SE519764C2 - Canardfenaggregat - Google Patents

Canardfenaggregat

Info

Publication number
SE519764C2
SE519764C2 SE0003061A SE0003061A SE519764C2 SE 519764 C2 SE519764 C2 SE 519764C2 SE 0003061 A SE0003061 A SE 0003061A SE 0003061 A SE0003061 A SE 0003061A SE 519764 C2 SE519764 C2 SE 519764C2
Authority
SE
Sweden
Prior art keywords
projectile
canard
fin
resp
phenomena
Prior art date
Application number
SE0003061A
Other languages
English (en)
Swedish (sv)
Other versions
SE0003061D0 (sv
SE0003061L (sv
Inventor
Lennart Selin
Reijo Vesa
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
Priority to SE0003061A priority Critical patent/SE519764C2/sv
Publication of SE0003061D0 publication Critical patent/SE0003061D0/xx
Priority to CA002420625A priority patent/CA2420625C/en
Priority to US10/362,825 priority patent/US7147181B2/en
Priority to DE60110917T priority patent/DE60110917T2/de
Priority to EP01961527A priority patent/EP1313997B1/de
Priority to PCT/SE2001/001801 priority patent/WO2002018867A1/en
Priority to ES01961527T priority patent/ES2239157T3/es
Priority to AU2001282787A priority patent/AU2001282787A1/en
Priority to IL15463201A priority patent/IL154632A0/xx
Publication of SE0003061L publication Critical patent/SE0003061L/
Priority to ZA200301536A priority patent/ZA200301536B/en
Priority to NO20030920A priority patent/NO327585B1/no
Publication of SE519764C2 publication Critical patent/SE519764C2/sv

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
    • 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

Landscapes

  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Toys (AREA)
  • Medicines Containing Antibodies Or Antigens For Use As Internal Diagnostic Agents (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Lasers (AREA)
SE0003061A 2000-08-31 2000-08-31 Canardfenaggregat SE519764C2 (sv)

Priority Applications (11)

Application Number Priority Date Filing Date Title
SE0003061A SE519764C2 (sv) 2000-08-31 2000-08-31 Canardfenaggregat
IL15463201A IL154632A0 (en) 2000-08-31 2001-08-24 Canard fin unit
EP01961527A EP1313997B1 (de) 2000-08-31 2001-08-24 Stabilisierungsflosseneinheit
US10/362,825 US7147181B2 (en) 2000-08-31 2001-08-24 Canard fin unit
DE60110917T DE60110917T2 (de) 2000-08-31 2001-08-24 Stabilisierungsflosseneinheit
CA002420625A CA2420625C (en) 2000-08-31 2001-08-24 Canard fin unit
PCT/SE2001/001801 WO2002018867A1 (en) 2000-08-31 2001-08-24 Canard fin unit
ES01961527T ES2239157T3 (es) 2000-08-31 2001-08-24 Unidad de aleteado.
AU2001282787A AU2001282787A1 (en) 2000-08-31 2001-08-24 Canard fin unit
ZA200301536A ZA200301536B (en) 2000-08-31 2003-02-25 Canard fin unit.
NO20030920A NO327585B1 (no) 2000-08-31 2003-02-27 Nesefinneseksjon for artillerimissil

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
SE0003061A SE519764C2 (sv) 2000-08-31 2000-08-31 Canardfenaggregat

Publications (3)

Publication Number Publication Date
SE0003061D0 SE0003061D0 (sv) 2000-08-31
SE0003061L SE0003061L (sv) 2002-03-01
SE519764C2 true SE519764C2 (sv) 2003-04-08

Family

ID=20280832

Family Applications (1)

Application Number Title Priority Date Filing Date
SE0003061A SE519764C2 (sv) 2000-08-31 2000-08-31 Canardfenaggregat

Country Status (11)

Country Link
US (1) US7147181B2 (de)
EP (1) EP1313997B1 (de)
AU (1) AU2001282787A1 (de)
CA (1) CA2420625C (de)
DE (1) DE60110917T2 (de)
ES (1) ES2239157T3 (de)
IL (1) IL154632A0 (de)
NO (1) NO327585B1 (de)
SE (1) SE519764C2 (de)
WO (1) WO2002018867A1 (de)
ZA (1) ZA200301536B (de)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20230072799A1 (en) * 2021-09-03 2023-03-09 Raytheon Company Control surface restraining system for tactical flight vehicles

