DE69611940T2 - Verfahren und Steuerungssystem für die Leitschaufeln eines Flugkörpers - Google Patents

Verfahren und Steuerungssystem für die Leitschaufeln eines Flugkörpers

Info

Publication number
DE69611940T2
DE69611940T2 DE69611940T DE69611940T DE69611940T2 DE 69611940 T2 DE69611940 T2 DE 69611940T2 DE 69611940 T DE69611940 T DE 69611940T DE 69611940 T DE69611940 T DE 69611940T DE 69611940 T2 DE69611940 T2 DE 69611940T2
Authority
DE
Germany
Prior art keywords
missile
control system
guide vanes
vanes
guide
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 - Lifetime
Application number
DE69611940T
Other languages
English (en)
Other versions
DE69611940D1 (de
Inventor
William M Hatalsky
Andrew B Facciano
Stephen D Haight
Sean A Johnson
Aszetta D Jordan
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.)
Raytheon Co
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 DE69611940D1 publication Critical patent/DE69611940D1/de
Publication of DE69611940T2 publication Critical patent/DE69611940T2/de
Anticipated expiration legal-status Critical
Expired - Lifetime 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
    • F02K9/805—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof characterised by thrust or thrust vector control servo-mechanisms or control devices therefor
    • 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
    • F02K9/90—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof characterised by thrust or thrust vector control using deflectors
    • 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
    • F02K9/97—Rocket nozzles
    • F02K9/978—Closures for nozzles; Nozzles comprising ejectable or discardable elements
    • 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
    • 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
    • F42B10/66—Steering by varying intensity or direction of thrust
    • F42B10/665—Steering by varying intensity or direction of thrust characterised by using a nozzle provided with at least a deflector mounted within the nozzle

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
DE69611940T 1995-05-26 1996-05-15 Verfahren und Steuerungssystem für die Leitschaufeln eines Flugkörpers Expired - Lifetime DE69611940T2 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US08/452,211 US5806791A (en) 1995-05-26 1995-05-26 Missile jet vane control system and method

Publications (2)

Publication Number Publication Date
DE69611940D1 DE69611940D1 (de) 2001-04-05
DE69611940T2 true DE69611940T2 (de) 2001-06-13

Family

ID=23795545

Family Applications (1)

Application Number Title Priority Date Filing Date
DE69611940T Expired - Lifetime DE69611940T2 (de) 1995-05-26 1996-05-15 Verfahren und Steuerungssystem für die Leitschaufeln eines Flugkörpers

Country Status (9)

Country Link
US (1) US5806791A (de)
EP (2) EP0878688B1 (de)
AU (1) AU686050B2 (de)
CA (1) CA2176048C (de)
DE (1) DE69611940T2 (de)
ES (1) ES2154487T3 (de)
IL (1) IL118251A (de)
NO (1) NO309668B1 (de)
TR (1) TR961035A2 (de)

