ES8102347A1 - Perfeccionamientos en misiles - Google Patents

Perfeccionamientos en misiles

Info

Publication number
ES8102347A1
ES8102347A1 ES492935A ES492935A ES8102347A1 ES 8102347 A1 ES8102347 A1 ES 8102347A1 ES 492935 A ES492935 A ES 492935A ES 492935 A ES492935 A ES 492935A ES 8102347 A1 ES8102347 A1 ES 8102347A1
Authority
ES
Spain
Prior art keywords
wing
missile
retractable
self
erecting
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
ES492935A
Other languages
English (en)
Other versions
ES492935A0 (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.)
General Dynamics Corp
Original Assignee
General Dynamics Corp
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 General Dynamics Corp filed Critical General Dynamics Corp
Publication of ES492935A0 publication Critical patent/ES492935A0/es
Publication of ES8102347A1 publication Critical patent/ES8102347A1/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
    • F42B10/146—Fabric fins, i.e. fins comprising at least one spar and a fin cover made of flexible sheet material

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)
  • Toys (AREA)
  • Tents Or Canopies (AREA)
  • Saccharide Compounds (AREA)
  • Seal Device For Vehicle (AREA)
  • Orthopedics, Nursing, And Contraception (AREA)
  • Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)

Abstract

DISPOSITIVOS DE DESPLIEGUE AUTOMATICO EN FORMA DE ALAS DE MISILES, PARA MEJORA DE LA ESTABILIDAD EN LA DIRECCION. LAS ALAS PLEGADAS ALOJADAS EN RANURAS LONGITUDINALES DEL CUERPO, CONSTAN DE UN PUNTAL MARGINAL DELANTERO (20) Y UNO TRASERO (22), QUE SOSTIENEN EL ALA HUECA (14) DE DOBLE PARED DE TELA FLEXIBLE E IMPERMEABLE AL AIRE. EL PUNTAL (20) DE FORMA DE BARRA Y EL PUNTAL (22) CON SECCION ACANALADA, EN POSICION DE PLEGADO QUEDAN UNO DENTRO DE OTRO Y AMBOS PIVOTAN SOBRE LAS ARTICULACIONES (24, 26); EL CONJUNTO ESTA DOTADO DE MEDIOS DE RETENCION Y EXTENSION PARA MANTENER EL ALA REPLEGADA O EXTENDERLA, QUE CONSISTEN EN OREJETAS Y BRAZOS DE RETEN Y MUELLES DE TORSION.
ES492935A 1979-09-24 1980-06-30 Perfeccionamientos en misiles Expired ES8102347A1 (es)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US06/077,966 US4351499A (en) 1979-09-24 1979-09-24 Double fabric, retractable, self-erecting wing for missle

Publications (2)

Publication Number Publication Date
ES492935A0 ES492935A0 (es) 1980-12-16
ES8102347A1 true ES8102347A1 (es) 1980-12-16

Family

ID=22141065

Family Applications (1)

Application Number Title Priority Date Filing Date
ES492935A Expired ES8102347A1 (es) 1979-09-24 1980-06-30 Perfeccionamientos en misiles

Country Status (17)

Country Link
US (1) US4351499A (es)
JP (1) JPS5646999A (es)
KR (1) KR840001056B1 (es)
AU (1) AU514367B2 (es)
BE (1) BE884267A (es)
CA (1) CA1146409A (es)
CH (1) CH636956A5 (es)
DE (1) DE3026409C2 (es)
DK (1) DK150259C (es)
ES (1) ES8102347A1 (es)
FR (1) FR2465644A1 (es)
GB (1) GB2059023B (es)
IL (1) IL60316A (es)
IT (1) IT1218440B (es)
NL (1) NL184382C (es)
NO (1) NO146828C (es)
SE (1) SE447420B (es)

