ES2105533T3 - Misil con bote de fibra optica con desarrollo interior. - Google Patents

Misil con bote de fibra optica con desarrollo interior.

Info

Publication number
ES2105533T3
ES2105533T3 ES94308573T ES94308573T ES2105533T3 ES 2105533 T3 ES2105533 T3 ES 2105533T3 ES 94308573 T ES94308573 T ES 94308573T ES 94308573 T ES94308573 T ES 94308573T ES 2105533 T3 ES2105533 T3 ES 2105533T3
Authority
ES
Spain
Prior art keywords
fiber optic
package
fiber
coil
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
ES94308573T
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
Application granted granted Critical
Publication of ES2105533T3 publication Critical patent/ES2105533T3/es
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B65—CONVEYING; PACKING; STORING; HANDLING THIN OR FILAMENTARY MATERIAL
    • B65H—HANDLING THIN OR FILAMENTARY MATERIAL, e.g. SHEETS, WEBS, CABLES
    • B65H49/00—Unwinding or paying-out filamentary material; Supporting, storing or transporting packages from which filamentary material is to be withdrawn or paid-out
    • B65H49/02—Methods or apparatus in which packages do not rotate
    • 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
    • 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
    • G02B6/4457—Bobbins; Reels
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B65—CONVEYING; PACKING; STORING; HANDLING THIN OR FILAMENTARY MATERIAL
    • B65H—HANDLING THIN OR FILAMENTARY MATERIAL, e.g. SHEETS, WEBS, CABLES
    • B65H2701/00—Handled material; Storage means
    • B65H2701/30—Handled filamentary material
    • B65H2701/32—Optical fibres or optical cables

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Physics & Mathematics (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • General Physics & Mathematics (AREA)
  • Optics & Photonics (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Light Guides In General And Applications Therefor (AREA)

Abstract

UN MISIL INCLUYE UN CARRETE DE FIBRA OPTICA CON LA FIBRA OPTICA ENROLLADA COMO UN PAQUETE DE FIBRA ANULAR QUE TIENE UNA ZONA DE SALIDA INICIAL QUE SE EXTIENDE DESDE LA SUPERFICIE ANULAR INTERIOR. UNA GUIA DE REFUERZO CUBRE LA REGION DE SALIDA INICIAL DE LA FIBRA OPTICA PARA FORMAR UNA ESTRUCTURA COMPUESTA GUIA. LA ESTRUCTURA COMPUESTA GUIA ESTA ENROLLADA DENTRO DE UNA BOBINA ESPIRAL PLANA QUE YACE PERPENDICULAR AL EJE DE SIMETRIA DEL PAQUETE DE FIBRA ANULAR, CON LA VUELTA EXTERIOR DE LA ESPIRAL GUIANDO LEJOS DEL PAQUETE DE FIBRA OPTICA. LA BOBINA ESTA ENCAJADA EN UNA MASA DE COMPONENTE DE RELLENO. AL INICIO DE LA SALIDA DE LA FIBRA OPTICA, LAS VUELTAS DE LA BOBINA PROGRESIVAMENTE SE DISTIENDEN LIBRE DE LA MASA DEL COMPONENTE DE RELLENO PARA REALIZAR UNA CARGA GRADUAL DE LA FIBRA OPTICA Y ABRIR UN CAMINO PARA LA SALIDA AXIAL DE LA PARTE DE LA FIBRA OPTICA NO PROTEGIDA POR LA GUIA DE REFUERZO.
ES94308573T 1993-11-22 1994-11-21 Misil con bote de fibra optica con desarrollo interior. Expired - Lifetime ES2105533T3 (es)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US08/155,270 US5385319A (en) 1993-11-22 1993-11-22 Missile with inside payout optical fiber canister

Publications (1)

Publication Number Publication Date
ES2105533T3 true ES2105533T3 (es) 1997-10-16

Family

ID=22554742

Family Applications (1)

Application Number Title Priority Date Filing Date
ES94308573T Expired - Lifetime ES2105533T3 (es) 1993-11-22 1994-11-21 Misil con bote de fibra optica con desarrollo interior.

Country Status (7)

Country Link
US (1) US5385319A (es)
EP (1) EP0660071B1 (es)
KR (1) KR100211486B1 (es)
CA (1) CA2117820C (es)
DE (1) DE69404819T2 (es)
ES (1) ES2105533T3 (es)
IL (1) IL111542A (es)

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5637825A (en) * 1996-01-17 1997-06-10 The United States Of America As Represented By The Secretary Of The Navy Control line spool
FR2825184B1 (fr) * 2001-05-22 2003-07-18 Sediver Isolateur electrique composite ayant un revetement exterieur et au moins une fibre optique compatibles entre eux
DE102005002724B3 (de) * 2005-01-20 2006-01-19 Lfk-Lenkflugkörpersysteme Gmbh In einem Flugkörper angeordnete Spule für einen Lichtwellenleiter, Verfahren zur Verklebung der Lagen eines Lichtwellenleiters und Verwendung eines auf einem Spulenkern angeordneten Lichtwellenleiters zur bidirektionalen Datenübertragung
DE202006020409U1 (de) 2006-08-10 2008-07-17 Lfk-Lenkflugkörpersysteme Gmbh Vorrichtung für einen Lichtwellenleiter beim Start eines Flugkörpers
FR3131816B1 (fr) 2022-01-12 2024-04-26 Sedi Ati Fibres Optiques Liaison fibre optique embarquée déployable pour drones aérien
CN120274589B (zh) * 2025-04-18 2025-09-23 江西光博光电技术有限公司 一种集成光纤惯性组合导航的无人机光纤制导系统

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
NL279858A (es) * 1961-06-19
GB1058566A (en) * 1964-11-17 1967-02-15 British Aircraft Corp Ltd Improvements relating to guided missiles
DE2144140A1 (de) * 1971-09-03 1973-03-15 Messerschmitt Boelkow Blohm Einrichtung zur startstabilisierung eines selbstgetriebenen flugkoerpers
DE2753494C3 (de) * 1977-12-01 1981-07-09 Messerschmitt-Bölkow-Blohm GmbH, 8000 München Einrichtung zur Stabilisierung eines Flugkörpers bei seinem Start
US5022607A (en) * 1988-11-18 1991-06-11 Hughes Aircraft Company Bend limiting stiff leader and retainer system
US5167382A (en) * 1989-11-01 1992-12-01 Hughes Aircraft Company Inside payout optical fiber canister having reduced adhesive in the optical fiber pack
US5189253A (en) * 1990-07-20 1993-02-23 Hughes Aircraft Company Filament dispenser
US5100078A (en) * 1991-05-09 1992-03-31 Optelecom, Inc. Method and apparatus for controlling optical fiber payout from the inside of a wound package of optical fiber
US5181270A (en) * 1991-08-09 1993-01-19 Hughes Aircraft Company Optical fiber canister

Also Published As

Publication number Publication date
DE69404819T2 (de) 1998-01-29
CA2117820A1 (en) 1995-05-23
DE69404819D1 (de) 1997-09-11
KR950014840A (ko) 1995-06-16
IL111542A (en) 1996-10-31
CA2117820C (en) 1996-12-10
EP0660071B1 (en) 1997-08-06
IL111542A0 (en) 1995-01-24
EP0660071A1 (en) 1995-06-28
KR100211486B1 (ko) 1999-08-02
US5385319A (en) 1995-01-31

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