Families Citing this family (29)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB0111171D0 (en) * 2001-05-08 2001-06-27 Special Cartridge Company Ltd Projictile
US7226017B2 (en) * 2003-10-02 2007-06-05 Blevio Sr Henry L Aerodynamically stable, high-lift, vertical takeoff aircraft
US6948685B2 (en) 2003-10-27 2005-09-27 Hr Textron, Inc. Locking device with solenoid release pin
FR2864613B1 (fr) 2003-12-31 2006-03-17 Giat Ind Sa Dispositif de deploiement et d'entrainement de gouvernes d'un projectile
US7195197B2 (en) 2005-02-11 2007-03-27 Hr Textron, Inc. Techniques for controlling a fin with unlimited adjustment and no backlash
US7325769B1 (en) * 2005-02-25 2008-02-05 Honeywell International, Inc. Fast-pivot missile flight control surface
FR2891618B1 (fr) * 2005-10-05 2010-06-11 Giat Ind Sa Dispositif d'entrainement de gouvernes de projectile.
US7475846B2 (en) * 2005-10-05 2009-01-13 General Dynamics Ordnance And Tactical Systems, Inc. Fin retention and deployment mechanism
US7526988B2 (en) * 2006-05-11 2009-05-05 The Boeing Company Electromagnetic railgun projectile
FR2916268B1 (fr) * 2007-05-15 2010-09-10 Saint Louis Inst Projectile et procede de pilotage associe
US7849800B2 (en) * 2007-06-24 2010-12-14 Raytheon Company Hybrid spin/fin stabilized projectile
WO2010011245A2 (en) * 2008-05-20 2010-01-28 Raytheon Company Multi-caliber fuze kit and methods for same
KR101069246B1 (ko) * 2009-06-11 2011-10-04 국방과학연구소 날개 전개 장치 및 이를 구비하는 비행체 발사 장치
US8319164B2 (en) * 2009-10-26 2012-11-27 Nostromo, Llc Rolling projectile with extending and retracting canards
FR2955653A1 (fr) * 2010-01-28 2011-07-29 Nexter Munitions Dispositif de deploiement simultane de gouvernes d'un projectile
US8895908B2 (en) * 2010-04-07 2014-11-25 Bae Systems Information And Electronic Systems Integration Inc. Wing slot seal
US8933383B2 (en) * 2010-09-01 2015-01-13 The United States Of America As Represented By The Secretary Of The Army Method and apparatus for correcting the trajectory of a fin-stabilized, ballistic projectile using canards
EP2990356B1 (de) * 2010-12-03 2019-08-28 Salflex Polymers Ltd. Entfaltbare kraftstofftankablenkplatte und kraftstofftanksystem
CN102121512B (zh) * 2010-12-23 2013-03-27 江西洪都航空工业集团有限责任公司 交叉折叠翼传动装置
US9086258B1 (en) * 2013-02-18 2015-07-21 Orbital Research Inc. G-hardened flow control systems for extended-range, enhanced-precision gun-fired rounds
US9429402B2 (en) * 2013-04-24 2016-08-30 Simmonds Precision Products, Inc. Multi-stage drive mechanisms
US9724502B2 (en) * 2015-07-10 2017-08-08 Coloplast A/S Dilator and method for penile prosthetic implantation
US10308347B2 (en) * 2016-10-26 2019-06-04 Simmonds Precision Products, Inc. Wing tip aileron actuation system
US10942013B2 (en) * 2018-08-31 2021-03-09 Bae Systems Information And Electronic Systems Integration Inc. Guidance, navigation and control for ballistic projectiles
US11340052B2 (en) * 2019-08-27 2022-05-24 Bae Systems Information And Electronic Systems Integration Inc. Wing deployment initiator and locking mechanism
US11624594B1 (en) 2020-03-31 2023-04-11 Barron Associates, Inc. Device, method and system for extending range and improving tracking precision of mortar rounds
US11852211B2 (en) 2020-09-10 2023-12-26 Bae Systems Information And Electronic Systems Integration Inc. Additively manufactured elliptical bifurcating torsion spring
CN112829924B (zh) * 2020-12-31 2022-12-13 上海机电工程研究所 一种可伸缩式鸭舵机构
DE102021001038B4 (de) 2021-02-26 2023-01-19 Diehl Defence Gmbh & Co. Kg Luftfahrzeug mit Flügel-Klappmechanismus

