EP1930686B1 - Drallstabilisierte bahnkorrigierbare Artilleriemunition - Google Patents

Drallstabilisierte bahnkorrigierbare Artilleriemunition Download PDF

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Publication number
EP1930686B1
EP1930686B1 EP07023111A EP07023111A EP1930686B1 EP 1930686 B1 EP1930686 B1 EP 1930686B1 EP 07023111 A EP07023111 A EP 07023111A EP 07023111 A EP07023111 A EP 07023111A EP 1930686 B1 EP1930686 B1 EP 1930686B1
Authority
EP
European Patent Office
Prior art keywords
artillery
canard
steering unit
munition
generator
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.)
Active
Application number
EP07023111A
Other languages
German (de)
English (en)
French (fr)
Other versions
EP1930686A1 (de
Inventor
Klaus Bär
Karl Kautzsch
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 Defence GmbH and Co KG
Original Assignee
Diehl BGT Defence GmbH and Co KG
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 BGT Defence GmbH and Co KG filed Critical Diehl BGT Defence GmbH and Co KG
Priority to PL07023111T priority Critical patent/PL1930686T3/pl
Publication of EP1930686A1 publication Critical patent/EP1930686A1/de
Application granted granted Critical
Publication of EP1930686B1 publication Critical patent/EP1930686B1/de
Active 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
    • F42B10/60—Steering arrangements
    • F42B10/62—Steering by movement of flight surfaces
    • F42B10/64—Steering by movement of flight surfaces of fins
    • 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
    • F42B10/02—Stabilising arrangements
    • F42B10/26—Stabilising arrangements using spin

Definitions

  • the invention relates to an artillery ammunition according to the preamble of the main claim.
  • Such a device is from the DE 1 01 34 785 A1 known.
  • This in itself unguided artillery ammunition is characterized by, with a single uniaxial pair of steering canards, so with only a two-dimensional control system, perform a spatial (ie three-dimensional) path correction and thereby the intrinsically systemic inherent delivery error in all directions to narrow targeted decisively ,
  • the opposite of the ammunition longitudinal axis electromotorically engageable Canarderiel on the steering unit, the uncoupled from ammunition body tapered front end of the artillery ammunition, depending on their sensory detected instantaneous position in space a pitch or yaw movement of artillery ammunition.
  • these two Canard wings for their employment with respect to the ammunition longitudinal axis via a common transverse to the ammunition longitudinal axis through the steering unit extending through Canardwelle which is rotatable by means of a single servomotor.
  • the electrical energy for the operation of this servomotor is obtained via the relative speed between ammunition body and steering unit in a generator which supplies the servomotor directly and / or via an energy store.
  • the generator operation represents a mechanical resistance to the rolling motion due to the mass moment of inertia of the projectile body.
  • a termination of the operation of the servomotor is compared to the load case, a relief of the generator and accordingly affects the effective between the stator and the rotor of the generator reaction torque, which in turn repercussions the momentary roll behavior of artillery ammunition and thus theirs Flight stability has. Therefore, the energy currently not required by the actuator motor is switched to a surplus load to avoid such repercussions on the rolling behavior as possible by constant load on the generator.
  • the present invention is based on the technical problem of designing an artillery ammunition of the generic type in such a way that the load-related heat radiation does not lead to critical heating in the steering unit.
  • the substitute load to which the generator in the roll decoupling engagement region of the Canard steering unit of a roll-stabilized railway-correctable artillery ammunition can be switched to avoid load fluctuations at the operating end of the servomotor, as electrical resistance or designed in Canard vom behind the leading edges, and preferably in non-adjustable mounted Entdrallcanards.
  • the spin-stabilized artillery ammunition 11 to be moved is equipped with a steering unit 13 in front of the ammunition body 12 receiving the payload, instead of a conventional impact, time or proximity detonator.
  • The is equipped behind their radome 14 with sensor devices 15 for trajectory monitoring and target approach, but above all also with a control system 16 for trajectory control.
  • a servomotor 17 acts in this example case the only control shaft 18 of a single-axis Canard control system 16, which extends transversely to the longitudinal axis 19 of the artillery ammunition 11 through the hollow conically configured steering unit 13 therethrough. With its two ends, the control shaft 18 is rotatably connected to a respective Canard control wing, the diametrically opposite each other from the outer contour of the steering unit 13 radially - but not überkalibrig - protrude.
  • the steering unit 13 is roll-coupled via axially staggered, preferably designed as bearings, bearings 20 from the ammunition body 12, in which it engages with a rear pipe stub.
  • This engagement region of the steering unit 13 including its conical area in front of the adjusting shaft 18, with respect to the ammunition body 12 leads a job of Canard wings against the ammunition longitudinal axis 19 by turning its control shaft 18 to a web change due Pitching and / or yawing movement of the artillery ammunition 11.
  • To control this setting process dynamically, is transverse to Pair of Canard wings a pair of Entdrallcanards 21 attached to the steering unit 13.
  • This speed difference is used in an electrodynamic generator 22 for obtaining electrical energy, in particular for the operation of the servomotor 17, but also for the sensor devices 15, for example.
  • the ammunition body 12 between the bearings 20 along a concentric to the axis 19 circle with mutually spaced, alternately poled permanent magnet 23 is fitted. Due to the relative rotation between ammunition body 12 and steering unit 13 pass through their induction coils 24, a magnetic alternating field and provide so without the requirement of slip rings a high-frequency AC voltage to a voltage conditioning circuit 25 with rectification inside the generator 22 supporting pipe socket of the steering unit 13.
  • a small-sized energy store 26 can be recharged or buffered; but above all is connected to the voltage conditioning circuit 25, the control system 16 with its Canard servomotor 17.
  • the respective Canarderiel 21 substantially or entirely of electrically conductive material (for example, from appropriately adjusted plastic), for example, by an insignificant in the drawing insulating barrier 31 a sufficiently large resistance of this replacement load 28 sufficiently long current path is enforced.
  • the heat generated in the reserve load 28 does not additionally burden the heat balance in the interior of the steering unit 13 and does not have to be dissipated specifically from the interior of the steering unit 13 - but is generated just outside the steering unit 13 and via the heavily impinged canard surfaces 30 is disposed of most effectively.

