CH636956A5 - Fusee comportant des ailes auto-deployables et retractables. - Google Patents

Fusee comportant des ailes auto-deployables et retractables. Download PDF

Info

Publication number
CH636956A5
CH636956A5 CH522880A CH522880A CH636956A5 CH 636956 A5 CH636956 A5 CH 636956A5 CH 522880 A CH522880 A CH 522880A CH 522880 A CH522880 A CH 522880A CH 636956 A5 CH636956 A5 CH 636956A5
Authority
CH
Switzerland
Prior art keywords
wing
levers
lever
locking
rocket
Prior art date
Application number
CH522880A
Other languages
English (en)
French (fr)
Inventor
Inge Maudal
Larry D Wedertz
Kenneth M Yost
Original Assignee
Gen 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 Gen Dynamics Corp filed Critical Gen Dynamics Corp
Publication of CH636956A5 publication Critical patent/CH636956A5/fr

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42BEXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B10/00Means 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
    • F42B10/02Stabilising arrangements
    • F42B10/14Stabilising arrangements using fins spread or deployed after launch, e.g. after leaving the barrel
    • F42B10/146Fabric 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)
CH522880A 1979-09-24 1980-07-08 Fusee comportant des ailes auto-deployables et retractables. CH636956A5 (fr)

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 (1)

Publication Number Publication Date
CH636956A5 true CH636956A5 (fr) 1983-06-30

Family

ID=22141065

Family Applications (1)

Application Number Title Priority Date Filing Date
CH522880A CH636956A5 (fr) 1979-09-24 1980-07-08 Fusee comportant des ailes auto-deployables et retractables.

Country Status (17)

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

Families Citing this family (33)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
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
US4568044A (en) * 1982-02-10 1986-02-04 General Dynamics, Pomona Division Wing housing and cover release assembly for self-erecting wing
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
DE3422231A1 (de) * 1984-06-15 1985-12-19 Diehl GmbH & Co, 8500 Nürnberg Einrichtung zum aerodynamischen abbremsen der rotationsbewegung eines koerpers
GB2162623B (en) * 1984-06-15 1988-08-10 Diehl Gmbh & Co A mechanism for aerodynamic deceleration and a body including such a mechanism
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
AU2018218189B2 (en) * 2017-02-09 2022-12-08 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
US4351499A (en) 1982-09-28
IT8049210A0 (it) 1980-07-10
NL8003592A (nl) 1981-03-26
IL60316A (en) 1982-11-30
GB2059023B (en) 1983-02-09
FR2465644A1 (fr) 1981-03-27
DK150259B (da) 1987-01-19
NO146828B (no) 1982-09-06
CA1146409A (en) 1983-05-17
KR830003723A (ko) 1983-06-22
AU514367B2 (en) 1981-02-05
FR2465644B1 (enExample) 1985-01-04
ES492935A0 (es) 1980-12-16
NO146828C (no) 1982-12-15
DK299680A (da) 1981-03-25
SE447420B (sv) 1986-11-10
NL184382B (nl) 1989-02-01
IT1218440B (it) 1990-04-19
ES8102347A1 (es) 1980-12-16
GB2059023A (en) 1981-04-15
SE8004650L (sv) 1981-03-25
KR840001056B1 (ko) 1984-07-27
JPS5646999A (en) 1981-04-28
BE884267A (fr) 1981-01-12
DE3026409C2 (de) 1984-02-23
NO802088L (no) 1981-03-25
DK150259C (da) 1988-01-25
DE3026409A1 (de) 1982-03-04
JPS6136160B2 (enExample) 1986-08-16
NL184382C (nl) 1989-07-03

Similar Documents

Publication Publication Date Title
CH636956A5 (fr) Fusee comportant des ailes auto-deployables et retractables.
EP1550837B1 (fr) Dispositif de déploiement et d'entrainement de gouvernes d'un projectile
FR2742220A1 (fr) Appareil pour deplier et fixer les ailettes d'un engin
EP3640414B1 (fr) Tente pliable comprenant deux structures parapluies
FR2901245A1 (fr) Dispositif d'articulation d'une porte d'une nacelle d'aeronef et nacelle equipee dudit dispositif d'articulation
US4411398A (en) Double fabric retractable wing construction
FR2741910A1 (fr) Inverseur de poussee de turboreacteur a portes a panneau arriere articule
FR2521280A1 (fr) Structure de support d'aile escamotable, notamment pour missiles
EP3983289A1 (fr) Porte d'aeronef a dispositif de maintien des bras de manipulation
FR3135757A1 (fr) Inverseur de poussee comprenant une membrane d’obturation a deploiement simplifie
FR2886620A1 (fr) Systeme d'ouverture et de fermeture de trappe pour case de train d'atterrissage d'un aeronef
FR2780819A1 (fr) Reflecteur d'antenne elastiquement deformable pour engin spatial
FR2521281A1 (fr) Logement d'aile et dispositif de deblocage de couvercle pour aile a erection automatique pour engins speciaux
FR3075173B1 (fr) Siege de pilote muni d'une echelle d'evacuation et aeronef muni d'un tel siege
EP0485327A1 (fr) Siège de sécurité pour sports aéronautiques
FR2780820A1 (fr) Reflecteur d'antenne elastiquement deformable pour engin spatial et engin spatial comportant un tel reflecteur
FR2749381A1 (fr) Projectile explosif
FR2601325A1 (fr) Structure tridimensionnelle pliable et aile pliable comportant une telle structure
EP0085075A1 (fr) Roue hydraulique a pales articulees
EP4033198B1 (fr) Dispositif de liaison entre un moyen d'allumage d'une charge propulsive et un étui combustible d'une munition, étui combustible et rondelle élastique associés à un tel dispositif de liaison
FR2613474A1 (fr) Element de voilure gonflable, notamment pour un engin volant
EP1468912B1 (fr) Structure à géométrie variable pour un appareil monté à bord d'un engin spatial
FR2928724A1 (fr) Perfectionnements aux engins munis de plans de commande de la trajectoire en vol
EP3692324B1 (fr) Dispositif de blocage d'ailette et projectile comportant un tel dispositif
WO2014009616A1 (fr) Dispositif d'ouverture et de fermeture d'une trappe de case de train d'aéronef

Legal Events

Date Code Title Description
PUE Assignment

Owner name: HUGHES MISSILE SYSTEMS COMPANY

PL Patent ceased