ES8801027A1 - Perfeccionamientos en cuerpos volantes como cohetes o pro- yectiles - Google Patents

Perfeccionamientos en cuerpos volantes como cohetes o pro- yectiles

Info

Publication number
ES8801027A1
ES8801027A1 ES546443A ES546443A ES8801027A1 ES 8801027 A1 ES8801027 A1 ES 8801027A1 ES 546443 A ES546443 A ES 546443A ES 546443 A ES546443 A ES 546443A ES 8801027 A1 ES8801027 A1 ES 8801027A1
Authority
ES
Spain
Prior art keywords
missile body
guide
wings
missile
pressurized gas
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
ES546443A
Other languages
English (en)
Other versions
ES546443A0 (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.)
Rheinmetall Industrie AG
Original Assignee
Rheinmetall GmbH
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 Rheinmetall GmbH filed Critical Rheinmetall GmbH
Publication of ES546443A0 publication Critical patent/ES546443A0/es
Publication of ES8801027A1 publication Critical patent/ES8801027A1/es
Expired 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
    • F42B10/00—Means for influencing, e.g. improving, the aerodynamic properties of projectiles or missiles; Arrangements on projectiles or missiles for stabilising, steering, range-reducing, range-increasing or fall-retarding
    • F42B10/02—Stabilising arrangements
    • F42B10/14—Stabilising arrangements using fins spread or deployed after launch, e.g. after leaving the barrel
    • F42B10/20—Stabilising arrangements using fins spread or deployed after launch, e.g. after leaving the barrel deployed by combustion gas pressure, or by pneumatic or hydraulic forces

Landscapes

  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)

Abstract

PERFECCIONAMIENTOS EN CUERPOS VOLANTES, COMO COHETES O PROYECTILES. CONSTA DE UN MECANISMO GUIADOR DE POPA Y UN SEGUNDO MECANISMO GUIADOR DE POPA Y UN SEGUNDO MECANISMO GUIADOR (12) CON ALETAS, TALES QUE SE CONSTITUYEN DE UN MODO PLEGABLE HACIA FUERA, ABRIENDOSE LAS ALETAS (14) EN DIRECCION CONTRARIA AL VUELO. ESTAS CONSTAN DE UNAS HENDIDURAS (20) AXIALES EN LA PARED DEL CUERPO VOLANTE, Y ESTAN APOYADAS GIRATORIAMENTE ALREDEDOR DE EJES (21) PERPENDICULARES AL EJE LONGITUDINAL DEL CUERPO VOLANTE. PARA LA RETENCION DE LAS ALETAS EN POSICION DE REPOSO SE HA PREVISTO UNA CORREDERA APOYADA DESLIZABLEMENTE EN EL CANAL DE GAS EN LA DIRECCION DEL EJE LONGITUDINAL.
ES546443A 1984-09-05 1985-08-27 Perfeccionamientos en cuerpos volantes como cohetes o pro- yectiles Expired ES8801027A1 (es)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE19843432614 DE3432614A1 (de) 1984-09-05 1984-09-05 Flugkoerper

Publications (2)

Publication Number Publication Date
ES546443A0 ES546443A0 (es) 1987-12-16
ES8801027A1 true ES8801027A1 (es) 1987-12-16

Family

ID=6244693

Family Applications (1)

Application Number Title Priority Date Filing Date
ES546443A Expired ES8801027A1 (es) 1984-09-05 1985-08-27 Perfeccionamientos en cuerpos volantes como cohetes o pro- yectiles

Country Status (4)

Country Link
US (1) US4659037A (es)
EP (1) EP0180722B1 (es)
DE (2) DE3432614A1 (es)
ES (1) ES8801027A1 (es)