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  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Power Steering Mechanism (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Analysing Materials By The Use Of Radiation (AREA)
  • Particle Formation And Scattering Control In Inkjet Printers (AREA)
  • Pinball Game Machines (AREA)
  • Saccharide Compounds (AREA)
  • Lasers (AREA)
  • Cosmetics (AREA)
  • Medicinal Preparation (AREA)
  • Feeding And Controlling Fuel (AREA)
EP07023111A 2006-12-05 2007-11-29 Drallstabilisierte bahnkorrigierbare Artilleriemunition Active EP1930686B1 (de)

Priority Applications (1)

Application Number Priority Date Filing Date Title
PL07023111T PL1930686T3 (pl) 2006-12-05 2007-11-29 Stabilizowany ruchem obrotowym pocisk artyleryjski z korekcją toru

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE102006057229A DE102006057229B9 (de) 2006-12-05 2006-12-05 Drallstabilisierte bahnkorrigierbare Artilleriemunition

Publications (2)

Publication Number Publication Date
EP1930686A1 EP1930686A1 (de) 2008-06-11
EP1930686B1 true EP1930686B1 (de) 2009-02-04

Family

ID=39140758

Family Applications (1)

Application Number Title Priority Date Filing Date
EP07023111A Active EP1930686B1 (de) 2006-12-05 2007-11-29 Drallstabilisierte bahnkorrigierbare Artilleriemunition

Country Status (6)

Country Link
US (1) US7584922B2 (pl)
EP (1) EP1930686B1 (pl)
AT (1) ATE422231T1 (pl)
DE (2) DE102006057229B9 (pl)
ES (1) ES2320708T3 (pl)
PL (1) PL1930686T3 (pl)

Families Citing this family (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7696459B2 (en) * 2007-06-12 2010-04-13 Hr Textron, Inc. Techniques for articulating a nose member of a guidable projectile
US7791007B2 (en) * 2007-06-21 2010-09-07 Woodward Hrt, Inc. Techniques for providing surface control to a guidable projectile
WO2010011245A2 (en) * 2008-05-20 2010-01-28 Raytheon Company Multi-caliber fuze kit and methods for same
US8319163B2 (en) * 2008-07-09 2012-11-27 Bae Systems Land & Armaments, L.P. Roll isolation bearing
US9939238B1 (en) 2009-11-09 2018-04-10 Orbital Research Inc. Rotational control actuation system for guiding projectiles
DE102010004820A1 (de) * 2010-01-15 2011-07-21 Rheinmetall Air Defence Ag Verfahren zur Flugbahnkorrektur eines insbesondere endphasengelenkten Geschosses sowie Geschoss zur Durchführung des Verfahrens
IL207800B (en) 2010-08-25 2018-12-31 Bae Systems Rokar Int Ltd Control apparatus for guiding a cannon shell in flight and method of using same
SE535991C2 (sv) * 2011-07-07 2013-03-19 Bae Systems Bofors Ab Rotationsstabiliserad styrbar projektil och förfarande därför
KR101413498B1 (ko) * 2011-11-09 2014-07-01 최용준 유도무기용 디커플링 베어링모듈
FR3041744B1 (fr) * 2015-09-29 2018-08-17 Nexter Munitions Projectile d'artillerie ayant une phase pilotee.
US11555679B1 (en) 2017-07-07 2023-01-17 Northrop Grumman Systems Corporation Active spin control
US12031802B2 (en) 2017-07-26 2024-07-09 Northrop Grumman Systems Corporation Despun wing control system for guided projectile maneuvers
US11578956B1 (en) 2017-11-01 2023-02-14 Northrop Grumman Systems Corporation Detecting body spin on a projectile
DE102018004510B4 (de) * 2018-06-07 2020-06-18 Diehl Defence Gmbh & Co. Kg Munition mit einer Vorrichtung zur Erzeugung eines Entsicherungskriteriums für einen Zünder der Munition
US10928169B2 (en) * 2019-02-07 2021-02-23 Bae Systems Rokar International Ltd. Seal for a projectile guiding kit
US11573069B1 (en) 2020-07-02 2023-02-07 Northrop Grumman Systems Corporation Axial flux machine for use with projectiles
IL285727A (en) * 2021-08-19 2024-09-01 Elbit Systems Rokar Ltd Testing and data transfer to artillery guiding kits
US12313389B1 (en) 2022-03-11 2025-05-27 Northrop Grumman Systems Corporation Tunable safe and arming devices and methods of manufacture

