NO20034174D0 - Synkronisering av et artillerimissils halefinner, og missil med slike - Google Patents

Synkronisering av et artillerimissils halefinner, og missil med slike

Info

Publication number
NO20034174D0
NO20034174D0 NO20034174A NO20034174A NO20034174D0 NO 20034174 D0 NO20034174 D0 NO 20034174D0 NO 20034174 A NO20034174 A NO 20034174A NO 20034174 A NO20034174 A NO 20034174A NO 20034174 D0 NO20034174 D0 NO 20034174D0
Authority
NO
Norway
Prior art keywords
missile
synchronization
artillery
tail fins
fins
Prior art date
Application number
NO20034174A
Other languages
English (en)
Other versions
NO20034174L (no
NO327496B1 (no
Inventor
Stig Johnsson
Original Assignee
Bofors Defence Ab
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 Bofors Defence Ab filed Critical Bofors Defence Ab
Publication of NO20034174D0 publication Critical patent/NO20034174D0/no
Publication of NO20034174L publication Critical patent/NO20034174L/no
Publication of NO327496B1 publication Critical patent/NO327496B1/no

Links

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
    • F42B10/02—Stabilising arrangements
    • F42B10/14—Stabilising arrangements using fins spread or deployed after launch, e.g. after leaving the barrel
    • F42B10/16—Wrap-around 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
    • F42B10/14—Stabilising arrangements using fins spread or deployed after launch, e.g. after leaving the barrel

Landscapes

  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Toys (AREA)
  • Magnetic Bearings And Hydrostatic Bearings (AREA)
  • Powder Metallurgy (AREA)
  • Radar Systems Or Details Thereof (AREA)
  • Prostheses (AREA)
NO20034174A 2001-03-20 2003-09-19 Synkronisering av et artillerimissils halefinner, og missil med slike NO327496B1 (no)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
SE0100956A SE521445C2 (sv) 2001-03-20 2001-03-20 Sätt att synkronisera fenutfällningen vid en fenstabiliserad artillerigranat samt en i enlighet därmed utformad artillerigranat
PCT/SE2002/000550 WO2002079716A1 (en) 2001-03-20 2002-03-20 Method of synchronizing fin fold-out on a fin-stabilized artillery shell, and an artillery shell designed in accordance therewith

Publications (3)

Publication Number Publication Date
NO20034174D0 true NO20034174D0 (no) 2003-09-19
NO20034174L NO20034174L (no) 2003-11-10
NO327496B1 NO327496B1 (no) 2009-07-20

Family

ID=20283429

Family Applications (1)

Application Number Title Priority Date Filing Date
NO20034174A NO327496B1 (no) 2001-03-20 2003-09-19 Synkronisering av et artillerimissils halefinner, og missil med slike

Country Status (8)

Country Link
US (2) US7104497B2 (no)
EP (1) EP1370824B1 (no)
CA (1) CA2441277C (no)
IL (3) IL157972A0 (no)
NO (1) NO327496B1 (no)
SE (1) SE521445C2 (no)
WO (1) WO2002079716A1 (no)
ZA (1) ZA200306817B (no)

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CN104833276B (zh) * 2015-05-18 2016-09-14 中国船舶重工集团公司第七○二研究所 栅格翼同步展开机构
CN105129082B (zh) * 2015-09-01 2018-07-27 湖南云顶智能科技有限公司 用于无人机的螺旋桨收折装置
US10184762B2 (en) * 2015-12-01 2019-01-22 Raytheon Company Base drag reduction fairing using shape memory materials
FR3054030B1 (fr) * 2016-07-18 2018-08-24 Nexter Munitions Projectile comprenant un dispositif de deploiement d'une voilure ou ailette
US11555679B1 (en) 2017-07-07 2023-01-17 Northrop Grumman Systems Corporation Active spin control
US11578956B1 (en) 2017-11-01 2023-02-14 Northrop Grumman Systems Corporation Detecting body spin on a projectile
SE541598C2 (sv) 2017-11-10 2019-11-12 Bae Systems Bofors Ab Akterparti för en fenstabiliserad projektil
FR3089620B1 (fr) * 2018-12-11 2022-04-01 Nexter Munitions Projectile a plans de voilure deployables
DE102018133113A1 (de) * 2018-12-20 2020-06-25 Rheinmetall Air Defence Ag Lenkflugkörper mit mehreren mittels einer Antriebsanordnung drehbaren Flügeln mit mindestens einem Aktuator und mindestens einem Planetengetriebe
RU2704381C1 (ru) * 2019-02-12 2019-10-28 Акционерное общество "Военно-промышленная корпорация "Научно-производственное объединение машиностроения" Способ аэродинамического управления летательным аппаратом
US11573069B1 (en) 2020-07-02 2023-02-07 Northrop Grumman Systems Corporation Axial flux machine for use with projectiles

