ITTO20000977A0 - Meccanismo di bloccaggio per le alette di un missile. - Google Patents

Meccanismo di bloccaggio per le alette di un missile.

Info

Publication number
ITTO20000977A0
ITTO20000977A0 IT2000TO000977A ITTO20000977A ITTO20000977A0 IT TO20000977 A0 ITTO20000977 A0 IT TO20000977A0 IT 2000TO000977 A IT2000TO000977 A IT 2000TO000977A IT TO20000977 A ITTO20000977 A IT TO20000977A IT TO20000977 A0 ITTO20000977 A0 IT TO20000977A0
Authority
IT
Italy
Prior art keywords
missile
flaps
locking mechanism
locking
Prior art date
Application number
IT2000TO000977A
Other languages
English (en)
Inventor
William W Hsu
Duncan D Bragg
Original Assignee
Hr Textron 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 Hr Textron Inc filed Critical Hr Textron Inc
Publication of ITTO20000977A0 publication Critical patent/ITTO20000977A0/it
Publication of ITTO20000977A1 publication Critical patent/ITTO20000977A1/it
Application granted granted Critical
Publication of IT1320708B1 publication Critical patent/IT1320708B1/it

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

Landscapes

  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Mechanical Control Devices (AREA)
IT2000TO000977A 1999-10-18 2000-10-18 Meccanismo di bloccaggio per le alette di un missile. IT1320708B1 (it)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US09/419,544 US6250584B1 (en) 1999-10-18 1999-10-18 Missile fin locking mechanism

Publications (3)

Publication Number Publication Date
ITTO20000977A0 true ITTO20000977A0 (it) 2000-10-18
ITTO20000977A1 ITTO20000977A1 (it) 2002-04-18
IT1320708B1 IT1320708B1 (it) 2003-12-10

Family

ID=23662716

Family Applications (1)

Application Number Title Priority Date Filing Date
IT2000TO000977A IT1320708B1 (it) 1999-10-18 2000-10-18 Meccanismo di bloccaggio per le alette di un missile.

Country Status (4)

Country Link
US (1) US6250584B1 (it)
GB (1) GB2355440B (it)
IL (1) IL139066A (it)
IT (1) IT1320708B1 (it)

Families Citing this family (20)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6352217B1 (en) * 2000-04-25 2002-03-05 Hr Textron, Inc. Missile fin locking and unlocking mechanism including a mechanical force amplifier
GB0111171D0 (en) * 2001-05-08 2001-06-27 Special Cartridge Company Ltd Projictile
US6474594B1 (en) * 2001-05-11 2002-11-05 Raytheon Company Output shaft assembly for a missile control actuation unit
DE10143312C1 (de) * 2001-09-04 2003-06-18 Diehl Munitionssysteme Gmbh Bremseinrichtung für ein bahnkorrigierbares drallstabilisiertes Artillerieprojektil
US7097132B2 (en) 2002-09-16 2006-08-29 Lockheed Martin Corporation Apparatus and method for selectivity locking a fin assembly
US7040210B2 (en) 2003-02-18 2006-05-09 Lockheed Martin Corporation Apparatus and method for restraining and releasing a control surface
US6948685B2 (en) 2003-10-27 2005-09-27 Hr Textron, Inc. Locking device with solenoid release pin
US7410120B2 (en) * 2005-01-21 2008-08-12 The Boeing Company Control surface assemblies with torque tube base
US7195197B2 (en) * 2005-02-11 2007-03-27 Hr Textron, Inc. Techniques for controlling a fin with unlimited adjustment and no backlash
US7316370B2 (en) * 2005-06-13 2008-01-08 Goodrich Corporation Missile fin locking method and assembly
US7559505B2 (en) * 2005-12-01 2009-07-14 Lockheed Martin Corporation Apparatus and method for restraining and deploying an airfoil
WO2009079057A1 (en) * 2007-09-24 2009-06-25 Raytheon Company Methods and apparatus for a control surface restraint and release system
US7700902B2 (en) * 2007-10-18 2010-04-20 Hr Textron, Inc. Locking assembly for rotary shafts
US9863745B2 (en) 2010-11-04 2018-01-09 Parker-Hannifin Corporation Rotational lock mechanism for actuator
EP2617647B1 (de) * 2012-01-18 2019-04-03 MBDA Deutschland GmbH Ver- und Entriegelungssystem mit reversibler Auslösemöglichkeit zum vorteilhaften Einsatz in Stellsystemen (Aktoren)
US8975566B2 (en) 2012-08-09 2015-03-10 Raytheon Company Fin buzz system and method for assisting in unlocking a missile fin lock mechanism
US9040886B1 (en) 2013-05-08 2015-05-26 The Boeing Company Adaptive aerodynamic control system for projectile maneuvering
IN2014MU02909A (it) * 2013-09-21 2015-10-09 Mbda Deutschland Gmbh
US11530905B2 (en) * 2021-01-29 2022-12-20 Woodward, Inc. Rotatable lock and release mechanism
US12007211B2 (en) 2021-05-04 2024-06-11 Honeywell International Inc. Manually resettable missile fin lock assembly

