ES2013541A6 - Dispositivo para un lanzador en un vehiculo aereo. - Google Patents

Dispositivo para un lanzador en un vehiculo aereo.

Info

Publication number
ES2013541A6
ES2013541A6 ES8902023A ES8902023A ES2013541A6 ES 2013541 A6 ES2013541 A6 ES 2013541A6 ES 8902023 A ES8902023 A ES 8902023A ES 8902023 A ES8902023 A ES 8902023A ES 2013541 A6 ES2013541 A6 ES 2013541A6
Authority
ES
Spain
Prior art keywords
launcher
profile
missile
longitudinal direction
shims
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
ES8902023A
Other languages
English (en)
Inventor
Hans Norrvi
Arne Warnstrom
Jean Erik Wuopio
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.)
Saab Missiles AB
Original Assignee
Saab Missiles AB
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 Saab Missiles AB filed Critical Saab Missiles AB
Publication of ES2013541A6 publication Critical patent/ES2013541A6/es
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41—WEAPONS
    • F41F—APPARATUS FOR LAUNCHING PROJECTILES OR MISSILES FROM BARRELS, e.g. CANNONS; LAUNCHERS FOR ROCKETS OR TORPEDOES; HARPOON GUNS
    • F41F3/00—Rocket or torpedo launchers
    • F41F3/04—Rocket or torpedo launchers for rockets
    • F41F3/0406—Rail launchers
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D7/00—Arrangements of military equipment, e.g. armaments, armament accessories, or military shielding, in aircraft; Adaptations of armament mountings for aircraft
    • B64D7/08—Arrangements of rocket launchers or releasing means

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Connection Of Plates (AREA)
  • Catching Or Destruction (AREA)

Abstract

DISPOSITIVO PARA UN LANZADOR EN UN VEHICULO AEREO. EL LANZADOR INCLUYE MEDIOS PARA EL TRANSPORTE SEPARABLE DEL MISIL Y MEDIOS PARA GUIAR EL MISIL EN LA DIRECCION LONGITUDINAL DEL LANZADOR. LOS ULTIMOS COMPRENDEN UN PRIMER ELEMENTO (2) DE PERFIL UNIDO AL LANZADOR Y UN SEGUNDO ELEMENTO (4) DE PERFIL UNIDO AL MISIL. EL DISPOSITIVO SE CARACTERIZA, EN PARTICULAR, PORQUE INCLUYE UNA PLACA DE PERFIL (7) Y PREFERENTEMENTE CIERTAS LAMINAS DE SUPLEMENTO (8) RELATIVAMENTE DELGADAS, ESTANDO LA PLACA DE PERFIL (7) Y LAS LAMINAS DE SUPLEMENTO DISPUESTAS DE MANERA ASEGURABLE EN EL PRIMER ELEMENTO (2) DE PERFIL PARA LIMITAR ASI EL MOVIMIENTO MUTUO ENTRE LOS ELEMENTOS DE PERFIL PRIMERO (2) Y SEGUNDO (4) AL DESPLAZAR LA CARGA TRANSVERSALMENTE A LA DIRECCION LONGITUDINAL DEL LANZADOR, MANTENIENDO LA HOLGURA REQUERIDA ENTRE LOS ELEMENTOS DE PERFIL (2, 4) PARA LA MOVILIDAD MUTUA ENTRE LOS ELEMENTOS DE PERFIL EN LA DIRECCION LONGITUDINAL DEL LANZADOR. EL DISPOSITIVO ESTA DESTINADO A TRANSPORTAR DE MANERA SEPARABLE Y GUIAR UN MISIL O SIMILAR.
ES8902023A 1988-06-10 1989-06-09 Dispositivo para un lanzador en un vehiculo aereo. Expired - Lifetime ES2013541A6 (es)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
SE8802168A SE461176B (sv) 1988-06-10 1988-06-10 Anordning vid lavett vid luftfarkost foer loesbar uppbaerning och styrning av robot eller liknande

Publications (1)

Publication Number Publication Date
ES2013541A6 true ES2013541A6 (es) 1990-05-01

Family

ID=20372577

Family Applications (1)

Application Number Title Priority Date Filing Date
ES8902023A Expired - Lifetime ES2013541A6 (es) 1988-06-10 1989-06-09 Dispositivo para un lanzador en un vehiculo aereo.

