GB1342342A - Control systems - Google Patents

Control systems

Info

Publication number
GB1342342A
GB1342342A GB322570A GB1342342DA GB1342342A GB 1342342 A GB1342342 A GB 1342342A GB 322570 A GB322570 A GB 322570A GB 1342342D A GB1342342D A GB 1342342DA GB 1342342 A GB1342342 A GB 1342342A
Authority
GB
United Kingdom
Prior art keywords
nozzle
dirigible
missile
swivel
centre
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.)
Expired
Application number
GB322570A
Other languages
English (en)
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.)
Hawker Siddeley Dynamics Ltd
Original Assignee
Hawker Siddeley Dynamics Ltd
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 Hawker Siddeley Dynamics Ltd filed Critical Hawker Siddeley Dynamics Ltd
Publication of GB1342342A publication Critical patent/GB1342342A/en
Expired legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K9/00—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
    • F02K9/80—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof characterised by thrust or thrust vector control
    • F02K9/84—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof characterised by thrust or thrust vector control using movable nozzles

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
GB322570A 1970-04-30 1971-04-30 Control systems Expired GB1342342A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB322570 1970-04-30

Publications (1)

Publication Number Publication Date
GB1342342A true GB1342342A (en) 1974-01-03

Family

ID=9754332

Family Applications (1)

Application Number Title Priority Date Filing Date
GB322570A Expired GB1342342A (en) 1970-04-30 1971-04-30 Control systems

Country Status (4)

Country Link
US (1) US3764091A (enExample)
FR (1) FR2165695B1 (enExample)
GB (1) GB1342342A (enExample)
SE (1) SE377719C (enExample)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2299558A (en) * 1995-03-31 1996-10-09 Nissan Motor Jetevator for rocket engine
CN102363444A (zh) * 2011-09-09 2012-02-29 江西洪都航空工业集团有限责任公司 一种尾翼横向折叠机构

Families Citing this family (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4085909A (en) * 1976-10-04 1978-04-25 Ford Motor Company Combined warm gas fin and reaction control servo
US6568628B1 (en) * 1977-07-28 2003-05-27 Raytheon Company Shipboard point defense system and elements therefor
US4274610A (en) * 1978-07-14 1981-06-23 General Dynamics, Pomona Division Jet tab control mechanism for thrust vector control
US4561357A (en) * 1982-09-15 1985-12-31 General Dynamics Pomona Division Steering mechanism for an explosively fired projectile
USH159H (en) 1984-12-17 1986-11-04 The United States Of America As Represented By The Secretary Of The Navy Shaped trajectory cruise missile launch mode
FR2635180B1 (fr) * 1988-08-05 1992-11-06 Aris Spa Ensemble de commande, de controle et de propulsion, en particulier pour des objets balistiques
US5125596A (en) * 1989-05-23 1992-06-30 Cavalleri Robert J Fluid shielded movable strut for missile and rocket thrust vector control
US6250584B1 (en) 1999-10-18 2001-06-26 Hr Textron, Inc. Missile fin locking mechanism
SE518657C2 (sv) * 2000-07-03 2002-11-05 Bofors Defence Ab Fenstabiliserad styrbar projektil
US6948685B2 (en) 2003-10-27 2005-09-27 Hr Textron, Inc. Locking device with solenoid release pin
US7262394B2 (en) * 2004-03-05 2007-08-28 The Boeing Company Mortar shell ring tail and associated method
US7195197B2 (en) * 2005-02-11 2007-03-27 Hr Textron, Inc. Techniques for controlling a fin with unlimited adjustment and no backlash
US8362408B2 (en) * 2009-10-22 2013-01-29 Honeywell International Inc. Steerable projectile charging system
FR2970702B1 (fr) * 2011-01-26 2013-05-10 Astrium Sas Procede et systeme de pilotage d'un engin volant a propulseur arriere
CN104085526B (zh) * 2014-06-25 2016-03-30 西北工业大学 一种实现巡飞器翼身连接、固定、锁死、解锁的一体化结构

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2780059A (en) * 1955-11-29 1957-02-05 Willy A Fiedler Jet direction control device
US3003312A (en) * 1957-08-19 1961-10-10 Thompson Ramo Wooldridge Inc Exhaust nozzle for jet engines
US3210935A (en) * 1959-09-23 1965-10-12 Lyman C Fisher Jetevator for missile control
US3069852A (en) * 1959-10-27 1962-12-25 Goodyear Aircraft Corp Thrust vectoring apparatus
US3210936A (en) * 1959-12-10 1965-10-12 Lyman C Fisher Jetevator for missile control
US3102390A (en) * 1960-03-09 1963-09-03 Fredrick R Barnet Jetevator system design
US3233834A (en) * 1962-07-09 1966-02-08 Aerojet General Co Sealing means for rocket nozzle and jet deflection device mounted thereon
US3285520A (en) * 1964-11-10 1966-11-15 Glenn A Johnson Eccentrically pivoted jetevator with conformable seal
US3438581A (en) * 1967-02-06 1969-04-15 Continental Aviat & Eng Corp Internally gimbaled vectoring nozzle

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2299558A (en) * 1995-03-31 1996-10-09 Nissan Motor Jetevator for rocket engine
GB2299558B (en) * 1995-03-31 1997-06-04 Nissan Motor Jetavator for rocket engine
US5735463A (en) * 1995-03-31 1998-04-07 Nissan Motor Co., Ltd. Jetavator for rocket engine
CN102363444A (zh) * 2011-09-09 2012-02-29 江西洪都航空工业集团有限责任公司 一种尾翼横向折叠机构

Also Published As

Publication number Publication date
FR2165695A1 (enExample) 1973-08-10
US3764091A (en) 1973-10-09
SE377719C (sv) 1978-11-20
SE377719B (enExample) 1975-07-21
FR2165695B1 (enExample) 1976-02-06

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Legal Events

Date Code Title Description
PS Patent sealed [section 19, patents act 1949]
732 Registration of transactions, instruments or events in the register (sect. 32/1977)
732 Registration of transactions, instruments or events in the register (sect. 32/1977)
PCNP Patent ceased through non-payment of renewal fee