ES8701975A1 - Perfeccionamientos en los sistemas de seguridad para impedirel armado de una carga aerotransportada - Google Patents

Perfeccionamientos en los sistemas de seguridad para impedirel armado de una carga aerotransportada

Info

Publication number
ES8701975A1
ES8701975A1 ES541842A ES541842A ES8701975A1 ES 8701975 A1 ES8701975 A1 ES 8701975A1 ES 541842 A ES541842 A ES 541842A ES 541842 A ES541842 A ES 541842A ES 8701975 A1 ES8701975 A1 ES 8701975A1
Authority
ES
Spain
Prior art keywords
charge
safety device
clamping assembly
traction
arming
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
Application number
ES541842A
Other languages
English (en)
Other versions
ES541842A0 (es
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.)
Rafaut and Cie
Original Assignee
Rafaut and Cie
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 Rafaut and Cie filed Critical Rafaut and Cie
Publication of ES8701975A1 publication Critical patent/ES8701975A1/es
Publication of ES541842A0 publication Critical patent/ES541842A0/es
Expired legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42—AMMUNITION; BLASTING
    • F42C—AMMUNITION FUZES; ARMING OR SAFETY MEANS THEREFOR
    • F42C14/00—Mechanical fuzes characterised by the ammunition class or type
    • F42C14/06—Mechanical fuzes characterised by the ammunition class or type for fall bombs
    • 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
    • B64D1/00—Dropping, ejecting, releasing, or receiving articles, liquids, or the like, in flight
    • B64D1/02—Dropping, ejecting, or releasing articles
    • B64D1/04—Dropping, ejecting, or releasing articles the articles being explosive, e.g. bombs
    • B64D1/06—Bomb releasing; Bombs doors
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16G—BELTS, CABLES, OR ROPES, PREDOMINANTLY USED FOR DRIVING PURPOSES; CHAINS; FITTINGS PREDOMINANTLY USED THEREFOR
    • F16G11/00—Means for fastening cables or ropes to one another or to other objects; Caps or sleeves for fixing on cables or ropes
    • F16G11/10—Quick-acting fastenings; Clamps holding in one direction only
    • F16G11/105—Clamps holding in one direction only

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Electric Cable Installation (AREA)
  • Burglar Alarm Systems (AREA)
  • Elimination Of Static Electricity (AREA)

Abstract

SISTEMA DE SEGURIDAD PARA IMPEDIR EL ARMADO DE UNA CARGA AEROTRANSPORTADA. EL SISTEMA TIENE UNA PINZA (2) QUE ES ATRAVESADA POR EL CABLE DE ARMADO (3) Y QUE ESTA PINZADA CUANDO ESTA CERRADA O LIBRE CUANDO ESTA ABIERTA. EL CIERRE SE PRODUCE POR EL DESPLAZAMIENTO DE DOS PIEZAS (5 Y 7) SEGUN LA DIRECCION DE TRACCION DEL CABLE DE TIRADO (4). UNA DE ESTAS PIEZAS (5) ES DE FIJACION Y ESTA FIJADA EN LA CARGA, MIENTRAS QUE LA OTRA (7) ES DE TRACCION Y VA DESLIZANTE EN LA CARGA Y FIJA EN EL CABLE DE TIRADO. EL CIERRE DE LA PINZA SE PRODUCE POR DESLIZAMIENTO DE LA SUPERFICIE INCLINADA DE LA PLACA DE TRACCION (7) POR LA SUPERFICIE (9) EN CONTACTO DE LA PINZA (2).
ES541842A 1984-04-04 1985-04-02 Perfeccionamientos en los sistemas de seguridad para impedirel armado de una carga aerotransportada Expired ES8701975A1 (es)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR8405298A FR2562654B1 (fr) 1984-04-04 1984-04-04 Dispositif de securite pour empecher l'armement d'une charge aeroportee

Publications (2)

Publication Number Publication Date
ES8701975A1 true ES8701975A1 (es) 1986-12-16
ES541842A0 ES541842A0 (es) 1986-12-16

Family

ID=9302829

Family Applications (1)

Application Number Title Priority Date Filing Date
ES541842A Expired ES8701975A1 (es) 1984-04-04 1985-04-02 Perfeccionamientos en los sistemas de seguridad para impedirel armado de una carga aerotransportada

Country Status (4)

Country Link
US (1) US4658698A (es)
EP (1) EP0157700A1 (es)
ES (1) ES8701975A1 (es)
FR (1) FR2562654B1 (es)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3833817A1 (de) * 1988-10-05 1990-04-19 Messerschmitt Boelkow Blohm Vorrichtung zum sichern und scharfmachen von submunitionskoerpern
US5305676A (en) * 1993-03-08 1994-04-26 Bw/Ip International, Inc. Low retention force release and arming mechanism for ordinance devices

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CH188941A (de) * 1936-11-28 1937-01-31 Weber Hans Klemme zum Festklemmen von Zugorganen.
US3378892A (en) * 1966-07-25 1968-04-23 Nasa Usa Quick-attach mechanism
US3595126A (en) * 1969-08-14 1971-07-27 Avco Corp Fuze initiator
FR2173669B1 (es) * 1972-01-28 1976-06-11 Rafaut & Cie
US4179150A (en) * 1977-10-31 1979-12-18 Imc Magnetics Corporation Safety arming device for missiles
US4322998A (en) * 1979-10-26 1982-04-06 The United States Of America As Represented By The Secretary Of The Navy Integral store suspension and communication device

Also Published As

Publication number Publication date
FR2562654B1 (fr) 1987-11-13
EP0157700A1 (fr) 1985-10-09
FR2562654A1 (fr) 1985-10-11
US4658698A (en) 1987-04-21
ES541842A0 (es) 1986-12-16

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Legal Events

Date Code Title Description
FD1A Patent lapsed

Effective date: 19960603