EP4111127C0 - Flugkörper-finnenausklappeinrichtung und flugkörper - Google Patents

Flugkörper-finnenausklappeinrichtung und flugkörper

Info

Publication number
EP4111127C0
EP4111127C0 EP21706569.7A EP21706569A EP4111127C0 EP 4111127 C0 EP4111127 C0 EP 4111127C0 EP 21706569 A EP21706569 A EP 21706569A EP 4111127 C0 EP4111127 C0 EP 4111127C0
Authority
EP
European Patent Office
Prior art keywords
missile
fin device
fin
missile fin
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
Application number
EP21706569.7A
Other languages
English (en)
French (fr)
Other versions
EP4111127A1 (de
EP4111127B1 (de
Inventor
Josef Klevanski
Etienne Dumont
Waldemar Rotärmel
Ivaylo Petkov
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Deutsches Zentrum fuer Luft und Raumfahrt eV
Original Assignee
Deutsches Zentrum fuer Luft und Raumfahrt eV
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 Deutsches Zentrum fuer Luft und Raumfahrt eV filed Critical Deutsches Zentrum fuer Luft und Raumfahrt eV
Publication of EP4111127A1 publication Critical patent/EP4111127A1/de
Application granted granted Critical
Publication of EP4111127C0 publication Critical patent/EP4111127C0/de
Publication of EP4111127B1 publication Critical patent/EP4111127B1/de
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
EP21706569.7A 2020-02-27 2021-02-18 Flugkörper-finnenausklappeinrichtung und flugkörper Active EP4111127B1 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE102020105188.3A DE102020105188B4 (de) 2020-02-27 2020-02-27 Flugkörper-Finnenausklappeinrichtung, Flugkörper und Verfahren zum Betrieb eines Flugkörpers
PCT/EP2021/054044 WO2021170484A1 (de) 2020-02-27 2021-02-18 Flugkörper-finnenausklappeinrichtung, flugkörper und verfahren zum betrieb eines flugkörpers

Publications (3)

Publication Number Publication Date
EP4111127A1 EP4111127A1 (de) 2023-01-04
EP4111127C0 true EP4111127C0 (de) 2025-04-23
EP4111127B1 EP4111127B1 (de) 2025-04-23

Family

ID=74668866

Family Applications (1)

Application Number Title Priority Date Filing Date
EP21706569.7A Active EP4111127B1 (de) 2020-02-27 2021-02-18 Flugkörper-finnenausklappeinrichtung und flugkörper

Country Status (3)

Country Link
EP (1) EP4111127B1 (de)
DE (1) DE102020105188B4 (de)
WO (1) WO2021170484A1 (de)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102022000496A1 (de) 2022-02-09 2023-08-10 Diehl Defence Gmbh & Co. Kg Trägerplattform zum Abschießen oder Abwerfen eines unbemannten Flugkörpers auf ein Ziel und Verfahren zum Betrieb einer solchen Trägerplattform

Family Cites Families (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3010027C2 (de) 1978-09-26 1985-07-11 Messerschmitt-Bölkow-Blohm GmbH, 8000 München Schwenkbare Anordnung eines Leitwerks, insbesondere bei Flugkörpern oder Geschossen
GB2150092B (en) 1983-11-25 1987-07-22 British Aerospace Deployment and actuation mechanisms
US6761331B2 (en) 2002-03-19 2004-07-13 Raytheon Company Missile having deployment mechanism for stowable fins
US6726147B1 (en) 2003-05-15 2004-04-27 Moog Inc. Multi-function actuator, and method of operating same
US6869044B2 (en) 2003-05-23 2005-03-22 Raytheon Company Missile with odd symmetry tail fins
FR2860577B1 (fr) * 2003-10-06 2006-01-27 Giat Ind Sa Dispositif de deploiement d'une ailette d'un projectile
US7628353B2 (en) 2006-11-14 2009-12-08 Raytheon Company Delayed tail fin deployment mechanism and method
US7906749B2 (en) 2007-11-19 2011-03-15 Raytheon Company System and method for deployment and actuation
EP2433084B1 (de) 2009-05-19 2013-05-08 Raytheon Company Lenkflugkörper
US8026465B1 (en) 2009-05-20 2011-09-27 The United States Of America As Represented By The Secretary Of The Navy Guided fuse with variable incidence panels
KR101069246B1 (ko) 2009-06-11 2011-10-04 국방과학연구소 날개 전개 장치 및 이를 구비하는 비행체 발사 장치
US8939056B1 (en) 2012-04-20 2015-01-27 Barron Associates, Inc. Systems, devices, and/or methods for managing targeted payload descent
US9593922B2 (en) 2013-03-14 2017-03-14 Bae Systems Land & Armaments L.P. Fin deployment system
US10295318B2 (en) 2014-03-13 2019-05-21 Moog Inc. Fin retention and release mechanism
US11175117B2 (en) 2016-07-21 2021-11-16 Chairman, Defence Research & Development Organisation (DRDO) Bi-directional wing unfolding mechanism
KR101864088B1 (ko) 2017-10-27 2018-06-04 국방과학연구소 발사체의 조종날개장치 및 그 제어방법

Also Published As

Publication number Publication date
EP4111127A1 (de) 2023-01-04
DE102020105188B4 (de) 2023-08-31
DE102020105188A1 (de) 2021-09-02
EP4111127B1 (de) 2025-04-23
WO2021170484A1 (de) 2021-09-02

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