Families Citing this family (23)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3507677A1 (de) * 1985-03-05 1986-09-11 Diehl GmbH & Co, 8500 Nürnberg Flugkoerper mit ueberkalibrigem leitwerk
FR2812936A1 (fr) * 1986-08-12 2002-02-15 Aerospatiale Missile a voilure variable
DE3721512C1 (de) * 1987-06-30 1989-03-30 Diehl Gmbh & Co Flugkoerper mit ueberkalibrigem Leitwerk
DE3918244A1 (de) * 1989-06-05 1990-12-06 Diehl Gmbh & Co Von einem flugkoerper wegklappbarer fluegel
US5120947A (en) * 1990-03-29 1992-06-09 International Totalizator Systems, Inc. Apparatus and method for processing a ticket
DE4020897C2 (de) * 1990-06-30 1993-11-11 Diehl Gmbh & Co Einrichtung zum Entriegeln und Ausschwenken der Ruderblätter eines Projektiles
DE4105142A1 (de) * 1991-02-20 1992-08-27 Diehl Gmbh & Co Projektil mit ausklappbarem leitwerk
US5211358A (en) * 1991-05-13 1993-05-18 General Dynamics Corporation Airfoil deployment system for missile or aircraft
US6073880A (en) * 1998-05-18 2000-06-13 Versatron, Inc. Integrated missile fin deployment system
US6186443B1 (en) 1998-06-25 2001-02-13 International Dynamics Corporation Airborne vehicle having deployable wing and control surface
DE10162136B4 (de) 2001-12-18 2004-10-14 Diehl Munitionssysteme Gmbh & Co. Kg Aus einem Rohr zu verschießender Flugkörper mit überkalibrigem Leitwerk
DE10205043C5 (de) * 2002-02-07 2010-06-17 Diehl Bgt Defence Gmbh & Co. Kg Aus einem Rohr zu verschließender Flugkörper mit überkalibrigem Leitwerk
US7800031B2 (en) * 2005-09-07 2010-09-21 Omnitek Partners Llc Actuators for gun-fired projectiles and mortars
FR2909972B1 (fr) * 2006-12-18 2009-10-23 Novadem Sarl Aeronef a decollage vertical
FR2952712A1 (fr) * 2009-11-16 2011-05-20 Nexter Munitions Corps de projectile equipe d'appendices deployables
CN103522248B (zh) * 2013-10-11 2015-08-05 北京航天新风机械设备有限责任公司 一种用于舵/翼面折叠的专用工装
EP3318490B1 (de) * 2016-11-03 2019-06-12 Diehl Defence GmbH & Co. KG Verfahren zum abwerfen eines flugkörpers
IL250433B (en) * 2017-02-02 2021-01-31 Israel Aerospace Ind Ltd Apparatus for a vehicle
US11300390B1 (en) 2018-03-05 2022-04-12 Dynamic Structures And Materials, Llc Control surface deployment apparatus and method of use
CN112525016A (zh) * 2020-12-22 2021-03-19 湖北航天化学技术研究所 一种气体产生装置及驱动装置
US12068422B2 (en) 2021-10-08 2024-08-20 Simmonds Precision Products, Inc. Systems and methods for cooling electronics
US12007212B2 (en) 2021-10-08 2024-06-11 Simmonds Precision Products, Inc. Joule-Thompson cooler actuation systems
CN113899265A (zh) * 2021-10-12 2022-01-07 西安现代控制技术研究所 一种基于光电元件的折叠舵翼张开时间测量装置

Family Cites Families (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3047257A (en) * 1958-04-24 1962-07-31 Martin Marietta Corp Device for changing airfoil profile
US3633846A (en) * 1970-05-28 1972-01-11 Us Navy Expandable aerodynamic fin
DE2342783C2 (de) * 1973-08-24 1983-12-22 Rheinmetall GmbH, 4000 Düsseldorf Mit einem Leitwerk versehenes Geschoß
DE2518593C3 (de) * 1975-04-26 1979-12-06 Diehl Gmbh & Co, 8500 Nuernberg Mörsergeschoß
SE428969B (sv) * 1977-02-09 1983-08-01 Bofors Ab Anordning vid fenstabiliserad granat
US4143838A (en) * 1977-08-22 1979-03-13 The United States Of America As Represented By The Secretary Of The Navy Folding fin assembly detent
US4203569A (en) * 1977-10-17 1980-05-20 Bei Electronics, Inc. Fin and nozzle unit for a free-flight rocket
DE7804927U1 (de) * 1978-02-18 1978-06-01 Messerschmitt-Boelkow-Blohm Gmbh, 8000 Muenchen Vorrichtung zum ausklappen von schwenkfluegeln
US4364531A (en) * 1980-10-09 1982-12-21 Knoski Jerry L Attachable airfoil with movable control surface
US4478150A (en) * 1983-01-12 1984-10-23 The United States Of America As Represented By The Secretary Of The Army Cartridge with elastic pusher cup
US4586681A (en) * 1983-06-27 1986-05-06 General Dynamics Pomona Division Supersonic erectable fabric wings

Also Published As

Publication number Publication date
DE3586163D1 (de) 1992-07-09
EP0180722A3 (en) 1990-03-21
EP0180722B1 (de) 1992-06-03
ES546443A0 (es) 1987-12-16
US4659037A (en) 1987-04-21
EP0180722A2 (de) 1986-05-14
DE3432614A1 (de) 1986-03-13

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