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US5631830A (en) 1995-02-03 1997-05-20 Loral Vought Systems Corporation Dual-control scheme for improved missle maneuverability
DE19632893C2 (de) * 1996-08-16 2001-02-08 Industrieanlagen Betr Sgmbh Ia Verfahren zur Herstellung von Flugkörperkomponenten aus faserverstärkter Keramik
DE19640540C1 (de) * 1996-10-01 1998-04-02 Daimler Benz Aerospace Ag Ruderstellsystem für einen Lenkflugkörper
US6308911B1 (en) 1998-10-30 2001-10-30 Lockheed Martin Corp. Method and apparatus for rapidly turning a vehicle in a fluid medium
US6668542B2 (en) 1999-10-27 2003-12-30 Allison Advanced Development Company Pulse detonation bypass engine propulsion pod
US6584764B2 (en) 2000-01-12 2003-07-01 Allison Advanced Development Company Propulsion module
US6450443B1 (en) 2000-08-17 2002-09-17 The United States Of America As Represented By The Secretary Of The Navy High torque 2.75-inch rocket nozzle
US6548794B2 (en) 2001-03-13 2003-04-15 Raytheon Company Dissolvable thrust vector control vane
DE10210433C1 (de) * 2002-03-09 2003-08-14 Dornier Gmbh Fluggerät zur IR-Flugzieldarstellung
US6726147B1 (en) * 2003-05-15 2004-04-27 Moog Inc. Multi-function actuator, and method of operating same
NO318772B1 (no) * 2003-09-24 2005-05-02 Nammo Raufoss As Rakettmotor med styrevinger i motorens dyse
DE102004037487A1 (de) * 2004-07-27 2006-03-23 Deutsches Zentrum für Luft- und Raumfahrt e.V. Strahlruder und Verfahren zur Herstellung eines Strahlruders
US7026540B1 (en) * 2005-04-04 2006-04-11 The United States Of America As Represented By The Secretary Of The Navy Tailcone assembly for a submarine countermeasure
US7509903B2 (en) 2005-04-08 2009-03-31 Raytheon Company Separable structure material
FR2891618B1 (fr) * 2005-10-05 2010-06-11 Giat Ind Sa Dispositif d'entrainement de gouvernes de projectile.
EP1934547B1 (de) * 2005-10-13 2012-12-12 Raytheon Company Auslassanordnung für massenausstoss-antriebssystem
US7800032B1 (en) * 2006-11-30 2010-09-21 Raytheon Company Detachable aerodynamic missile stabilizing system
US7755012B2 (en) 2007-01-10 2010-07-13 Hr Textron, Inc. Eccentric drive control actuation system
US8193754B2 (en) * 2007-07-10 2012-06-05 Omnitek Partners Llc Mechanical stepper motors
US9341453B2 (en) * 2007-07-10 2016-05-17 Omnitek Partners, Llc Mechanical stepper motors for guided munitions and industrial machinery
US8117847B2 (en) 2008-03-07 2012-02-21 Raytheon Company Hybrid missile propulsion system with reconfigurable multinozzle grid
US8387360B2 (en) * 2008-05-21 2013-03-05 Raytheon Company Integral thrust vector and roll control system
EP3789725A1 (de) 2009-02-02 2021-03-10 Aerovironment Multimodales unbemanntes fluggerät
DE102009013150B4 (de) 2009-03-06 2011-05-05 Deutsches Zentrum für Luft- und Raumfahrt e.V. Bauteil zum Einsatz in Heißgasströmungen
CA2789722C (en) 2009-09-09 2018-08-28 Aerovironment, Inc. Systems and devices for remotely operated unmanned aerial vehicle report-suppressing launcher with portable rf transparent launch tube
CN106800085B (zh) * 2009-09-09 2020-08-18 威罗门飞行公司 升降副翼控制系统
US8436285B2 (en) * 2010-07-26 2013-05-07 Raytheon Company Projectile that includes a fin adjustment mechanism with changing backlash
KR101244490B1 (ko) * 2010-10-27 2013-03-18 최용준 제트베인 분리식 발사체의 방향 조종 장치
CN104089546B (zh) * 2014-04-29 2015-09-30 北京理工大学 弹体的可变气动布局结构
KR101603154B1 (ko) 2014-08-26 2016-03-14 국방과학연구소 제트베인 분리가 가능한 통합형 구동장치
JP6361404B2 (ja) * 2014-09-17 2018-07-25 三菱重工業株式会社 推力偏向装置、および、推力偏向装置を備える飛しょう体
FR3041744B1 (fr) * 2015-09-29 2018-08-17 Nexter Munitions Projectile d'artillerie ayant une phase pilotee.
US10222189B2 (en) * 2016-07-22 2019-03-05 Raytheon Company Stage separation mechanism and method
CN107416213B (zh) * 2017-05-16 2020-03-24 上海航天控制技术研究所 一种带燃气舵的飞行器尾端防火结构
US10112691B1 (en) * 2017-06-12 2018-10-30 The Boeing Company Releasable forward section of an underwater vehicle
CN108915901B (zh) * 2018-07-26 2021-04-20 西安航天动力技术研究所 一种柔性喷管固定体与扩张段防错位结构及方法
RU2740978C1 (ru) * 2020-02-10 2021-01-22 Акционерное общество Московский научно-производственный комплекс "Авионика" имени О.В. Успенского (АО МНПК "Авионика") Блок рулевых приводов ракеты или снаряда
CN111946461A (zh) * 2020-07-27 2020-11-17 山东鑫聚龙动力科技集团有限公司 一种航天发动机用翼轴及其制造工艺
US11733011B2 (en) * 2020-11-24 2023-08-22 Raytheon Company Steering system with power take-off from actuators
US11879416B1 (en) 2022-09-09 2024-01-23 Raytheon Company Method for reducing jet tab exposure during thrust vectoring

Family Cites Families (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
BE520064A (de) *
US2654552A (en) * 1948-02-24 1953-10-06 Northrop Aircraft Inc Movable jet deflector to compensate for destabilizing moment in a jet aircraft
US5082202A (en) * 1975-01-06 1992-01-21 The United States Of America As Represented By The Secretary Of The Navy Droppable jet vane TVC
US4063685A (en) * 1976-07-30 1977-12-20 The United States Of America As Represented By The Secretary Of The Army Thrust vector control by circulation control over aerodynamic surfaces in a supersonic nozzle
GB2164612B (en) * 1979-09-10 1986-09-03 British Aerospace Vehicles fitted with thrust vector control systems
US4364530A (en) * 1980-09-08 1982-12-21 The United States Of America As Represented By The Secretary Of The Navy Propulsion/control modular booster
NZ198917A (en) * 1980-11-14 1985-01-31 Commw Of Australia Rocket controlled by spoiler tabs in exhaust
DE3138869C2 (de) * 1981-09-30 1984-07-12 Messerschmitt-Bölkow-Blohm GmbH, 8000 München "Lenkflugkörper"
US4561357A (en) * 1982-09-15 1985-12-31 General Dynamics Pomona Division Steering mechanism for an explosively fired projectile
US4844380A (en) * 1985-11-25 1989-07-04 Hughes Aircraft Company Detachable thrust vector mechanism for an aeronautical vehicle
US4913379A (en) * 1988-02-23 1990-04-03 Japan as represented by Director General, Technical Research and Development Institute, Japan Defence Agency Rocket flight direction control system
US4867393A (en) * 1988-08-17 1989-09-19 Morton Thiokol, Inc. Reduced fin span thrust vector controlled pulsed tactical missile
US5511745A (en) * 1994-12-30 1996-04-30 Thiokol Corporation Vectorable nozzle having jet vanes

Also Published As

Publication number Publication date
AU686050B2 (en) 1998-01-29
EP0744591A2 (de) 1996-11-27
NO309668B1 (no) 2001-03-05
IL118251A0 (en) 1996-09-12
AU5224096A (en) 1996-12-05
US5806791A (en) 1998-09-15
DE69611940D1 (de) 2001-04-05
NO962105D0 (no) 1996-05-23
EP0744591A3 (de) 1997-12-03
EP0878688B1 (de) 2001-02-28
EP0878688A1 (de) 1998-11-18
CA2176048A1 (en) 1996-11-27
CA2176048C (en) 2000-02-29
TR961035A2 (tr) 1996-12-21
IL118251A (en) 1998-04-05
NO962105L (no) 1996-11-27
ES2154487T3 (es) 2001-04-01

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Legal Events

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8364 No opposition during term of opposition