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SE432670B (sv) * 1979-09-27 1984-04-09 Kurt Andersson Sett att stabilisera en artilleriprojektil och i slutfasen korrigera dess bana och artilleriprojektil for genomforande av settet
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US6247666B1 (en) * 1998-07-06 2001-06-19 Lockheed Martin Corporation Method and apparatus for non-propulsive fin control in an air or sea vehicle using planar actuation
SE518665C2 (sv) * 2000-03-21 2002-11-05 Bofors Weapon Sys Ab Fenstabiliserad artillerigranat
DE10015514B4 (de) * 2000-03-30 2007-10-04 Rheinmetall Waffe Munition Gmbh Flügelstabilisiertes Geschoß
US6360987B1 (en) * 2000-05-23 2002-03-26 Bae Systems Integrated Defense Solutions Methods and apparatus for swash plate guidance and control
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SE519757C2 (sv) * 2000-08-15 2003-04-08 Bofors Defence Ab Styrbar artilleriprojektil med extremt lång skottvidd
US7086337B2 (en) * 2000-09-28 2006-08-08 Klein John M Non-lethal projectile ammunition
US6474594B1 (en) * 2001-05-11 2002-11-05 Raytheon Company Output shaft assembly for a missile control actuation unit
TW583264B (en) * 2001-09-26 2004-04-11 Nanya Plastics Corp Improved copolyester with improved extrusion processing and color for extrusion blow molding
US6571715B1 (en) * 2002-03-11 2003-06-03 Raytheon Company Boot mechanism for complex projectile base survival
US6761331B2 (en) * 2002-03-19 2004-07-13 Raytheon Company Missile having deployment mechanism for stowable fins
US6637699B2 (en) * 2002-03-25 2003-10-28 Lockheed Martin Corporation Method and apparatus for controlling a trajectory of a projectile
ES2238107B1 (es) * 2002-06-13 2006-11-01 Iñigo Echenique Gordillo Sistema de estabilizadores integrados para buques.
US6869043B1 (en) * 2003-03-24 2005-03-22 At&T Corp. Deployable flare with simplified design
US6921052B2 (en) * 2003-11-28 2005-07-26 The United States Of America As Represented By The Secretary Of The Army Dragless flight control system for flying objects

Also Published As

Publication number Publication date
US7487934B2 (en) 2009-02-10
US20070114323A1 (en) 2007-05-24
US7104497B2 (en) 2006-09-12
IL181105A (en) 2009-07-20
SE0100956D0 (sv) 2001-03-20
NO20034174L (no) 2003-11-10
CA2441277A1 (en) 2002-10-10
CA2441277C (en) 2009-06-09
NO327496B1 (no) 2009-07-20
EP1370824B1 (en) 2017-05-03
SE0100956L (sv) 2002-09-21
IL157972A (en) 2009-07-20
SE521445C2 (sv) 2003-11-04
IL181105A0 (en) 2007-07-04
IL157972A0 (en) 2004-03-28
EP1370824A1 (en) 2003-12-17
US20050229806A1 (en) 2005-10-20
WO2002079716A1 (en) 2002-10-10
ZA200306817B (en) 2004-09-01

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