Families Citing this family (33)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4568044A (en) * 1982-02-10 1986-02-04 General Dynamics, Pomona Division Wing housing and cover release assembly for self-erecting wing
US4586680A (en) * 1982-02-10 1986-05-06 General Dynamics Pomona Division Spring-erected telescopic wing support structure
IL66624A (en) * 1982-02-10 1986-04-29 Gen Dynamics Corp Wing housing and cover release assembly for self-erecting wing of a structure such as missile
US4586681A (en) * 1983-06-27 1986-05-06 General Dynamics Pomona Division Supersonic erectable fabric wings
DE3403573A1 (de) * 1983-11-09 1985-08-08 Diehl GmbH & Co, 8500 Nürnberg Geschoss mit herausklappbaren fluegeln
DE3340501C2 (de) * 1983-11-09 1986-12-04 Diehl GmbH & Co, 8500 Nürnberg Geschoß mit herausklappbaren Flügeln
JPS60166489A (ja) * 1984-02-10 1985-08-29 凸版印刷株式会社 針金綴装置
GB2162623B (en) * 1984-06-15 1988-08-10 Diehl Gmbh & Co A mechanism for aerodynamic deceleration and a body including such a mechanism
DE3422231A1 (de) * 1984-06-15 1985-12-19 Diehl GmbH & Co, 8500 Nürnberg Einrichtung zum aerodynamischen abbremsen der rotationsbewegung eines koerpers
DE8428118U1 (de) * 1984-09-25 1986-07-03 Rheinmetall GmbH, 4000 Düsseldorf Leitwerk mit entfaltbaren Flügeln
DE3510913A1 (de) * 1985-03-26 1986-10-09 Diehl GmbH & Co, 8500 Nürnberg Projektil
DE3523769A1 (de) * 1985-07-03 1987-01-08 Diehl Gmbh & Co Submunitions-flugkoerper mit ausstellbaren gleitfluegeln
SE460738B (sv) * 1988-03-16 1989-11-13 Bofors Ab Foer missiler och andra projektiler avsedd utfaellbar vinge
US4858851A (en) * 1988-06-07 1989-08-22 General Dynamics Pomona Division Folding wing structure for missile
GB8815060D0 (en) * 1988-06-24 1988-11-16 British Aerospace Fin assembly for projectile
DE3838738A1 (de) * 1988-11-15 1990-05-23 Diehl Gmbh & Co Projektil mit ausklappbaren fluegeln
DE3916690C1 (de) * 1989-05-23 1998-10-01 Bodenseewerk Geraetetech Ausklappbare Flügelanordnung für Flugkörper
DE3918244A1 (de) * 1989-06-05 1990-12-06 Diehl Gmbh & Co Von einem flugkoerper wegklappbarer fluegel
JP2639515B2 (ja) * 1990-05-09 1997-08-13 防衛庁技術研究本部長 多段式飛しょう体
US5671899A (en) * 1996-02-26 1997-09-30 Lockheed Martin Corporation Airborne vehicle with wing extension and roll control
FR2864612B1 (fr) * 2003-12-24 2007-11-23 Giat Ind Sa Dispositif de deploiement des ailettes d'un projectile
US7732741B1 (en) 2006-08-31 2010-06-08 The United States Of America As Represented By The Secretary Of The Navy Folding articulating wing mechanism
US7829830B1 (en) * 2007-10-19 2010-11-09 Woodward Hrt, Inc. Techniques for controlling access through a slot on a projectile
WO2012003025A2 (en) * 2010-04-07 2012-01-05 Bae Systems Information And Electronic Systems Integration Inc. Wing slot seal
KR101022357B1 (ko) * 2010-06-07 2011-03-22 엘아이지넥스원 주식회사 날개 전개시간 측정 장치
US10151568B2 (en) * 2016-03-15 2018-12-11 The Boeing Company Guided projectile and method of enabling guidance thereof
US11383895B2 (en) * 2017-02-09 2022-07-12 The Decor Corporation Pty. Ltd. Storage container with clip
US11340052B2 (en) 2019-08-27 2022-05-24 Bae Systems Information And Electronic Systems Integration Inc. Wing deployment initiator and locking mechanism
US11852211B2 (en) 2020-09-10 2023-12-26 Bae Systems Information And Electronic Systems Integration Inc. Additively manufactured elliptical bifurcating torsion spring
CN112693628B (zh) * 2020-12-28 2022-04-12 中国航天空气动力技术研究院 一种火星着陆巡视器的气动布局结构
CN114348237A (zh) * 2021-12-31 2022-04-15 洛阳瑞极光电科技有限公司 一种小型航空器折叠翼面弹出口的封闭和锁定机构
CN114852372B (zh) * 2022-07-06 2022-09-09 沈阳建筑大学 一种具有折叠机翼功能的空天变体飞行器及其发射系统
DE102022003754B4 (de) * 2022-10-11 2024-05-16 Diehl Defence Gmbh & Co. Kg Flugkörper

