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)
Spanish (es)
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

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Fluid Mechanics (AREA)
  • Chemical & Material Sciences (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • Physics & Mathematics (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Toys (AREA)
  • Casings For Electric Apparatus (AREA)
  • Axle Suspensions And Sidecars For Cycles (AREA)
  • User Interface Of Digital Computer (AREA)
  • Closures For Containers (AREA)
  • Organic Low-Molecular-Weight Compounds And Preparation Thereof (AREA)
  • Clamps And Clips (AREA)
  • Executing Machine-Instructions (AREA)
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 (cg-RX-API-DMAC7.html)
KR (1) KR860000220B1 (cg-RX-API-DMAC7.html)
AU (1) AU530408B2 (cg-RX-API-DMAC7.html)
BE (1) BE894382A (cg-RX-API-DMAC7.html)
CA (1) CA1190434A (cg-RX-API-DMAC7.html)
CH (1) CH661347A5 (cg-RX-API-DMAC7.html)
DE (1) DE3234269C2 (cg-RX-API-DMAC7.html)
DK (1) DK153183C (cg-RX-API-DMAC7.html)
ES (1) ES8308060A1 (cg-RX-API-DMAC7.html)
FR (1) FR2521281B1 (cg-RX-API-DMAC7.html)
GB (1) GB2115117B (cg-RX-API-DMAC7.html)
HK (1) HK36588A (cg-RX-API-DMAC7.html)
IL (1) IL66624A (cg-RX-API-DMAC7.html)
IT (1) IT1149076B (cg-RX-API-DMAC7.html)
NL (1) NL184340C (cg-RX-API-DMAC7.html)
NO (1) NO150820C (cg-RX-API-DMAC7.html)
SE (1) SE452364B (cg-RX-API-DMAC7.html)

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
NO150820B (no) 1984-09-10
NO150820C (no) 1985-01-09
FR2521281A1 (fr) 1983-08-12
NL184340C (nl) 1989-06-16
JPS58138998A (ja) 1983-08-18
NO823115L (no) 1983-08-11
ES515721A0 (es) 1983-08-16
NL8203531A (nl) 1983-09-01
FR2521281B1 (fr) 1986-06-06
DK153183C (da) 1988-11-14
DK410182A (da) 1983-08-11
CA1190434A (en) 1985-07-16
DE3234269C2 (de) 1985-05-09
GB2115117B (en) 1985-11-06
DK153183B (da) 1988-06-20
SE8205200D0 (sv) 1982-09-13
BE894382A (fr) 1983-03-14
KR840001706A (ko) 1984-05-16
JPS6364720B2 (cg-RX-API-DMAC7.html) 1988-12-13
IT8249119A0 (it) 1982-09-15
AU530408B2 (en) 1983-07-14
IT1149076B (it) 1986-12-03
IL66624A (en) 1986-04-29
GB2115117A (en) 1983-09-01
NL184340B (nl) 1989-01-16
DE3234269A1 (de) 1983-08-25
SE452364B (sv) 1987-11-23
KR860000220B1 (ko) 1986-03-15
HK36588A (en) 1988-05-27
CH661347A5 (de) 1987-07-15
SE8205200L (sv) 1983-08-11

Similar Documents

Publication Publication Date Title
KR830003723A (ko) 미사일용의 접개들이식 자립날개(retractable self-erecting wing)구조
ES8308059A1 (es) Perfeccionamientos en una estructura de sustentacion de ala telescopica para misil desplegada por resorte.
SE8304731L (sv) Flygburet forvarningssystem
DE3870880D1 (de) Anbau.
ES8308060A1 (es) Perfeccionamientos en una estructura de alas abatibles para misiles.
IT1162364B (it) Dispositivo di separazione per losgancio di un dispositivo di frenatura aerodinamica da un carico per esempio lo sgancio di paracadute
US4568044A (en) Wing housing and cover release assembly for self-erecting wing
US4496122A (en) Extended moment arm anti-spin device
FR2455545A1 (fr) Perfectionnement aux dispositifs sureleves des avions et planeurs ou deltaplanes
CN221367561U (zh) 一种无人机起落架自动折叠装置
Crema et al. Some trends in airship technology developments
GB1155314A (en) Improvements in or relating to Fin Assemblies for Missiles, and Missiles Provided With Improved Fin Assemblies.
FR2316178A1 (fr) Dispositif de hissage des charges sur avion, incorpore au systeme d'emport et a liberation automatique
GB1322241A (en) Extensible boom assemblies for spacecraft
USD243667S (en) Airplane
AU4217089A (en) Craft with fixed wing hinged at the top of a mast
ES2177236T3 (es) Sistema de bloqueo del tren de aterrizaje de un avion.
IT1192641B (it) Timone per la generazione aerodinamica di momenti su aeroplani
JPS6058499U (ja) 展開装置
Guiraud et al. A note on an instability mechanism for the core of a rolled-up vortex sheet
IT7851578A0 (it) Paracadute particolarmente adattoper avio-lancio di carichi
Rogers The shock tube- Talisman, tool or technique
BUIAKAS Stabilization of the shape of a deploying surface(for large space radio telescope)
BOUTTES et al. Compared effects of the aerodynamic coefficients on the aeroelastic stability of an airplane automatically piloted(Effects of aerodynamic coefficients on aeroelastic stability of autopiloted aircraft)
GARDNER Asymptotic behavior of semilinear reaction-diffusion systems with Dirichlet boundary conditions[Technical Summary Report]

Legal Events

Date Code Title Description
FD1A Patent lapsed

Effective date: 20000201