IL265487B2 - bullet - Google Patents

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Info

Publication number
IL265487B2
IL265487B2 IL265487A IL26548719A IL265487B2 IL 265487 B2 IL265487 B2 IL 265487B2 IL 265487 A IL265487 A IL 265487A IL 26548719 A IL26548719 A IL 26548719A IL 265487 B2 IL265487 B2 IL 265487B2
Authority
IL
Israel
Prior art keywords
retaining
component
piston
retaining component
projectile according
Prior art date
Application number
IL265487A
Other languages
English (en)
Hebrew (he)
Other versions
IL265487A (en
IL265487B1 (en
Inventor
Stubenrauch Philipp
Original Assignee
Diehl Defence Gmbh & Co Kg
Stubenrauch Philipp
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 Defence Gmbh & Co Kg, Stubenrauch Philipp filed Critical Diehl Defence Gmbh & Co Kg
Publication of IL265487A publication Critical patent/IL265487A/en
Publication of IL265487B1 publication Critical patent/IL265487B1/en
Publication of IL265487B2 publication Critical patent/IL265487B2/en

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
    • F42B10/02—Stabilising arrangements
    • F42B10/14—Stabilising arrangements using fins spread or deployed after launch, e.g. after leaving the barrel
    • F42B10/20—Stabilising arrangements using fins spread or deployed after launch, e.g. after leaving the barrel deployed by combustion gas pressure, or by pneumatic or hydraulic forces

Landscapes

  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Toys (AREA)
  • Fluid-Damping Devices (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
IL265487A 2018-03-21 2019-03-19 bullet IL265487B2 (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE102018002321 2018-03-21

Publications (3)

Publication Number Publication Date
IL265487A IL265487A (en) 2019-05-30
IL265487B1 IL265487B1 (en) 2024-12-01
IL265487B2 true IL265487B2 (en) 2025-04-01

Family

ID=65812197

Family Applications (1)

Application Number Title Priority Date Filing Date
IL265487A IL265487B2 (en) 2018-03-21 2019-03-19 bullet

Country Status (4)

Country Link
EP (1) EP3543640B1 (de)
ES (1) ES2992330T3 (de)
HU (1) HUE069114T2 (de)
IL (1) IL265487B2 (de)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN118310707B (zh) * 2024-06-05 2024-08-09 中国航空工业集团公司沈阳空气动力研究所 一种折叠翼展开动态风洞试验解锁装置及方法

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
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
EP1548392A1 (de) * 2003-12-24 2005-06-29 Giat Industries Vorrichtung zur Entfaltung der Steuerflächen eines Projektils
EP2620738A1 (de) * 2012-01-27 2013-07-31 Tda Armements S.A.S. Ansteuerungsteil fur Munition
US8592737B2 (en) * 2010-01-28 2013-11-26 Nexter Munitions Device for simultaneous deployment of the control surfaces of a projectile
WO2015128861A1 (en) * 2014-02-26 2015-09-03 Israel Aerospace Industries Ltd. Fin deployment system
CN105737685B (zh) * 2016-02-18 2017-07-21 江西洪都航空工业集团有限责任公司 一种翼面双向双位折叠结构

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2949848B1 (fr) 2009-09-10 2012-09-28 Nexter Munitions Dispositif d'ouverture et verrouillage d'une ailette canard.
US9702673B1 (en) * 2014-09-24 2017-07-11 The United States Of America As Represented By The Secretary Of The Army Projectile tail boom with self-locking fin
CN106839897B (zh) * 2017-01-03 2019-01-15 北京临近空间飞行器系统工程研究所 一种直线螺旋展开折叠翼机构

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
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
EP1548392A1 (de) * 2003-12-24 2005-06-29 Giat Industries Vorrichtung zur Entfaltung der Steuerflächen eines Projektils
US8592737B2 (en) * 2010-01-28 2013-11-26 Nexter Munitions Device for simultaneous deployment of the control surfaces of a projectile
EP2620738A1 (de) * 2012-01-27 2013-07-31 Tda Armements S.A.S. Ansteuerungsteil fur Munition
WO2015128861A1 (en) * 2014-02-26 2015-09-03 Israel Aerospace Industries Ltd. Fin deployment system
CN105737685B (zh) * 2016-02-18 2017-07-21 江西洪都航空工业集团有限责任公司 一种翼面双向双位折叠结构

Also Published As

Publication number Publication date
EP3543640A3 (de) 2020-01-08
EP3543640A2 (de) 2019-09-25
ES2992330T3 (es) 2024-12-11
IL265487A (en) 2019-05-30
EP3543640B1 (de) 2024-08-14
IL265487B1 (en) 2024-12-01
HUE069114T2 (hu) 2025-02-28

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