ATE283470T1 - Ausfahrbare und steuerbare flügel/ruder anordnung eines flugkörpers - Google Patents

Ausfahrbare und steuerbare flügel/ruder anordnung eines flugkörpers

Info

Publication number
ATE283470T1
ATE283470T1 AT01308931T AT01308931T ATE283470T1 AT E283470 T1 ATE283470 T1 AT E283470T1 AT 01308931 T AT01308931 T AT 01308931T AT 01308931 T AT01308931 T AT 01308931T AT E283470 T1 ATE283470 T1 AT E283470T1
Authority
AT
Austria
Prior art keywords
control surface
control
flight vehicle
guided munition
wing
Prior art date
Application number
AT01308931T
Other languages
English (en)
Inventor
Thomas Pijaca
William J Schellens
Original Assignee
Smiths Aerospace Inc
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 Smiths Aerospace Inc filed Critical Smiths Aerospace Inc
Application granted granted Critical
Publication of ATE283470T1 publication Critical patent/ATE283470T1/de

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
    • F42B10/60—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)
  • Transmission Devices (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
AT01308931T 2001-06-04 2001-10-19 Ausfahrbare und steuerbare flügel/ruder anordnung eines flugkörpers ATE283470T1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US09/873,498 US6581871B2 (en) 2001-06-04 2001-06-04 Extendable and controllable flight vehicle wing/control surface assembly

Publications (1)

Publication Number Publication Date
ATE283470T1 true ATE283470T1 (de) 2004-12-15

Family

ID=25361757

Family Applications (1)

Application Number Title Priority Date Filing Date
AT01308931T ATE283470T1 (de) 2001-06-04 2001-10-19 Ausfahrbare und steuerbare flügel/ruder anordnung eines flugkörpers

Country Status (4)

Country Link
US (1) US6581871B2 (de)
EP (1) EP1265050B1 (de)
AT (1) ATE283470T1 (de)
DE (1) DE60107397D1 (de)

Families Citing this family (13)

* 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
US6921052B2 (en) * 2003-11-28 2005-07-26 The United States Of America As Represented By The Secretary Of The Army Dragless flight control system for flying objects
US7255304B2 (en) * 2003-12-08 2007-08-14 General Dynamics Ordnance And Tactical Systems, Inc. Tandem motor actuator
US7412930B2 (en) * 2004-09-30 2008-08-19 General Dynamic Ordnance And Tactical Systems, Inc. Frictional roll control apparatus for a spinning projectile
FR2887224B1 (fr) * 2005-06-16 2008-10-17 Julien Apeloig Engin multimilieux
WO2007030687A2 (en) * 2005-09-09 2007-03-15 General Dynamics Ordnance And Tactical Systems Projectile trajectory control system
US7475846B2 (en) * 2005-10-05 2009-01-13 General Dynamics Ordnance And Tactical Systems, Inc. Fin retention and deployment mechanism
DE102007002948B4 (de) * 2007-01-19 2009-04-02 Diehl Bgt Defence Gmbh & Co. Kg Vorrichtung zur Tragflächenentfaltung
US8624172B2 (en) 2010-10-13 2014-01-07 Woodward Hrt, Inc. Shift lock assembly
US8847134B2 (en) * 2012-02-16 2014-09-30 Lockheed Martin Corporation Deployable wing and fin control surface actuation
US8975566B2 (en) * 2012-08-09 2015-03-10 Raytheon Company Fin buzz system and method for assisting in unlocking a missile fin lock mechanism
EP3984885B1 (de) * 2020-10-15 2024-01-31 INSITU, INC. a subsidiary of The Boeing Company Modulares anschlusssystem für ein unbemanntes luftfahrzeug
CN114370790B (zh) * 2021-12-22 2024-02-06 山西中辐核仪器有限责任公司 一种弹道二维修正机构

Family Cites Families (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4336914A (en) * 1978-12-29 1982-06-29 The Commonwealth Of Australia Deployable wing mechanism
AU524255B2 (en) 1978-12-29 1982-09-09 Commonwealth Of Australia, The Deployable wing
GB2150092B (en) * 1983-11-25 1987-07-22 British Aerospace Deployment and actuation mechanisms
US4575025A (en) * 1984-04-25 1986-03-11 Sadvary John W Fin deployment mechanism for missiles
US5582364A (en) 1991-11-07 1996-12-10 Hughes Missile Systems Company Flyable folding fin
US5480111A (en) * 1994-05-13 1996-01-02 Hughes Missile Systems Company Missile with deployable control fins
US5829715A (en) 1996-04-19 1998-11-03 Lockheed Martin Vought Systems Corp. Multi-axis unfolding mechanism with rate controlled synchronized movement
US6073880A (en) * 1998-05-18 2000-06-13 Versatron, Inc. Integrated missile fin deployment system
US6186443B1 (en) * 1998-06-25 2001-02-13 International Dynamics Corporation Airborne vehicle having deployable wing and control surface
US6224013B1 (en) * 1998-08-27 2001-05-01 Lockheed Martin Corporation Tail fin deployment device

Also Published As

Publication number Publication date
US20020179778A1 (en) 2002-12-05
US6581871B2 (en) 2003-06-24
EP1265050B1 (de) 2004-11-24
DE60107397D1 (de) 2004-12-30
EP1265050A1 (de) 2002-12-11

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Legal Events

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