ITTO20010394A0 - Meccanismo di bloccaggio e sbloccaggio per aletta stabilizzatrice di missile, includente un amplificatore di forza meccanico. - Google Patents

Meccanismo di bloccaggio e sbloccaggio per aletta stabilizzatrice di missile, includente un amplificatore di forza meccanico.

Info

Publication number
ITTO20010394A0
ITTO20010394A0 IT2001TO000394A ITTO20010394A ITTO20010394A0 IT TO20010394 A0 ITTO20010394 A0 IT TO20010394A0 IT 2001TO000394 A IT2001TO000394 A IT 2001TO000394A IT TO20010394 A ITTO20010394 A IT TO20010394A IT TO20010394 A0 ITTO20010394 A0 IT TO20010394A0
Authority
IT
Italy
Prior art keywords
missile
flip
stabilizer
locking
mechanical force
Prior art date
Application number
IT2001TO000394A
Other languages
English (en)
Inventor
William H Hsu
Matthew Miotla
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 ITTO20010394A0 publication Critical patent/ITTO20010394A0/it
Publication of ITTO20010394A1 publication Critical patent/ITTO20010394A1/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
    • F42B10/60—Steering arrangements
    • F42B10/62—Steering by movement of flight surfaces
    • F42B10/64—Steering by movement of flight surfaces of fins
IT2001TO000394A 2000-04-25 2001-04-24 Meccanismo di bloccaggio e sbloccaggio per aletta stabilizzatrice di missile, includente un amplificatore di forza meccanico. ITTO20010394A1 (it)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US09/556,807 US6352217B1 (en) 2000-04-25 2000-04-25 Missile fin locking and unlocking mechanism including a mechanical force amplifier

Publications (2)

Publication Number Publication Date
ITTO20010394A0 true ITTO20010394A0 (it) 2001-04-24
ITTO20010394A1 ITTO20010394A1 (it) 2002-10-24

Family

ID=24222937

Family Applications (1)

Application Number Title Priority Date Filing Date
IT2001TO000394A ITTO20010394A1 (it) 2000-04-25 2001-04-24 Meccanismo di bloccaggio e sbloccaggio per aletta stabilizzatrice di missile, includente un amplificatore di forza meccanico.

Country Status (4)

Country Link
US (1) US6352217B1 (it)
GB (1) GB2361681B (it)
IL (1) IL142263A (it)
IT (1) ITTO20010394A1 (it)

Families Citing this family (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB0111171D0 (en) * 2001-05-08 2001-06-27 Special Cartridge Company Ltd Projictile
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
US7559505B2 (en) * 2005-12-01 2009-07-14 Lockheed Martin Corporation Apparatus and method for restraining and deploying an airfoil
WO2007077525A2 (fr) 2006-01-04 2007-07-12 Boujon, Claire-Lise Courses d'obstacles
US7700902B2 (en) * 2007-10-18 2010-04-20 Hr Textron, Inc. Locking assembly for rotary shafts
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
IL231186A (en) 2014-02-26 2017-07-31 Israel Aerospace Ind Ltd Wing opening mechanism
CN109506525B (zh) * 2018-11-23 2020-12-15 江西洪都航空工业集团有限责任公司 一种动力源偏置型折叠展开机构
US11530905B2 (en) 2021-01-29 2022-12-20 Woodward, Inc. Rotatable lock and release mechanism

Family Cites Families (22)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB560931A (en) 1942-08-24 1944-04-27 Gordon Alexander Allan King Improvements in or relating to projectiles
US2852210A (en) 1955-11-03 1958-09-16 Aerophysics Dev Corp Inertia spoiler control for aircraft
US3093075A (en) 1960-07-29 1963-06-11 Edgar J Garrett Fin latch assembly
US3045779A (en) 1961-03-07 1962-07-24 Rosenthai Sidney Electromechanical linear reciprocal actuator
US3182564A (en) 1963-05-14 1965-05-11 Lake Ct Switch Company Motors
FR1590790A (it) 1968-11-05 1970-04-20
US3711040A (en) 1971-04-20 1973-01-16 Us Navy Outboard missile control surface and actuator
US3759466A (en) 1972-01-10 1973-09-18 Us Army Cruise control for non-ballistic missiles by a special arrangement of spoilers
US4175720A (en) * 1978-04-05 1979-11-27 The United States Of America As Represented By The Secretary Of The Navy Retainer/release mechanism for use on fin stabilized gun fired projectiles
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
US4603594A (en) 1984-05-31 1986-08-05 Sundstrand Corporation Fail safe actuator
US4667899A (en) * 1984-11-28 1987-05-26 General Dynamics, Pomona Division Double swing wing self-erecting missile wing structure
DE3507677A1 (de) 1985-03-05 1986-09-11 Diehl GmbH & Co, 8500 Nürnberg Flugkoerper mit ueberkalibrigem leitwerk
US4691880A (en) 1985-11-14 1987-09-08 Grumman Aerospace Corporation Torsion spring powered missile wing deployment system
US4795110A (en) 1986-12-30 1989-01-03 Sundstrand Corporation Flight control surface actuation lock system
DE3721512C1 (de) 1987-06-30 1989-03-30 Diehl Gmbh & Co Flugkoerper mit ueberkalibrigem Leitwerk
GB2237362B (en) 1989-10-24 1994-01-19 British Aerospace Retardation and arming mechanism for a projectile
DE4020897C2 (de) * 1990-06-30 1993-11-11 Diehl Gmbh & Co Einrichtung zum Entriegeln und Ausschwenken der Ruderblätter eines Projektiles
US5409185A (en) 1993-07-12 1995-04-25 Lucas Aerospace Power Equipment Corporation Fin control actuator having a fin shaft lock device
US5950963A (en) * 1997-10-09 1999-09-14 Versatron Corporation Fin lock mechanism
US6224013B1 (en) * 1998-08-27 2001-05-01 Lockheed Martin Corporation Tail fin deployment device
US6250584B1 (en) * 1999-10-18 2001-06-26 Hr Textron, Inc. Missile fin locking mechanism

Also Published As

Publication number Publication date
GB2361681A (en) 2001-10-31
ITTO20010394A1 (it) 2002-10-24
GB0107451D0 (en) 2001-05-16
IL142263A0 (en) 2002-03-10
IL142263A (en) 2009-09-01
GB2361681B (en) 2002-07-24
US6352217B1 (en) 2002-03-05

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