PL4200577T3 - Rozkładany układ skrzydłowy dla pocisku, pocisk zawierający taki układ skrzydłowy, zastosowanie układu skrzydłowego oraz sposób rozkładania łopatki skrzydłowej dla pocisku - Google Patents

Rozkładany układ skrzydłowy dla pocisku, pocisk zawierający taki układ skrzydłowy, zastosowanie układu skrzydłowego oraz sposób rozkładania łopatki skrzydłowej dla pocisku

Info

Publication number
PL4200577T3
PL4200577T3 PL21858710.3T PL21858710T PL4200577T3 PL 4200577 T3 PL4200577 T3 PL 4200577T3 PL 21858710 T PL21858710 T PL 21858710T PL 4200577 T3 PL4200577 T3 PL 4200577T3
Authority
PL
Poland
Prior art keywords
projectile
wing
wing system
deploying
application
Prior art date
Application number
PL21858710.3T
Other languages
English (en)
Inventor
Jan-Peter ROSÉN
Henrik Karlsson
Original Assignee
Saab 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 Saab Ab filed Critical Saab Ab
Publication of PL4200577T3 publication Critical patent/PL4200577T3/pl

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
    • F42B10/16—Wrap-around fins

Landscapes

  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Toys (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
PL21858710.3T 2020-08-19 2021-08-19 Rozkładany układ skrzydłowy dla pocisku, pocisk zawierający taki układ skrzydłowy, zastosowanie układu skrzydłowego oraz sposób rozkładania łopatki skrzydłowej dla pocisku PL4200577T3 (pl)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
SE2000144A SE544987C2 (en) 2020-08-19 2020-08-19 A wing arrangement, a projectile, a use and a method for deploying a wing blade
PCT/SE2021/050813 WO2022039659A1 (en) 2020-08-19 2021-08-19 A deployable wing arrangement for a projectile, a projectile comprising such a wing arrangement, an use of such a wing arrangement and a method for deploying a wing blade for a projectile

Publications (1)

Publication Number Publication Date
PL4200577T3 true PL4200577T3 (pl) 2025-09-08

Family

ID=80323630

Family Applications (1)

Application Number Title Priority Date Filing Date
PL21858710.3T PL4200577T3 (pl) 2020-08-19 2021-08-19 Rozkładany układ skrzydłowy dla pocisku, pocisk zawierający taki układ skrzydłowy, zastosowanie układu skrzydłowego oraz sposób rozkładania łopatki skrzydłowej dla pocisku

Country Status (4)

Country Link
EP (1) EP4200577B1 (pl)
PL (1) PL4200577T3 (pl)
SE (1) SE544987C2 (pl)
WO (1) WO2022039659A1 (pl)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN119240031B (zh) * 2024-09-29 2025-11-04 北京工业大学 一种包含多锁止机构的折叠尾翼的旋转轴组件

Family Cites Families (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3563495A (en) * 1969-02-03 1971-02-16 Us Air Force Power operated folding wing for rockets and missiles
US4575025A (en) * 1984-04-25 1986-03-11 Sadvary John W Fin deployment mechanism for missiles
US4884766A (en) * 1988-05-25 1989-12-05 The United States Of America As Represented By The Secretary Of The Air Force Automatic fin deployment mechanism
GB2274904A (en) * 1993-02-05 1994-08-10 British Aerospace Deployable wing
KR0176320B1 (ko) * 1995-12-09 1999-04-01 배문한 유도탄 날개 전개 및 고정 장치
US7097132B2 (en) * 2002-09-16 2006-08-29 Lockheed Martin Corporation Apparatus and method for selectivity locking a fin assembly
DE102004039770A1 (de) * 2004-08-16 2006-03-02 Diehl Bgt Defence Gmbh & Co. Kg Flügelanordnung
US20070045466A1 (en) * 2005-08-31 2007-03-01 Hellis Neil C Foldable, lockable control surface and method of using same
US7322545B2 (en) * 2005-12-29 2008-01-29 The Boeing Company Structural mechanism for unlocking and engaging a controllable surface on a hinged platform (wing)
DE102017009671A1 (de) * 2016-11-03 2018-05-03 Diehl Defence Gmbh & Co. Kg Verfahren zum Abwerfen eines Flugkörpers

Also Published As

Publication number Publication date
EP4200577B1 (en) 2025-07-16
EP4200577C0 (en) 2025-07-16
SE544987C2 (en) 2023-02-21
EP4200577A4 (en) 2024-08-28
EP4200577A1 (en) 2023-06-28
WO2022039659A1 (en) 2022-02-24
SE2000144A1 (en) 2022-02-20

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