ES2017567A6 - Aparato para acoplar un conductor de fibra optica a un objeto en movimiento, un retenedor para guiar un filamento de fibra optica y un metodo para largar una guia de fibra optica. - Google Patents

Aparato para acoplar un conductor de fibra optica a un objeto en movimiento, un retenedor para guiar un filamento de fibra optica y un metodo para largar una guia de fibra optica.

Info

Publication number
ES2017567A6
ES2017567A6 ES8903924A ES8903924A ES2017567A6 ES 2017567 A6 ES2017567 A6 ES 2017567A6 ES 8903924 A ES8903924 A ES 8903924A ES 8903924 A ES8903924 A ES 8903924A ES 2017567 A6 ES2017567 A6 ES 2017567A6
Authority
ES
Spain
Prior art keywords
leader
channel
missile
stiffened
fiberoptic
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
ES8903924A
Other languages
English (en)
Inventor
Daniel K Schotter
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
Hughes Aircraft 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 Hughes Aircraft Co filed Critical Hughes Aircraft Co
Publication of ES2017567A6 publication Critical patent/ES2017567A6/es
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • G—PHYSICS
    • G02—OPTICS
    • G02B—OPTICAL ELEMENTS, SYSTEMS OR APPARATUS
    • G02B6/00—Light guides; Structural details of arrangements comprising light guides and other optical elements, e.g. couplings
    • G02B6/44—Mechanical structures for providing tensile strength and external protection for fibres, e.g. optical transmission cables
    • G02B6/4439—Auxiliary devices
    • G02B6/4471—Terminating devices ; Cable clamps
    • G02B6/4478—Bending relief means
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41—WEAPONS
    • F41G—WEAPON SIGHTS; AIMING
    • F41G7/00—Direction control systems for self-propelled missiles
    • F41G7/20—Direction control systems for self-propelled missiles based on continuous observation of target position
    • F41G7/30—Command link guidance systems
    • F41G7/32—Command link guidance systems for wire-guided missiles
    • 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
    • F42B15/01—Arrangements thereon for guidance or control
    • F42B15/04—Arrangements thereon for guidance or control using wire, e.g. for guiding ground-to-ground rockets

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Optics & Photonics (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Light Guides In General And Applications Therefor (AREA)
  • Laying Of Electric Cables Or Lines Outside (AREA)
  • Earth Drilling (AREA)
  • Supports For Pipes And Cables (AREA)

Abstract

APARATO PARA ACOPLAR UN CONDUCTO DE FIBRA OPTICA A UN OBJETO EN MOVIMIENTO, UN RETENEDOR PARA GUIAR UN FILAMENTO DE FIBRA OPTICA Y UN METODO PARA LARGAR UNA GUIA DE FIBRA ENTRE UN MISIL Y UN TUBO DE LANZAMIENTO. UNA GUIA FIRBROOPTICA (20) ES ALARGADA, AL LANZARSE UN MISIL CON UN GRADO CONTROLADO DE CURVATURA DEL FILAMENTO FIBROOPTIMA. Y ESTA ADEMAS PROTEGIDA CONTRA LOS EFECTOS DEL CHORRO DE PROPULSION DURANTE EL LANZAMIENTO. EL FILAMENTO FIBROOPTICO ES RIGIDIZADO DENTRO DE UNA GUIA (30). UN REVESTIMIENTO PROTECTOR DE ALAMBRES LONGITUDINALES, DE ALTA RESISTENCIA A LA TRACCION, ESTA DISPUESTO ALREDEDOR DE UN MANGUITO ENVOLVIENDOLO, Y, A SU VEZ, ESTA ENVUELTO POR UN MANGUITO EXTERIOR. LA GUIA RIGIDIZADA ES CONDUCIDA A LO LARGO DE UN RETENEDOR (20) UNIDO AL COSTADO DEL MISIL. EL RETENEDOR (20) ESTA DISPUESTO EN UN CANAL SOBRE UNA PARTE LONGITUDINAL DEL MISIL. LA GUIA RIGIDIZADA ES CONDUCIDA A LO LARGO DE UN RETENEDOR (20) UNIDO AL COSTADO DEL MISIL. EL RETENEDOR (20) ESTA DISPUESTO EN UN CANALSOBRE UNA PARTE LONGITUDINAL DEL MISIL. LA GUIA RIGIDIZADA (20) SE TIENDE CONTRA UNO DE LOS BRAZOS RETENEDORES, Y BAJO EL, DESDE EL EXTREMO TRASERO DEL MISIL (10), EN DONDE LA GUIA FIBROOPTICA (30) ES EXPULSADA DURANTE EL LANZAMIENTO, HASTA EL EXTREMO DELANTERO DEL MISIL (10) Y DEL RETENEDOR (20).
ES8903924A 1988-11-18 1989-11-17 Aparato para acoplar un conductor de fibra optica a un objeto en movimiento, un retenedor para guiar un filamento de fibra optica y un metodo para largar una guia de fibra optica. Expired - Lifetime ES2017567A6 (es)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US07/273,310 US5022607A (en) 1988-11-18 1988-11-18 Bend limiting stiff leader and retainer system