Country Status (7)

Country Link
US (1) US4976183A (es)
EP (1) EP0379539B1 (es)
AU (1) AU611306B2 (es)
CA (1) CA1308949C (es)
ES (1) ES2013541A6 (es)
SE (1) SE461176B (es)
WO (1) WO1989012210A1 (es)

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5201808A (en) * 1992-02-10 1993-04-13 Telectronics Pacing Systems, Inc. Minute volume rate-responsive pacemaker employing impedance sensing on a unipolar lead
DE19600494C2 (de) * 1996-01-09 2002-11-28 Bodenseewerk Geraetetech Gleitschuh zur Führung eines Flugkörpers in einem Startgerät
GB0100277D0 (en) 2001-01-05 2001-02-14 Flight Refueling Ltd Release suspension for an airborne store
WO2004108529A2 (en) * 2003-03-06 2004-12-16 Drs Training & Control Systems, Inc. Hanger assembly for aircraft
IL165812A (en) * 2004-12-16 2011-09-27 Rafael Advanced Defense Sys Mitla hung up

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2981150A (en) * 1954-06-15 1961-04-25 Jr Arthur H Miller Launcher
US2940362A (en) * 1956-06-22 1960-06-14 Charles N Paxton Missile launcher adapter
US3668970A (en) * 1958-07-22 1972-06-13 Secr Defence Rocket launchers
US3040629A (en) * 1960-04-11 1962-06-26 Garnett C Duncan Missile launcher
US4155286A (en) * 1977-12-01 1979-05-22 Mihm John J Wedge clamp for missile launcher
DE3016925A1 (de) * 1980-05-02 1981-11-12 Dornier Gmbh, 7990 Friedrichshafen Starteinrichtung zum tragen und starten von flugkoerpern, insbesondere fuer luftfahrzeuge
GB2166526B (en) * 1984-10-30 1988-05-25 Nash Frazer Ltd Airborne missile launcher
US4750404A (en) * 1987-04-06 1988-06-14 Varo, Inc. Aircraft missile launcher snubber apparatus

Also Published As

Publication number Publication date
AU611306B2 (en) 1991-06-06
SE461176B (sv) 1990-01-15
SE8802168D0 (sv) 1988-06-10
EP0379539A1 (en) 1990-08-01
CA1308949C (en) 1992-10-20
AU3752889A (en) 1990-01-05
EP0379539B1 (en) 1993-03-24
US4976183A (en) 1990-12-11
WO1989012210A1 (en) 1989-12-14

Similar Documents

Publication Publication Date Title
ES8503088A1 (es) Perfeccionamientos en un accionador electrico
FR2437763A1 (fr) Harnais de cables
DE68924473D1 (de) Übertragungssteuerung für geheime Dokumente.
IT8821724A0 (it) Copertura per un dispositivo di protezione con involucro a gas dagli urti in autoveicoli, applicato sul lato del guidatore.
GB1557371A (en) Control system for lift trucks or the like
EP0180310A3 (en) Clamping means for a strap
IT8567331A1 (it) Dispositivo di comando di mezzi attuatori montati su un veicolo.
ES2012744A4 (es) Metodo y aparato para manipular ropas en percheros
DE68915532D1 (de) Regelungssystem des aufhängungskolbens für fahrzeuge.
ES2013541A6 (es) Dispositivo para un lanzador en un vehiculo aereo.
CA2017928A1 (en) Fastening element carrier strip
DE68922774D1 (de) Ladesteuerverfahren für Fahrzeuge.
IT1169824B (it) Dispositivo d'idrottero stabilizzato da impennaggio,e veicolo nautico munito di tale dispositivo
JPS52141706A (en) Control system for adjusting member having dead time
IL67567A (en) Hydraulic control and feedback arrangement particularly for aircraft flap activation system
NO950169L (no) Undervannsfartöy
MY100588A (en) A device for selectively preventing one or more modes of actuating manual control members equipping an apparatus.
DE3661572D1 (en) Positioning motor
EP0371505A3 (en) Linear driving apparatus
IT8421212A0 (it) Meccanismo per regolare un mezzo che comanda un flusso d'aria specialmente in un autoveicolo.
DE68920489D1 (de) Sicherheits- und Regulierventil für Gas.
DE3564976D1 (en) An electrically actuated lock and control system for application to vehicles
DE3853149D1 (de) Sicherheitsvorrichtung für Fahrzeuge.
GB2197149B (en) The optical-electronic system for the determination of the direction and of the speed of a moving vehicle by means of the internal emisson of laser beams
ATE107410T1 (de) Vorrichtung für die korrektur einer flugbahn.

Legal Events

Date Code Title Description
FD1A Patent lapsed

Effective date: 20020603