Family Cites Families (21)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2952207A (en) * 1952-06-30 1960-09-13 Michael M Kamimoto Missile
US3001474A (en) 1954-01-18 1961-09-26 William B Mclean Propellant servo and power supply for missile guidance
US3093075A (en) * 1960-07-29 1963-06-11 Edgar J Garrett Fin latch assembly
US3154015A (en) 1962-09-19 1964-10-27 Martin Marietta Corp Missile flight control system
SE377719C (sv) 1970-04-30 1978-11-20 Hawker Siddeley Dynamics Ltd Anordning for styrning och framatdrivande av suft- eller rymdfarkost
US3697019A (en) 1970-05-13 1972-10-10 Us Navy Stabilizing fin assembly
US3711040A (en) 1971-04-20 1973-01-16 Us Navy Outboard missile control surface and actuator
US4374577A (en) * 1976-01-14 1983-02-22 The United States Of America As Represented By The Secretary Of The Navy Adapter assembly for flat trajectory flight
US4141520A (en) 1977-06-20 1979-02-27 Adams Rite Products, Inc. Fail-safe lock for an airplane rudder
US4173322A (en) 1978-04-27 1979-11-06 The United States Of America As Represented By The Secretary Of The Air Force Flutter prevention means for aircraft primary flight control surfaces
US4795110A (en) 1986-12-30 1989-01-03 Sundstrand Corporation Flight control surface actuation lock system
US4738412A (en) * 1987-08-24 1988-04-19 The United States Of America As Represented By The Secretary Of The Navy Air stabilized gimbal platform
GB9003260D0 (en) * 1990-02-13 1990-11-21 Normalair Garrett Ltd Lock means for missile control fins
DE4025516C2 (de) 1990-08-11 1994-04-14 Deutsche Aerospace Flugkörpertragflächen-Verriegelungseinrichtung
JPH04288499A (ja) 1991-02-27 1992-10-13 Mitsubishi Electric Corp 誘導飛しょう体
US5127605A (en) 1991-04-23 1992-07-07 Allied-Signal Inc. Control surface structures for fluid-borne vehicles and method for rotationally moving such structures
US5192037A (en) 1991-08-23 1993-03-09 Mcdonnell Douglas Corporation Double-pivoting deployment system for aerosurfaces
US5409185A (en) 1993-07-12 1995-04-25 Lucas Aerospace Power Equipment Corporation Fin control actuator having a fin shaft lock device
ATE154147T1 (de) 1994-03-17 1997-06-15 Detra Sa Verfahren zur versorgung eines einphasigen schrittmotors sowie schaltung hierfür
DE19635847C2 (de) 1996-09-04 1998-07-16 Daimler Benz Aerospace Ag Lenkflugkörper mit Staustrahlantrieb
US5950963A (en) 1997-10-09 1999-09-14 Versatron Corporation Fin lock mechanism

Also Published As

Publication number Publication date
GB0024968D0 (en) 2000-11-29
IT1320708B1 (it) 2003-12-10
ITTO20000977A1 (it) 2002-04-18
GB2355440A (en) 2001-04-25
IL139066A0 (en) 2001-11-25
GB2355440B (en) 2002-01-09
IL139066A (en) 2003-07-06
US6250584B1 (en) 2001-06-26

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