EP2216619A3 - Flugabbruchvorrichtung für einen Flugkörper - Google Patents

Flugabbruchvorrichtung für einen Flugkörper Download PDF

Info

Publication number
EP2216619A3
EP2216619A3 EP10001071.9A EP10001071A EP2216619A3 EP 2216619 A3 EP2216619 A3 EP 2216619A3 EP 10001071 A EP10001071 A EP 10001071A EP 2216619 A3 EP2216619 A3 EP 2216619A3
Authority
EP
European Patent Office
Prior art keywords
missile
flight
abort device
transmission
control surfaces
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.)
Granted
Application number
EP10001071.9A
Other languages
English (en)
French (fr)
Other versions
EP2216619B1 (de
EP2216619A2 (de
Inventor
Thomas Klaffert
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.)
MBDA Deutschland GmbH
Original Assignee
MBDA Deutschland GmbH
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 MBDA Deutschland GmbH filed Critical MBDA Deutschland GmbH
Publication of EP2216619A2 publication Critical patent/EP2216619A2/de
Publication of EP2216619A3 publication Critical patent/EP2216619A3/de
Application granted granted Critical
Publication of EP2216619B1 publication Critical patent/EP2216619B1/de
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42BEXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B10/00Means 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
    • F42B10/60Steering arrangements
    • F42B10/62Steering by movement of flight surfaces
    • F42B10/64Steering by movement of flight surfaces of fins
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42BEXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B10/00Means 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
    • F42B10/32Range-reducing or range-increasing arrangements; Fall-retarding means
    • F42B10/48Range-reducing, destabilising or braking arrangements, e.g. impact-braking arrangements; Fall-retarding means, e.g. balloons, rockets for braking or fall-retarding

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)

Abstract

Eine Flugabbruchvorrichtung für einen Flugkörper mit aerodynamischen Steuerflächen (1) zur Steuerung des Flugkörpers, wobei die Steuerflächen (1) von zumindest einer Antriebseinrichtung (3) über zumindest ein Getriebe (2) zur Verstellung antreibbar sind, zeichnet sich durch zumindest ein von einer Auslösevorrichtung (6) betätigbares Wirkelement (4), das in das Getriebe (2) integriert ist, aus.
EP10001071.9A 2009-02-05 2010-02-03 Flugabbruchvorrichtung für einen Flugkörper Active EP2216619B1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE200910007731 DE102009007731A1 (de) 2009-02-05 2009-02-05 Flugabbruchvorrichtung für einen Flugkörper

Publications (3)

Publication Number Publication Date
EP2216619A2 EP2216619A2 (de) 2010-08-11
EP2216619A3 true EP2216619A3 (de) 2014-03-19
EP2216619B1 EP2216619B1 (de) 2016-12-14

Family

ID=41785918

Family Applications (1)

Application Number Title Priority Date Filing Date
EP10001071.9A Active EP2216619B1 (de) 2009-02-05 2010-02-03 Flugabbruchvorrichtung für einen Flugkörper

Country Status (2)

Country Link
EP (1) EP2216619B1 (de)
DE (1) DE102009007731A1 (de)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102020119446B4 (de) 2020-05-18 2022-01-05 Deutsches Zentrum für Luft- und Raumfahrt e.V. Risikominimierungsvorrichtung für den Flugabbruch eines Flugsystems, Verfahren zur Risikominimierung beim Flugabbruch eines Flugsystems und Flugsystem
US20240060552A1 (en) * 2022-08-17 2024-02-22 Raytheon Company Sliding pin-yoke mechanism

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3352513A (en) * 1966-03-25 1967-11-14 George W Baker Helicopter rotor shaft and rotor blade severing means
GB2260954A (en) * 1991-10-29 1993-05-05 Diehl Gmbh & Co Rudder control apparatus
DE19635847A1 (de) * 1996-09-04 1998-03-12 Daimler Benz Aerospace Ag Lenkflugkörper mit Staustrahlantrieb

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3352513A (en) * 1966-03-25 1967-11-14 George W Baker Helicopter rotor shaft and rotor blade severing means
GB2260954A (en) * 1991-10-29 1993-05-05 Diehl Gmbh & Co Rudder control apparatus
DE19635847A1 (de) * 1996-09-04 1998-03-12 Daimler Benz Aerospace Ag Lenkflugkörper mit Staustrahlantrieb

Also Published As

Publication number Publication date
EP2216619B1 (de) 2016-12-14
EP2216619A2 (de) 2010-08-11
DE102009007731A1 (de) 2010-08-19

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