ATE352022T1 - Verriegelungseinrichtung für die steuerflossen - Google Patents

Verriegelungseinrichtung für die steuerflossen

Info

Publication number
ATE352022T1
ATE352022T1 AT01963763T AT01963763T ATE352022T1 AT E352022 T1 ATE352022 T1 AT E352022T1 AT 01963763 T AT01963763 T AT 01963763T AT 01963763 T AT01963763 T AT 01963763T AT E352022 T1 ATE352022 T1 AT E352022T1
Authority
AT
Austria
Prior art keywords
fin
piston
locking device
control fins
missile
Prior art date
Application number
AT01963763T
Other languages
English (en)
Inventor
Alfred Sorvino
Original Assignee
Raytheon Co
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 Raytheon Co filed Critical Raytheon Co
Application granted granted Critical
Publication of ATE352022T1 publication Critical patent/ATE352022T1/de

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

Landscapes

  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Actuator (AREA)
  • Vehicle Body Suspensions (AREA)
  • Steering Control In Accordance With Driving Conditions (AREA)
  • Lock And Its Accessories (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Carbon And Carbon Compounds (AREA)
  • Orthopedics, Nursing, And Contraception (AREA)
AT01963763T 2000-08-02 2001-07-31 Verriegelungseinrichtung für die steuerflossen ATE352022T1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US09/631,149 US6450444B1 (en) 2000-08-02 2000-08-02 Fin lock system

Publications (1)

Publication Number Publication Date
ATE352022T1 true ATE352022T1 (de) 2007-02-15

Family

ID=24529981

Family Applications (1)

Application Number Title Priority Date Filing Date
AT01963763T ATE352022T1 (de) 2000-08-02 2001-07-31 Verriegelungseinrichtung für die steuerflossen

Country Status (7)

Country Link
US (1) US6450444B1 (de)
EP (1) EP1305564B1 (de)
AT (1) ATE352022T1 (de)
AU (1) AU2001284687A1 (de)
DE (1) DE60126092T2 (de)
IL (1) IL154249A0 (de)
WO (1) WO2002010670A2 (de)

Families Citing this family (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7195197B2 (en) * 2005-02-11 2007-03-27 Hr Textron, Inc. Techniques for controlling a fin with unlimited adjustment and no backlash
US8338769B1 (en) 2008-02-07 2012-12-25 Simmonds Precision Products, Inc. Pyrotechnic fin deployment and retention mechanism
US8866057B2 (en) * 2011-10-17 2014-10-21 Raytheon Company Fin deployment method and apparatus
US8686328B2 (en) 2012-07-20 2014-04-01 Raytheon Company Resettable missile control fin lock assembly
US8975566B2 (en) 2012-08-09 2015-03-10 Raytheon Company Fin buzz system and method for assisting in unlocking a missile fin lock mechanism
US9372055B2 (en) * 2014-01-31 2016-06-21 The Boeing Company Passive control fin stops for air launched boosted (two stage) high speed vehicles
KR101833625B1 (ko) * 2016-07-08 2018-03-02 국방과학연구소 외력에 의한 날개의 흔들림 방지장치
DE102016009384B4 (de) * 2016-08-02 2019-10-31 Diehl Defence Gmbh & Co. Kg Verfahren zum Abwurf eines Lenkflugkörpers von einer fliegenden Plattform
US12007211B2 (en) 2021-05-04 2024-06-11 Honeywell International Inc. Manually resettable missile fin lock assembly
US11781844B2 (en) * 2021-08-03 2023-10-10 Raytheon Company Missile component attachment assembly
US12092436B2 (en) * 2021-09-03 2024-09-17 Raytheon Company Control surface restraining system for tactical flight vehicles

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CA1055003A (en) * 1976-12-17 1979-05-22 Frederick D. Ward Spring actuated differential for controlling angular position of a vane
US4412420A (en) * 1980-07-03 1983-11-01 Networks Electronics Corp. Explosive actuated pin puller
DE3721512C1 (de) * 1987-06-30 1989-03-30 Diehl Gmbh & Co Flugkoerper mit ueberkalibrigem Leitwerk
GB9003260D0 (en) * 1990-02-13 1990-11-21 Normalair Garrett Ltd Lock means for missile control fins
US5004186A (en) * 1990-06-01 1991-04-02 Aerotech, Inc. Finlock alignment mechanism for rockets
JPH04158198A (ja) * 1990-10-23 1992-06-01 Mitsubishi Heavy Ind Ltd 飛しょう体の操舵翼ロック装置
US5409185A (en) * 1993-07-12 1995-04-25 Lucas Aerospace Power Equipment Corporation Fin control actuator having a fin shaft lock device
JPH10253300A (ja) * 1997-03-12 1998-09-25 Mitsubishi Heavy Ind Ltd 飛しょう体の操舵翼

Also Published As

Publication number Publication date
EP1305564A2 (de) 2003-05-02
DE60126092D1 (de) 2007-03-08
EP1305564B1 (de) 2007-01-17
DE60126092T2 (de) 2007-10-18
AU2001284687A1 (en) 2002-02-13
US6450444B1 (en) 2002-09-17
WO2002010670A3 (en) 2002-04-25
WO2002010670A2 (en) 2002-02-07
IL154249A0 (en) 2003-09-17

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Legal Events

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