ES2543196T3 - Procedimiento para el aumento del alcance de una granada de calibre reducido, y granadas de calibre reducido de largo alcance - Google Patents
Procedimiento para el aumento del alcance de una granada de calibre reducido, y granadas de calibre reducido de largo alcance Download PDFInfo
- Publication number
- ES2543196T3 ES2543196T3 ES06784176.7T ES06784176T ES2543196T3 ES 2543196 T3 ES2543196 T3 ES 2543196T3 ES 06784176 T ES06784176 T ES 06784176T ES 2543196 T3 ES2543196 T3 ES 2543196T3
- Authority
- ES
- Spain
- Prior art keywords
- grenade
- grenades
- reduced caliber
- fins
- procedure
- 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
Links
- 239000002360 explosive Substances 0.000 abstract 1
- 239000000126 substance Substances 0.000 abstract 1
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B14/00—Projectiles or missiles characterised by arrangements for guiding or sealing them inside barrels, or for lubricating or cleaning barrels
- F42B14/06—Sub-calibre projectiles having sabots; Sabots therefor
- F42B14/064—Sabots enclosing the rear end of a kinetic energy projectile, i.e. having a closed disk shaped obturator base and petals extending forward from said base
-
- 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
- F42B10/38—Range-increasing arrangements
-
- 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
- F42B10/02—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
- F42B10/32—Range-reducing or range-increasing arrangements; Fall-retarding means
- F42B10/38—Range-increasing arrangements
- F42B10/40—Range-increasing arrangements with combustion of a slow-burning charge, e.g. fumers, base-bleed projectiles
-
- 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
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
- Toys (AREA)
- Drilling And Exploitation, And Mining Machines And Methods (AREA)
- Cold Cathode And The Manufacture (AREA)
- Mechanical Coupling Of Light Guides (AREA)
- Forging (AREA)
Abstract
Procedimiento para aumentar el alcance de granadas (1, 8, 13) cargadas con una sustancia explosiva o dotadas de alguna otra carga útil activa, por lo que las granadas (1, 8, 13) por una parte, se fabrican de calibre reducido y están dotadas de aletas de guía posteriores fijas (5, 10), en las que la envergadura o extensión radial de las aletas de guía posteriores fijas no excede el espacio disponible entre el exterior del cuerpo envolvente de la granada respectiva (1, 8, 13) y el interior del cañón de una pieza de artillería utilizada para disparar la granada (1, 8, 13) y, por otra parte, están dotadas de aletas tipo canard delanteras orientables no retráctiles (6, 9), en las que la envergadura o extensión radial de las aletas tipo canard (6, 9) no excede el espacio disponible entre el exterior del respectivo cuerpo envolvente de la granada (1, 8, 13) y el interior del cañón de una pieza de artillería utilizada para disparar la granada (1, 8, 13), cuyas aletas posteriores y delanteras (5, 6, 9, 10) proporcionan conjuntamente a la granada (1, 8, 13) superficies de apoyo aerodinámico principalmente durante la parte final de su trayectoria, y porque las granadas de calibre reducido (1, 8, 13) son disparadas desde la pieza de artillería respectiva con espejos de propulsión (2) adaptados con este objetivo.