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3114315A (en) * 1961-09-26 1963-12-17 William E Trump Dive brake
US4438893A (en) * 1973-08-10 1984-03-27 Sanders Associates, Inc. Prime power source and control for a guided projectile
DE4020897C2 (de) 1990-06-30 1993-11-11 Diehl Gmbh & Co Einrichtung zum Entriegeln und Ausschwenken der Ruderblätter eines Projektiles
US6186443B1 (en) * 1998-06-25 2001-02-13 International Dynamics Corporation Airborne vehicle having deployable wing and control surface
US6726147B1 (en) * 2003-05-15 2004-04-27 Moog Inc. Multi-function actuator, and method of operating same

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20230072799A1 (en) * 2021-09-03 2023-03-09 Raytheon Company Control surface restraining system for tactical flight vehicles
US12092436B2 (en) * 2021-09-03 2024-09-17 Raytheon Company Control surface restraining system for tactical flight vehicles

Also Published As

Publication number Publication date
US7147181B2 (en) 2006-12-12
WO2002018867A1 (en) 2002-03-07
AU2001282787A1 (en) 2002-03-13
EP1313997A1 (de) 2003-05-28
EP1313997B1 (de) 2005-05-18
ZA200301536B (en) 2004-02-25
SE0003061D0 (sv) 2000-08-31
SE0003061L (sv) 2002-03-01
DE60110917D1 (de) 2005-06-23
NO20030920L (no) 2003-04-28
DE60110917T2 (de) 2006-01-19
US20060071120A1 (en) 2006-04-06
CA2420625C (en) 2009-02-10
IL154632A0 (en) 2003-09-17
NO20030920D0 (no) 2003-02-27
ES2239157T3 (es) 2005-09-16
WO2002018867A8 (en) 2002-12-19
CA2420625A1 (en) 2002-03-07
NO327585B1 (no) 2009-08-24

Similar Documents

Publication Publication Date Title
SE519764C2 (sv) Canardfenaggregat
US7475846B2 (en) Fin retention and deployment mechanism
US10788297B2 (en) Artillery projectile with a piloted phase
US6186443B1 (en) Airborne vehicle having deployable wing and control surface
US7185847B1 (en) Winged vehicle with variable-sweep cantilevered wing mounted on a translating wing-support body
US6880780B1 (en) Cover ejection and fin deployment system for a gun-launched projectile
US3063375A (en) Folding fin
US8674278B2 (en) Control of projectiles or the like
CN108871103B (zh) 一种小型导弹折叠舵片的延时展开机构
US10323917B2 (en) Fin deployment mechanism for projectile and method for fin deployment
SE518657C2 (sv) Fenstabiliserad styrbar projektil
US3273500A (en) Self-erecting folding fin
US5240203A (en) Folding wing structure with a flexible cover
KR100187747B1 (ko) 전개 가능한 제어 핀들을 구비한 미사일
US10458764B2 (en) Canard stowage lock
US3695556A (en) Hinged stability and control fin assembly
US2925966A (en) Folding fin or wing for missiles
CN212458140U (zh) 筒式亚音速小型导弹
US7434762B2 (en) Retractable thrust vector control vane system and method
US3515360A (en) Pivot system for folding control surfaces
CN115962685B (zh) 折叠舵面锁定和展开机构及具有其的制导炮弹
CN114194377B (zh) 一种无人机机翼扭转展开结构
GB2265443A (en) Fin assembly for a projectile
CN118758118A (zh) 一种飞弹舵板折叠结构
CN116697824A (zh) 一种pgk折叠翼装置

Legal Events

Date Code Title Description
NUG Patent has lapsed