ES8308060A1 - Perfeccionamientos en una estructura de alas abatibles para misiles. - Google Patents

Perfeccionamientos en una estructura de alas abatibles para misiles.

Info

Publication number
ES8308060A1
ES8308060A1 ES515721A ES515721A ES8308060A1 ES 8308060 A1 ES8308060 A1 ES 8308060A1 ES 515721 A ES515721 A ES 515721A ES 515721 A ES515721 A ES 515721A ES 8308060 A1 ES8308060 A1 ES 8308060A1
Authority
ES
Spain
Prior art keywords
wing
housing
self
airframe
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
ES515721A
Other languages
English (en)
Other versions
ES515721A0 (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 ES515721A0 publication Critical patent/ES515721A0/es
Publication of ES8308060A1 publication Critical patent/ES8308060A1/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
    • F42B15/00—Self-propelled projectiles or missiles, e.g. rockets; Guided missiles
    • 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
    • E—FIXED CONSTRUCTIONS
    • E05—LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
    • E05C—BOLTS OR FASTENING DEVICES FOR WINGS, SPECIALLY FOR DOORS OR WINDOWS
    • E05C9/00—Arrangements of simultaneously actuated bolts or other securing devices at well-separated positions on the same wing
    • E05C9/02—Arrangements of simultaneously actuated bolts or other securing devices at well-separated positions on the same wing with one sliding bar for fastening when moved in one direction and unfastening when moved in opposite direction; with two sliding bars moved in the same direction when fastening or unfastening

Abstract

ESTRUCTURA DE ALAS ABATIBLES PARA MISILES. COMPRENDE: MEDIOS QUE DEFINEN UN COMPARTIMENTO (20) PARA CONTENER UN ALA DE DESPLIEGUE AUTOMATICO EN ESTADO ABATIDO Y UNA ESTRUCTURA DE ABERTURA (22) A TRAVES DE LA CUAL SE EXTIENDE EL ALA AL DESPLEGARSE; UNA CUBIERTA (26) MONTADA DE UNA FORMA SOLTABLE SOBRE LA ABERTURA; Y MEDIOS DE RETENCION SOLTABLES PARA RETENER LA CUBIERTA EN POSICION SOBRE LA ABERTURA. EL COMPARTIMENTO ES ALARGADO Y SE EXTIENDE A LO LARGO DEL EJE DEL FUSELAJE, Y LOS MEDIOS DE RETENCION COMPRENDEN MEDIOS DE RETENCION FIJOS Y MOVILES, EXTENDIDOS RESPECTIVAMENTE A CADA UNO DE LOS LADOS DEL COMPARTIMENTO (20).
ES515721A 1982-02-10 1982-09-15 Perfeccionamientos en una estructura de alas abatibles para misiles. Expired ES8308060A1 (es)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US34766082A 1982-02-10 1982-02-10

Publications (2)

Publication Number Publication Date
ES515721A0 ES515721A0 (es) 1983-08-16
ES8308060A1 true ES8308060A1 (es) 1983-08-16

Family

ID=23364680

Family Applications (1)

Application Number Title Priority Date Filing Date
ES515721A Expired ES8308060A1 (es) 1982-02-10 1982-09-15 Perfeccionamientos en una estructura de alas abatibles para misiles.

Country Status (17)

Country Link
JP (1) JPS58138998A (es)
KR (1) KR860000220B1 (es)
AU (1) AU530408B2 (es)
BE (1) BE894382A (es)
CA (1) CA1190434A (es)
CH (1) CH661347A5 (es)
DE (1) DE3234269C2 (es)
DK (1) DK153183C (es)
ES (1) ES8308060A1 (es)
FR (1) FR2521281B1 (es)
GB (1) GB2115117B (es)
HK (1) HK36588A (es)
IL (1) IL66624A (es)
IT (1) IT1149076B (es)
NL (1) NL184340C (es)
NO (1) NO150820C (es)
SE (1) SE452364B (es)

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3403573A1 (de) * 1983-11-09 1985-08-08 Diehl GmbH & Co, 8500 Nürnberg Geschoss mit herausklappbaren fluegeln
GB8815060D0 (en) * 1988-06-24 1988-11-16 British Aerospace Fin assembly for projectile
DE3918244A1 (de) * 1989-06-05 1990-12-06 Diehl Gmbh & Co Von einem flugkoerper wegklappbarer fluegel
DE4105142A1 (de) * 1991-02-20 1992-08-27 Diehl Gmbh & Co Projektil mit ausklappbarem leitwerk
FR2721702B1 (fr) * 1994-06-28 1996-08-14 Luchaire Defense Sa Dispositif de déploiement d'une ailette de projectile.
DE102004007311A1 (de) 2004-02-14 2005-09-01 Diehl Bgt Defence Gmbh & Co. Kg Geschoss mit vom Geschoss-Rumpf wegklappbaren Flügeln

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1715558A (en) * 1929-06-04 X t trunk lock
FR1490554A (fr) * 1966-05-03 1967-08-04 Ruggieri Ets Perfectionnement aux empennages déployants de roquettes
US3853288A (en) * 1967-07-17 1974-12-10 H Bode Encasement for the tail section of a rocket with a central nozzle and extendible control vanes
BE756110A (fr) * 1970-09-14 1971-02-15 Gohlke Werner Dispositif pour l'influence thermique des fonctions d'engins volants.
DE2623562A1 (de) * 1976-05-26 1977-12-08 Basf Ag Verfahren zur herstellung von glykolestern und deren folgeprodukten
US4351499A (en) * 1979-09-24 1982-09-28 General Dynamics Double fabric, retractable, self-erecting wing for missle

Also Published As

Publication number Publication date
BE894382A (fr) 1983-03-14
IT1149076B (it) 1986-12-03
SE452364B (sv) 1987-11-23
ES515721A0 (es) 1983-08-16
FR2521281A1 (fr) 1983-08-12
IT8249119A0 (it) 1982-09-15
DK410182A (da) 1983-08-11
NO150820B (no) 1984-09-10
NO150820C (no) 1985-01-09
JPS6364720B2 (es) 1988-12-13
FR2521281B1 (fr) 1986-06-06
NL184340C (nl) 1989-06-16
CH661347A5 (de) 1987-07-15
DK153183C (da) 1988-11-14
DK153183B (da) 1988-06-20
GB2115117A (en) 1983-09-01
IL66624A (en) 1986-04-29
AU530408B2 (en) 1983-07-14
SE8205200D0 (sv) 1982-09-13
JPS58138998A (ja) 1983-08-18
NL184340B (nl) 1989-01-16
DE3234269C2 (de) 1985-05-09
CA1190434A (en) 1985-07-16
NL8203531A (nl) 1983-09-01
NO823115L (no) 1983-08-11
KR840001706A (ko) 1984-05-16
SE8205200L (sv) 1983-08-11
DE3234269A1 (de) 1983-08-25
HK36588A (en) 1988-05-27
GB2115117B (en) 1985-11-06
KR860000220B1 (ko) 1986-03-15

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Legal Events

Date Code Title Description
FD1A Patent lapsed

Effective date: 20000201