Publications (1)

Publication Number Publication Date
ES2017567A6 true ES2017567A6 (es) 1991-02-16

Family

ID=23043403

Family Applications (1)

Application Number Title Priority Date Filing Date
ES8903924A Expired - Lifetime ES2017567A6 (es) 1988-11-18 1989-11-17 Aparato para acoplar un conductor de fibra optica a un objeto en movimiento, un retenedor para guiar un filamento de fibra optica y un metodo para largar una guia de fibra optica.

Country Status (12)

Country Link
US (1) US5022607A (es)
EP (1) EP0396706B1 (es)
JP (1) JP2749413B2 (es)
KR (1) KR950004544B1 (es)
AU (1) AU620173B2 (es)
CA (1) CA2000672C (es)
DE (1) DE68912931T2 (es)
EG (1) EG19935A (es)
ES (1) ES2017567A6 (es)
IL (1) IL92072A (es)
NO (1) NO180131C (es)
WO (1) WO1990005888A1 (es)

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5031997A (en) * 1990-03-28 1991-07-16 Hughes Aircraft Company Open breech hot launched fiber optic payout system
US5213280A (en) * 1991-03-14 1993-05-25 Hughes Aircraft Company Linear payout leader holder
US5385319A (en) * 1993-11-22 1995-01-31 Hughes Missile Systems Company Missile with inside payout optical fiber canister
GB9401221D0 (en) * 1994-01-22 2007-01-10 British Aerospace Missile launch apparatus
DE4414737C1 (de) * 1994-04-27 1996-01-04 Daimler Benz Aerospace Ag Vorrichtung zur Fernsteuerung von Flugkörpern oder Torpedos
US6502522B1 (en) * 1998-12-21 2003-01-07 The United States Of America As Represented By The Secretary Of The Navy Coil restraint device

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
NL6411455A (es) * 1963-10-16 1965-04-20
US3703874A (en) * 1970-07-15 1972-11-28 Us Navy Flexible hose wire payout system
DE3046575C2 (de) * 1980-12-11 1982-12-02 Messerschmitt-Bölkow-Blohm GmbH, 8000 München Lenkkabel für einen mit Lichtsignalen fernlenkbaren Flugkörper
US4573647A (en) * 1984-05-30 1986-03-04 The United States Of America As Represented By The Secretary Of The Army Fiber deployment mechanism
US4886562A (en) * 1987-03-31 1989-12-12 The Boeing Company Method of manufacturing reinforced optical fiber
US4796833A (en) * 1987-03-31 1989-01-10 The Boeing Company Optical fiber guided tube-launched projectile system
US4770370A (en) * 1987-03-31 1988-09-13 The Boeing Company Optical fiber guided tube-launched projectile system

Also Published As

Publication number Publication date
WO1990005888A1 (en) 1990-05-31
JP2749413B2 (ja) 1998-05-13
US5022607A (en) 1991-06-11
NO180131B (no) 1996-11-11
NO903171L (no) 1990-07-16
DE68912931T2 (de) 1994-05-19
KR900702320A (ko) 1990-12-06
CA2000672C (en) 1994-04-19
NO903171D0 (no) 1990-07-16
JPH03502360A (ja) 1991-05-30
EP0396706B1 (en) 1994-02-02
KR950004544B1 (ko) 1995-05-02
EG19935A (en) 1996-10-31
AU620173B2 (en) 1992-02-13
AU4518189A (en) 1990-06-12
DE68912931D1 (de) 1994-03-17
NO180131C (no) 1997-02-19
IL92072A (en) 1994-05-30
CA2000672A1 (en) 1990-05-18
EP0396706A1 (en) 1990-11-14

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Legal Events

Date Code Title Description
SA6 Expiration date (snapshot 920101)

Free format text: 2009-11-17

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