ES2046862T3 - Sistema para el pilotaje de un misil mediante toberas laterales. - Google Patents

Sistema para el pilotaje de un misil mediante toberas laterales.

Info

Publication number
ES2046862T3
ES2046862T3 ES199191400520T ES91400520T ES2046862T3 ES 2046862 T3 ES2046862 T3 ES 2046862T3 ES 199191400520 T ES199191400520 T ES 199191400520T ES 91400520 T ES91400520 T ES 91400520T ES 2046862 T3 ES2046862 T3 ES 2046862T3
Authority
ES
Spain
Prior art keywords
shutter
missile
gas
piston
nozzles
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
ES199191400520T
Other languages
English (en)
Inventor
Jean-Pierre Morgand
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.)
Airbus Group SAS
Original Assignee
Airbus Group SAS
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 Airbus Group SAS filed Critical Airbus Group SAS
Application granted granted Critical
Publication of ES2046862T3 publication Critical patent/ES2046862T3/es
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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
    • F42B10/66—Steering by varying intensity or direction of thrust
    • F42B10/663—Steering by varying intensity or direction of thrust using a plurality of transversally acting auxiliary nozzles, which are opened or closed by valves

Landscapes

  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
  • Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)
  • Nozzles (AREA)
  • Jet Pumps And Other Pumps (AREA)

Abstract

SISTEMA PARA EL CONTROL DE UN MISIL (1) POR MEDIO DE CHORROS GASEOSOS, QUE COMPRENDE UN GENERADOR DE GAS SUSCEPTIBLE DE SER CONECTADO A AL MENOS UN PAR DE TOBERAS LATERALES (8) MEDIANTE ELEMENTOS DE OBTURACION ROTATIVOS (14), MOVILES BAJO LA ACCION DE MEDIOS MOTORES (30) Y QUE ACCIONAN EL PASO DE LOS GASES A TRAVES DE DICHAS TOBERAS. SEGUN LA INVENCION: RA (8) ESTA ASOCIADO UN OBTURADOR ROTATIVO INDIVIDUAL (14); CADA OBTURADOR (14) ESTA ACCIONADO EN ROTACION POR UN PISTON (31) DE UN GATO (30) QUE DIVIDE EN DOS CAMARAS (38A, 38B) DE SECCIONES DIFERENTES QUE RECIBEN CADA UNA, UNA PARTE DEL GAS GENERADO POR DICHO GENERADOR DE GAS Y SIENDO ACCIONADA LA POSICION DE DICHO PISTON POR EL CONTROL DEL VOLUMEN DE DICHO GAS A TRAVES DE LA CAMARA (38A) DE MAYOR SECCION; Y ES (14) ESTAN CONECTADOS EL UNO AL OTRO POR UN ENLACE MECANICO (50) DE TAL MANERA QUE, CUANDO UN OBTURADOR GIRA EN UN SENTIDO, EL OTRO OBTURADOR GIRE EN EL SENTIDO OPUESTO Y TENIENDO LA MISMA AMPLITUD ANGULAR.
ES199191400520T 1990-03-14 1991-02-26 Sistema para el pilotaje de un misil mediante toberas laterales. Expired - Lifetime ES2046862T3 (es)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR909003252A FR2659733B1 (fr) 1990-03-14 1990-03-14 Systeme pour le pilotage d'un missile au moyen de tuyeres laterales.

Publications (1)

Publication Number Publication Date
ES2046862T3 true ES2046862T3 (es) 1994-02-01

Family

ID=9394722

Family Applications (1)

Application Number Title Priority Date Filing Date
ES199191400520T Expired - Lifetime ES2046862T3 (es) 1990-03-14 1991-02-26 Sistema para el pilotaje de un misil mediante toberas laterales.

Country Status (8)

Country Link
US (1) US5074492A (es)
EP (1) EP0447283B1 (es)
JP (1) JP3181930B2 (es)
AU (1) AU631969B2 (es)
CA (1) CA2038091C (es)
DE (1) DE69100454T2 (es)
ES (1) ES2046862T3 (es)
FR (1) FR2659733B1 (es)