Family Cites Families (26)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3156433A (en) * 1962-01-10 1964-11-10 Jr Edward A White Magnetohydrodynamic generator
US4142696A (en) * 1962-02-27 1979-03-06 Novatronics, Inc. Guidance devices
IL29535A (en) * 1968-02-27 1973-06-29 Popper J A delay fuse including a turbine
US3606207A (en) * 1968-03-08 1971-09-20 Nuclear Materials & Equipment Reentry vehicle for thermoelectric generator
CH539262A (de) * 1971-06-03 1973-07-15 Oerlikon Buehrle Ag Elektromagnetischer Generator für einen Drallgeschosszünder
US3826193A (en) * 1973-02-16 1974-07-30 Kongsberg Vapenfab As Method for supporting a rotating body in generators for missiles and a supporting arrangement for supporting such bodies
US4568039A (en) * 1973-08-10 1986-02-04 Sanders Associates, Inc. Guidance system for a projectile
CH578723A5 (pl) * 1974-05-10 1976-08-13 Oerlikon Buehrle Ag
CH589839A5 (pl) * 1975-03-14 1977-07-15 Oerlikon Buehrle Ag
US4004519A (en) * 1976-04-12 1977-01-25 The United States Of America As Represented By The Secretary Of The Navy Projectile power generator
NO140947C (no) * 1977-12-21 1979-12-12 Kongsberg Vapenfab As Kombinasjonstennroer for missiler.
US4577116A (en) * 1983-11-14 1986-03-18 The Boeing Company System for providing electrical energy to a missile and the like
US4665332A (en) * 1986-05-20 1987-05-12 Seti, Inc. Electric generator assembly for a projectile
DE3742836C1 (de) * 1987-12-17 1989-07-13 Messerschmitt Boelkow Blohm Flugkoerper mit verstellbaren Steuerorganen
DE3827590A1 (de) * 1988-08-13 1990-02-22 Messerschmitt Boelkow Blohm Flugkoerper
US5115742A (en) * 1991-06-24 1992-05-26 United States Of America As Represented By The Secretary Of The Navy Integrated and mechanically aided warhead arming device
US5452864A (en) * 1994-03-31 1995-09-26 Alliant Techsystems Inc. Electro-mechanical roll control apparatus and method
DE19839636A1 (de) * 1998-08-31 2000-03-02 Asea Brown Boveri Kraftwerk mit einem von einer Turbine angetriebenen Generator sowie Verfahren zum Betrieb eines solchen Kraftwerkes
DE10134785A1 (de) * 2001-07-17 2003-02-06 Diehl Munitionssysteme Gmbh Verfahren zur Flugbahnkorrektur ballistisch verschossener drallstabilisierter Artilleriemunition
US6845714B1 (en) * 2003-06-16 2005-01-25 The United States Of America As Represented By The Secretary Of The Army On-board power generation system for a guided projectile
DE10341713B3 (de) * 2003-09-10 2005-06-09 Diehl Bgt Defence Gmbh & Co. Kg Drallstabilisiertes Artillerieprojektil mit einem Generator
US6981672B2 (en) * 2003-09-17 2006-01-03 Aleiant Techsystems Inc. Fixed canard 2-D guidance of artillery projectiles
US7109679B2 (en) * 2004-03-09 2006-09-19 Hr Textron, Inc. Damping for electromechanical actuators
US7095193B2 (en) * 2004-05-19 2006-08-22 Hr Textron, Inc. Brushless DC motors with remote Hall sensing and methods of making the same
US7116100B1 (en) * 2005-03-21 2006-10-03 Hr Textron, Inc. Position sensing for moveable mechanical systems and associated methods and apparatus
US7431237B1 (en) * 2006-08-10 2008-10-07 Hr Textron, Inc. Guided projectile with power and control mechanism

Also Published As

Publication number Publication date
PL1930686T3 (pl) 2009-07-31
ATE422231T1 (de) 2009-02-15
EP1930686A1 (de) 2008-06-11
DE102006057229B9 (de) 2009-03-19
US7584922B2 (en) 2009-09-08
DE102006057229B4 (de) 2008-12-04
DE502007000419D1 (de) 2009-03-19
DE102006057229A1 (de) 2008-06-19
US20080302906A1 (en) 2008-12-11
ES2320708T3 (es) 2009-05-27

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