Description
Claims (1)
-
imagen1
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
SE0502509A SE0502509L (sv) | 2005-11-15 | 2005-11-15 | Underkalibrerad granat med lång räckvidd |
SE0502509 | 2005-11-15 | ||
PCT/SE2006/001047 WO2007058573A2 (en) | 2005-11-15 | 2006-09-14 | Method of increasing the range of a subcalibre shell and subcalibre shells with long range |
Publications (2)
Publication Number | Publication Date |
---|---|
ES2543196T3 true ES2543196T3 (es) | 2015-08-17 |
ES2543196T5 ES2543196T5 (es) | 2022-12-02 |
Family
ID=37596400
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
ES06784176T Active ES2543196T5 (es) | 2005-11-15 | 2006-09-14 | Método de aumento del alcance de un obús de calibre reducido y obuses de calibre reducido de largo alcance |
Country Status (6)
Country | Link |
---|---|
US (1) | US8097838B2 (es) |
EP (1) | EP1949019B2 (es) |
ES (1) | ES2543196T5 (es) |
IL (1) | IL191446A (es) |
SE (1) | SE0502509L (es) |
WO (1) | WO2007058573A2 (es) |
Families Citing this family (17)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB0803282D0 (en) | 2008-02-22 | 2008-04-02 | Qinetiq Ltd | Control of projectiles or the like |
US20110197549A1 (en) * | 2010-02-15 | 2011-08-18 | Illinois Tool Works Inc. | Method and apparatus for compressing and holding in compression woven fabric articles |
US8640589B2 (en) | 2010-07-20 | 2014-02-04 | Raytheon Company | Projectile modification method |
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 |
RU2458316C1 (ru) * | 2011-02-22 | 2012-08-10 | Открытое акционерное общество "Государственное машиностроительное конструкторское бюро "Вымпел" им. И.И. Торопова" | Складной руль управляемой ракеты |
SE535991C2 (sv) * | 2011-07-07 | 2013-03-19 | Bae Systems Bofors Ab | Rotationsstabiliserad styrbar projektil och förfarande därför |
US9086258B1 (en) | 2013-02-18 | 2015-07-21 | Orbital Research Inc. | G-hardened flow control systems for extended-range, enhanced-precision gun-fired rounds |
US9759535B2 (en) * | 2014-04-30 | 2017-09-12 | Bae Systems Land & Armaments L.P. | Gun launched munition with strakes |
US9724502B2 (en) * | 2015-07-10 | 2017-08-08 | Coloplast A/S | Dilator and method for penile prosthetic implantation |
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 |
US10480916B1 (en) | 2017-09-07 | 2019-11-19 | Gregory Saltz | Low-observable projectile |
US11578956B1 (en) | 2017-11-01 | 2023-02-14 | Northrop Grumman Systems Corporation | Detecting body spin on a projectile |
US11573069B1 (en) | 2020-07-02 | 2023-02-07 | Northrop Grumman Systems Corporation | Axial flux machine for use with projectiles |
CN113899255B (zh) * | 2021-08-31 | 2024-04-09 | 北京航空航天大学 | 一种带控制舱段和滑翔增程舱段的精确控制火箭 |
UA153114U (uk) * | 2022-09-05 | 2023-05-24 | Володимир Миколайович Ярошок | Ракетоплан |
Family Cites Families (27)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
BE526652A (es) | 1953-12-10 | |||
US3038382A (en) | 1958-09-26 | 1962-06-12 | William R Noyes | Bore riders for launching of projectiles |
US5439188A (en) * | 1964-09-04 | 1995-08-08 | Hughes Missile Systems Company | Control system |
US4438893A (en) | 1973-08-10 | 1984-03-27 | Sanders Associates, Inc. | Prime power source and control for a guided projectile |
US4336914A (en) * | 1978-12-29 | 1982-06-29 | The Commonwealth Of Australia | Deployable wing mechanism |
DE3719768A1 (de) | 1987-06-13 | 1988-12-22 | Rheinmetall Gmbh | Unterkalibriges fluegelstabilisiertes geschoss |