Families Citing this family (19)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2659734B1 (fr) * 1990-03-14 1992-07-03 Aerospatiale Systeme pour le pilotage d'un missile au moyen de jets gazeux lateraux.
WO1994010527A1 (fr) * 1992-10-23 1994-05-11 Arkhangelsky Ivan I Procede de guidage d'un missile et son dispositif de mise en ×uvre
FR2699610B1 (fr) * 1992-12-22 1995-02-10 Aerospatiale Dispositif d'actionnement d'un organe mécanique, notamment pour le pilotage en force d'un missile, et missile équipé dudit dispositif.
US6254031B1 (en) * 1994-08-24 2001-07-03 Lockhead Martin Corporation Precision guidance system for aircraft launched bombs
US5631830A (en) 1995-02-03 1997-05-20 Loral Vought Systems Corporation Dual-control scheme for improved missle maneuverability
RU2125701C1 (ru) * 1998-03-16 1999-01-27 Государственное научно-производственное предприятие "Сплав" Ракета
US6308911B1 (en) 1998-10-30 2001-10-30 Lockheed Martin Corp. Method and apparatus for rapidly turning a vehicle in a fluid medium
RU2247926C1 (ru) * 2003-06-18 2005-03-10 Государственное унитарное предприятие "Конструкторское бюро приборостроения" Способ стабилизации ракеты в полете и ракета для его реализации
US7287725B2 (en) * 2005-04-25 2007-10-30 Raytheon Company Missile control system and method
US7856806B1 (en) * 2006-11-06 2010-12-28 Raytheon Company Propulsion system with canted multinozzle grid
US7872215B2 (en) * 2008-02-29 2011-01-18 Raytheon Company Methods and apparatus for guiding a projectile
US8269156B2 (en) 2008-03-04 2012-09-18 The Charles Stark Draper Laboratory, Inc. Guidance control system for projectiles
US8117847B2 (en) 2008-03-07 2012-02-21 Raytheon Company Hybrid missile propulsion system with reconfigurable multinozzle grid
US8338768B2 (en) 2008-10-15 2012-12-25 Honeywell International Inc. Actuation assembly
US8362408B2 (en) * 2009-10-22 2013-01-29 Honeywell International Inc. Steerable projectile charging system
FR2980265B1 (fr) * 2011-09-21 2017-02-24 Mbda France Systeme pour le pilotage d'un engin volant a l'aide de paires de tuyeres laterales
RU2485342C1 (ru) * 2012-02-20 2013-06-20 Российская Федерация, от имени которой выступает Министерство обороны Российской Федерации Силовой блок двигательной установки ракеты-носителя
US9068808B2 (en) * 2013-01-17 2015-06-30 Raytheon Company Air vehicle with bilateral steering thrusters
KR102134354B1 (ko) * 2020-04-16 2020-07-15 국방과학연구소 화염 차단 장치 및 이를 포함하는 유도 무기

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3136250A (en) * 1962-05-04 1964-06-09 Samuel A Humphrey Integrated auxiliary power unit
US4085909A (en) * 1976-10-04 1978-04-25 Ford Motor Company Combined warm gas fin and reaction control servo
FR2504252B1 (fr) * 1981-04-21 1987-03-06 Thomson Brandt Projectile guide
FR2536720A1 (fr) * 1982-11-29 1984-06-01 Aerospatiale Systeme pour le pilotage d'un missile au moyen de jets gazeux lateraux et missile comportant un tel systeme
FR2538098B1 (fr) * 1982-12-17 1987-11-20 Thomson Brandt Dispositif de pilotage par jets de gaz lateraux
FR2620812B1 (fr) * 1987-09-18 1992-04-17 Thomson Brandt Armements Dispositif de commutation de jets de gaz lateraux destine au pilotage d'engins
FR2622066B1 (fr) * 1987-10-16 1995-08-25 Rossi Rinaldo Machine electrique a entrefers radiaux

Also Published As

Publication number Publication date
JP3181930B2 (ja) 2001-07-03
CA2038091A1 (fr) 1991-09-15
FR2659733A1 (fr) 1991-09-20
FR2659733B1 (fr) 1994-07-01
DE69100454D1 (de) 1993-11-11
CA2038091C (fr) 2000-08-29
US5074492A (en) 1991-12-24
AU631969B2 (en) 1992-12-10
AU7136991A (en) 1991-09-19
JPH04222399A (ja) 1992-08-12
DE69100454T2 (de) 1994-03-03
EP0447283B1 (fr) 1993-10-06
EP0447283A1 (fr) 1991-09-18

Similar Documents

Publication Publication Date Title
ES2046862T3 (es) Sistema para el pilotaje de un misil mediante toberas laterales.
ES2044692T3 (es) Sistema para el pilotaje de un misil por medio de chorros de gas laterales.
ES2146292T3 (es) Valvula de control de presion de dos etapas.
US3952813A (en) Percussive device for driving holes in soil
ES2030879T3 (es) Aparato de inyeccion de liquido, sin aguja en particular para uso en cuidados dentales.
ES2097919T3 (es) Metodo para la combustion de liquidos residuales.
ES2139811T3 (es) Fijador de puerta para automoviles accionado por fuerza auxiliar continuamente.
ES2100649T3 (es) Armaduras regulables de asiento.
GB1524022A (en) Inflatable impact-absorbing protectors
ES2165145T3 (es) Accionamiento motorizado.
SE8803595L (sv) Maskin foer ett gasformigt medium
ES8204810A1 (es) Perfeccionamientos en un compresor rotatorio del tipo de pa-letas deslizantes
ES2102773T3 (es) Unas mejoras en y relativas a sistemas de recubrimiento en polvo y un aparato segun dicho sistema.
JPS55123797A (en) Enclosure for preventing invasion
US3718410A (en) Reversible pressure fluid actuated vane motor
ES2092359T3 (es) Sistema de cierre.
SE7704680L (sv) Pneumatisk slaganordning
AR022993A1 (es) Banco de prueba pirotecnica
DE60105883T8 (de) Panzerfahrzeugschutzvorrichtung gegen Wuchtgeschosse
ES419494A1 (es) Perfeccionamientos en las espoletas giratorias de rotor basculante.
ES2075786B1 (es) Motor rotativo.
SU386297A1 (es)
ES2160862T3 (es) Modulo de fijacion para airbag del acompañante.
SU990329A1 (ru) Пневматический вибровозбудитель
GB1031095A (en) Improvements in or relating to inflation devices for pneumatic tyres

Legal Events

Date Code Title Description
FG2A Definitive protection

Ref document number: 447283

Country of ref document: ES