ES2175634T3 - AUTOMATIC GOVERNMENT DEVICE OF AT LEAST ONE MOBILE ELEMENT, SUCH AS A VENTRAL MISSILE DERIVA. - Google Patents

AUTOMATIC GOVERNMENT DEVICE OF AT LEAST ONE MOBILE ELEMENT, SUCH AS A VENTRAL MISSILE DERIVA.

Info

Publication number
ES2175634T3
ES2175634T3 ES98402267T ES98402267T ES2175634T3 ES 2175634 T3 ES2175634 T3 ES 2175634T3 ES 98402267 T ES98402267 T ES 98402267T ES 98402267 T ES98402267 T ES 98402267T ES 2175634 T3 ES2175634 T3 ES 2175634T3
Authority
ES
Spain
Prior art keywords
missile
deriva
ventral
organ
mobile element
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
ES98402267T
Other languages
Spanish (es)
Inventor
Jean-Marie Thyssens
Philippe Bertin
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.)
Aerospatiale Matra
Original Assignee
Aerospatiale Matra
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 Aerospatiale Matra filed Critical Aerospatiale Matra
Application granted granted Critical
Publication of ES2175634T3 publication Critical patent/ES2175634T3/en
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
    • F42B15/00—Self-propelled projectiles or missiles, e.g. rockets; Guided missiles
    • F42B15/36—Means for interconnecting rocket-motor and body section; Multi-stage connectors; Disconnecting means

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Combustion & Propulsion (AREA)
  • General Engineering & Computer Science (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Bidet-Like Cleaning Device And Other Flush Toilet Accessories (AREA)

Abstract

UN DISPOSITIVO DE CONTROL (18) ESTA TOTALMENTE INTEGRADO EN EL CUERPO DE UN MISIL, ENFRENTE DE UN PISTON EYECTOR QUE PERTENECE AL MASTIL PORTADOR, POR EL CUAL EL MISIL ESTA CONECTADO A UNA AERONAVE. EL PISTON EYECTOR ACTUA SOBRE UN ORGANO DE DESBLOQUEO (29), NORMALMENTE MANTENIDO EN POSICION DE REPOSO POR UN ORGANO DE BLOQUEO COMO UN PASADOR ROMPIBLE (44). EL ACCIONAMIENTO DEL PISTON EYECTOR TIENE COMO EFECTO UN CIZALLADO DEL PASADOR (44) Y UN DESPLAZAMIENTO DEL ORGANO DE DESBLOQUEO EN UNA POSICION TAL QUE SE LIBERA UN PISTON PERCUTOR (58). SE ENCIENDE ENTONCES UNA LINEA PIROTECNICA DE CONTROL DEL DESPLIEGUE DE LOS PLANOS DE DERIVA VENTRALES DEL MISIL.A CONTROL DEVICE (18) IS FULLY INTEGRATED IN THE BODY OF A MISSILE, IN FRONT OF AN EJECTOR PISTON BELONGING TO THE MASTIL CARRIER, BY WHICH THE MISSILE IS CONNECTED TO AN AIRCRAFT. THE EJECTOR PISTON ACTS ON AN UNBLOCKING ORGAN (29), NORMALLY MAINTAINED IN A POSITION OF A BLOCK ORGAN AS A BREAKABLE PIN (44). THE OPERATION OF THE EJECTOR PISTON HAS THE EFFECT OF A SHEAR OF THE PIN (44) AND A DISPLACEMENT OF THE UNLOCK ORGAN IN A POSITION THAT IS RELEASED A PISTON PERCUTOR (58). THEN A PIROTECHNICAL LINE OF CONTROL OF THE DEPLOYMENT OF THE VENTRAL DERIVA PLANS OF THE MISIL IS ON.

ES98402267T 1997-09-16 1998-09-15 AUTOMATIC GOVERNMENT DEVICE OF AT LEAST ONE MOBILE ELEMENT, SUCH AS A VENTRAL MISSILE DERIVA. Expired - Lifetime ES2175634T3 (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR9711493A FR2768503B1 (en) 1997-09-16 1997-09-16 DEVICE FOR AUTOMATICALLY CONTROLLING AT LEAST ONE MOBILE ELEMENT SUCH AS A VENTRAL MISSILE DRIFT

Publications (1)

Publication Number Publication Date
ES2175634T3 true ES2175634T3 (en) 2002-11-16

Family

ID=9511116

Family Applications (1)

Application Number Title Priority Date Filing Date
ES98402267T Expired - Lifetime ES2175634T3 (en) 1997-09-16 1998-09-15 AUTOMATIC GOVERNMENT DEVICE OF AT LEAST ONE MOBILE ELEMENT, SUCH AS A VENTRAL MISSILE DERIVA.

Country Status (5)

Country Link
EP (1) EP0908696B1 (en)
DE (1) DE69805034T2 (en)
ES (1) ES2175634T3 (en)
FR (1) FR2768503B1 (en)
NO (1) NO317638B1 (en)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110775277B (en) * 2019-12-06 2024-04-19 中国工程物理研究院总体工程研究所 Unmanned aerial vehicle airborne microminiature missile throwing and separating device with synchronism
CN115493462A (en) * 2022-08-29 2022-12-20 中国兵器工业第二一三研究所 Cross-shaped four-way missile wing synchronous unlocking mechanism

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2261173C3 (en) 1972-12-14 1979-06-13 Messerschmitt-Boelkow-Blohm Gmbh, 8000 Muenchen Device for detachable fixing
DE2648523C3 (en) * 1976-10-27 1979-09-27 Messerschmitt-Boelkow-Blohm Gmbh, 8000 Muenchen Sliding projectile with ejectable keel fin
DE2827781C2 (en) * 1978-06-24 1985-11-14 Messerschmitt-Bölkow-Blohm GmbH, 8012 Ottobrunn Coupling head for external loads on aircraft
US5141175A (en) * 1991-03-22 1992-08-25 Harris Gordon L Air launched munition range extension system and method

Also Published As

Publication number Publication date
DE69805034T2 (en) 2002-11-28
DE69805034D1 (en) 2002-05-29
FR2768503A1 (en) 1999-03-19
NO317638B1 (en) 2004-11-29
EP0908696A1 (en) 1999-04-14
EP0908696B1 (en) 2002-04-24
NO984215L (en) 1999-03-17
FR2768503B1 (en) 1999-12-03
NO984215D0 (en) 1998-09-11

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