flugkoerper
FR2686687B1 (fr) * 1987-04-22 1994-05-13 Thomson Brandt Armements Procede et dispositif de pilotage d'un projectile selon ses trois axes de roulis tangage et lacet.
EP0418636B1 (fr) * 1989-09-19 1993-12-29 DIEHL GMBH & CO. Projectile à trajectoire corrigé
DE4036166A1 (de) * 1990-11-14 1992-05-21 Diehl Gmbh & Co Bahnkorrigierbares projektil
US5456429A (en) * 1993-08-02 1995-10-10 Loral Corp. Thrust maneuver system
US5647558A (en) * 1995-02-14 1997-07-15 Bofors Ab Method and apparatus for radial thrust trajectory correction of a ballistic projectile
DE19957363A1 (de) * 1999-11-29 2001-05-31 Diehl Munitionssysteme Gmbh Verfahren zur zielbezogenen Korrektur einer ballistischen Flugbahn
DE10143312C1 (de) * 2001-09-04 2003-06-18 Diehl Munitionssysteme Gmbh Bremseinrichtung für ein bahnkorrigierbares drallstabilisiertes Artillerieprojektil
DE10242588B4 (de) * 2001-09-04 2005-06-30 Diehl Bgt Defence Gmbh & Co. Kg Bremseinrichtung für ein bahnkorrigierbares drallstabilisiertes Artillerieprojektil
WO2004031682A1 (fr) 2002-09-13 2004-04-15 Diehl Bgt Defence Gmbh & Co. Kg Dispositif de freinage pour projectile d'artillerie stabilisee par rotation a correction de trajectoire
US7121210B2 (en) * 2003-02-18 2006-10-17 Kdi Precision Products, Inc. Accuracy fuze for airburst cargo delivery projectiles

Also Published As

Publication number Publication date
US20070095238A1 (en) 2007-05-03
ATE418059T1 (de) 2009-01-15
DE102005052474B3 (de) 2007-07-12
US7360490B2 (en) 2008-04-22
EP1783451A2 (fr) 2007-05-09
DE502006002369D1 (de) 2009-01-29
EP1783451A3 (fr) 2007-08-29
ES2317401T3 (es) 2009-04-16

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