Family Cites Families (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1243542A (en) * 1917-02-15 1917-10-16 William Robbert Moore Projectile.
US1339188A (en) * 1918-11-20 1920-05-04 Zigmond Frecska Aerial torpedo
US1330079A (en) * 1919-08-21 1920-02-10 Kobuchi Luis Projectile
GB745252A (en) * 1953-07-29 1956-02-22 Ml Aviation Co Ltd Improvements relating to rocket propelled projectiles
US2959143A (en) * 1954-02-02 1960-11-08 Endrezze William Eugene Radial expanding taper formed movable fins for missles or torpedos
US2923241A (en) * 1957-09-09 1960-02-02 Aerojet General Co Folding stabilizing fins
DE1203647B (de) * 1962-09-11 1965-10-21 Dynamit Nobel Ag Flossenleitwerk, insbesondere fuer Raketengeschosse
US3185412A (en) * 1963-04-29 1965-05-25 Francis M Rogallo Flexible wing vehicle configurations
DE1244586B (de) * 1963-07-05 1967-07-13 Dornier System Gmbh Fluggeraet mit flexiblen Fluegelflaechen
US3888175A (en) * 1966-10-18 1975-06-10 Us Army Mechanical stabilizer
FR1506571A (fr) * 1966-11-10 1967-12-22 Matra Engins Bombe d'avion
US3633846A (en) * 1970-05-28 1972-01-11 Us Navy Expandable aerodynamic fin
US3788578A (en) * 1971-05-19 1974-01-29 T Sweeney Semi-rigid airfoil for airborne vehicles
US3990656A (en) * 1974-09-30 1976-11-09 The United States Of America As Represented By The Secretary Of The Army Pop-up fin

Also Published As

Publication number Publication date
FR2465644B1 (es) 1985-01-04
GB2059023A (en) 1981-04-15
US4351499A (en) 1982-09-28
BE884267A (fr) 1981-01-12
NO802088L (no) 1981-03-25
NL184382C (nl) 1989-07-03
NO146828C (no) 1982-12-15
FR2465644A1 (fr) 1981-03-27
NO146828B (no) 1982-09-06
DK150259B (da) 1987-01-19
JPS5646999A (en) 1981-04-28
KR830003723A (ko) 1983-06-22
NL8003592A (nl) 1981-03-26
DE3026409A1 (de) 1982-03-04
ES492935A0 (es) 1980-12-16
SE8004650L (sv) 1981-03-25
IT1218440B (it) 1990-04-19
SE447420B (sv) 1986-11-10
DK150259C (da) 1988-01-25
IT8049210A0 (it) 1980-07-10
DE3026409C2 (de) 1984-02-23
JPS6136160B2 (es) 1986-08-16
NL184382B (nl) 1989-02-01
KR840001056B1 (ko) 1984-07-27
CA1146409A (en) 1983-05-17
AU514367B2 (en) 1981-02-05
DK299680A (da) 1981-03-25
IL60316A (en) 1982-11-30
GB2059023B (en) 1983-02-09
CH636956A5 (fr) 1983-06-30

Similar Documents

Publication Publication Date Title
ES8102347A1 (es) Perfeccionamientos en misiles
GB376216A (en) Improvements in bladed projectiles
FR2442767B1 (es)
US4411398A (en) Double fabric retractable wing construction
GB745252A (en) Improvements relating to rocket propelled projectiles
GB1153747A (en) Toy Airplane with Folding Wings
SE8600812D0 (sv) Flugkorper mit uberkalibrigem leitwerk
GB869410A (en) Improvements relating to projectiles and rockets
GB1522018A (en) Assembly of a rocket-propelled missile and a retardation device
US4568044A (en) Wing housing and cover release assembly for self-erecting wing
US3942441A (en) Model rocket-glider
GB846069A (en) Improvements in and relating to a fin arrangement for projectiles
GB993839A (en) Toy projectile which converts to space platform during flight
US5299966A (en) Projectile toy apparatus
US3430562A (en) Aircraft bomb
US2942545A (en) Stabilizing system for mine dropped from aircraft
GB995061A (en) Helicopter which can be packed for transport
US2485870A (en) Rocket target
CN209719894U (zh) 一种巡飞弹可折叠垂尾结构
GB2115117A (en) Wing housing and cover release assembly for self-erecting wing
CN211373368U (zh) 一种灵巧型干扰弹投放靶机
US5042744A (en) Guideable stores
JPS6299202A (ja) 二重墜落防止付、バチカル式、水陸両用機
GB457570A (en) Improvements in machine gun mountings for aeroplanes
Klug Transport aircraft with relaxed/negative longitudinal stability: Results of a design study

Legal Events

Date Code Title Description
FD1A Patent lapsed

Effective date: 19971001