US4826105A (en) * | 1988-02-08 | 1989-05-02 | Rockwell International Corporation | Missile fin unfolding device |
DE3928965A1 (de) | 1989-09-01 | 1991-03-14 | Rheinmetall Gmbh | Tandem-geschossanordnung |
DE3932952A1 (de) | 1989-10-03 | 1991-04-11 | Rheinmetall Gmbh | Wuchtgeschoss |
DE3940969C2 (de) | 1989-12-12 | 1995-01-05 | Rheinmetall Gmbh | Unterkalibriges Wuchtgeschoß |
DE19617221C2 (de) * | 1996-04-30 | 1999-07-01 | Diehl Stiftung & Co | Als Mörsergeschoß verbringbares Lenkprojektil |
US6126109A (en) * | 1997-04-11 | 2000-10-03 | Raytheon Company | Unlocking tail fin assembly for guided projectiles |
FR2768809B1 (fr) * | 1997-09-24 | 1999-10-15 | Giat Ind Sa | Projectile d'artillerie de campagne de gros calibre a longue portee |
SE518665C2 (sv) * | 2000-03-21 | 2002-11-05 | Bofors Weapon Sys Ab | Fenstabiliserad artillerigranat |
SE518657C2 (sv) * | 2000-07-03 | 2002-11-05 | Bofors Defence Ab | Fenstabiliserad styrbar projektil |
SE518654C2 (sv) * | 2000-07-03 | 2002-11-05 | Bofors Defence Ab | Sätt och anordning vid artilleriprojektiler |
SE518656C2 (sv) * | 2000-07-03 | 2002-11-05 | Bofors Defence Ab | Fenstabiliserad artillerigranat |
SE519757C2 (sv) * | 2000-08-15 | 2003-04-08 | Bofors Defence Ab | Styrbar artilleriprojektil med extremt lång skottvidd |
ITMI20010648A1 (it) | 2001-03-27 | 2002-09-27 | Finmeccanica S P A Alenia Dife | Gruppo di controllo per alette direzionali di missili e/o proiettili |
DE10130383A1 (de) * | 2001-06-23 | 2003-01-09 | Diehl Munitionssysteme Gmbh | Artillerie-Projektil mit austauschbarer Nutzlast |
US6588700B2 (en) | 2001-10-16 | 2003-07-08 | Raytheon Company | Precision guided extended range artillery projectile tactical base |
DE10162136B4 (de) * | 2001-12-18 | 2004-10-14 | Diehl Munitionssysteme Gmbh & Co. Kg | Aus einem Rohr zu verschießender Flugkörper mit überkalibrigem Leitwerk |
US6880780B1 (en) * | 2003-03-17 | 2005-04-19 | General Dynamics Ordnance And Tactical Systems, Inc. | Cover ejection and fin deployment system for a gun-launched projectile |
US6869044B2 (en) * | 2003-05-23 | 2005-03-22 | Raytheon Company | Missile with odd symmetry tail fins |
IL156739A0 (en) | 2003-07-02 | 2009-02-11 | Elta Systems Ltd | Method and system for destroying rockets |
US7255304B2 (en) | 2003-12-08 | 2007-08-14 | General Dynamics Ordnance And Tactical Systems, Inc. | Tandem motor actuator |
US8058597B2 (en) * | 2009-05-06 | 2011-11-15 | Raytheon Company | Low cost deployment system and method for airborne object |
-
2005
- 2005-11-15 SE SE0502509A patent/SE0502509L/xx unknown
-
2006
- 2006-09-14 WO PCT/SE2006/001047 patent/WO2007058573A2/en active Application Filing
- 2006-09-14 US US12/093,220 patent/US8097838B2/en active Active
- 2006-09-14 ES ES06784176T patent/ES2543196T5/es active Active
- 2006-09-14 EP EP06784176.7A patent/EP1949019B2/en active Active
-
2008
- 2008-05-14 IL IL191446A patent/IL191446A/en active IP Right Grant
Also Published As
Publication number | Publication date |
---|---|
EP1949019B2 (en) | 2022-10-12 |
EP1949019B1 (en) | 2015-04-22 |
WO2007058573A3 (en) | 2008-03-20 |
IL191446A (en) | 2012-01-31 |
WO2007058573A2 (en) | 2007-05-24 |
SE528624C2 (sv) | 2007-01-09 |
US8097838B2 (en) | 2012-01-17 |
SE0502509L (sv) | 2007-01-09 |
EP1949019A2 (en) | 2008-07-30 |
US20090090809A1 (en) | 2009-04-09 |
EP1949019A4 (en) | 2011-07-06 |
ES2543196T5 (es) | 2022-12-02 |
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