IT8249119A0 - WING CASING STRUCTURE FOR SELF-ERECTING RETRACTABLE WINGS, PARTICULARLY OF MISSILE - Google Patents

WING CASING STRUCTURE FOR SELF-ERECTING RETRACTABLE WINGS, PARTICULARLY OF MISSILE

Info

Publication number: IT8249119A0
Authority: IT; Italy
Prior art keywords: missile; erecting; self; casing structure; retractable wings
Prior art date: 1982-02-10

Application number

IT8249119A

Other languages

Italian (it)

Other versions

IT1149076B (en

Inventor

Anthony Di Tommaso

Ronald T Inglis

Richard C Worley

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.)

1982-02-10

Filing date

1982-09-15

Publication date

1982-09-15

1982-09-15 Application filed by Gen Dynamics Corp filed Critical Gen Dynamics Corp

1982-09-15 Publication of IT8249119A0 publication Critical patent/IT8249119A0/en

1986-12-03 Application granted granted Critical

1986-12-03 Publication of IT1149076B publication Critical patent/IT1149076B/en

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)
Mechanical Engineering (AREA)
Chemical & Material Sciences (AREA)
Aviation & Aerospace Engineering (AREA)
Combustion & Propulsion (AREA)
Physics & Mathematics (AREA)
Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
Toys (AREA)
Casings For Electric Apparatus (AREA)
Closures For Containers (AREA)
Clamps And Clips (AREA)
Axle Suspensions And Sidecars For Cycles (AREA)
Organic Low-Molecular-Weight Compounds And Preparation Thereof (AREA)
Executing Machine-Instructions (AREA)

IT49119/82A 1982-02-10 1982-09-15 WING ENVELOPE STRUCTURE FOR SELF-ERECTION RE-ENTERABLE WINGS, IN PARTICULAR OF MISSILES IT1149076B (en)

Applications Claiming Priority (1)

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

Publications (2)

Publication Number	Publication Date
IT8249119A0 true IT8249119A0 (en)	1982-09-15
IT1149076B IT1149076B (en)	1986-12-03

Family

ID=23364680

Family Applications (1)

Application Number	Title	Priority Date	Filing Date
IT49119/82A IT1149076B (en)	1982-02-10	1982-09-15	WING ENVELOPE STRUCTURE FOR SELF-ERECTION RE-ENTERABLE WINGS, IN PARTICULAR OF MISSILES

Country Status (17)

Country	Link
JP (1)	JPS58138998A (en)
KR (1)	KR860000220B1 (en)
AU (1)	AU530408B2 (en)
BE (1)	BE894382A (en)
CA (1)	CA1190434A (en)
CH (1)	CH661347A5 (en)
DE (1)	DE3234269C2 (en)
DK (1)	DK153183C (en)
ES (1)	ES515721A0 (en)
FR (1)	FR2521281B1 (en)
GB (1)	GB2115117B (en)
HK (1)	HK36588A (en)
IL (1)	IL66624A (en)
IT (1)	IT1149076B (en)
NL (1)	NL184340C (en)
NO (1)	NO150820C (en)
SE (1)	SE452364B (en)

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number	Priority date	Publication date	Assignee	Title
DE3403573A1 (en) *	1983-11-09	1985-08-08	Diehl GmbH & Co, 8500 Nürnberg	BULLET WITH FOLD-OUT WINGS
GB8815060D0 (en) *	1988-06-24	1988-11-16	British Aerospace	Fin assembly for projectile
DE3918244A1 (en) *	1989-06-05	1990-12-06	Diehl Gmbh & Co	FOLDING WING FROM A MISSILE
DE4105142A1 (en) *	1991-02-20	1992-08-27	Diehl Gmbh & Co	PROJECTILE WITH FOLD-OUT PAD
FR2721702B1 (en) *	1994-06-28	1996-08-14	Luchaire Defense Sa	Device for deploying a projectile fin.
DE102004007311A1 (en)	2004-02-14	2005-09-01	Diehl Bgt Defence Gmbh & Co. Kg	Projectile with wings that can be folded away from the projectile fuselage

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 (en) *	1966-05-03	1967-08-04	Ruggieri Ets	Development of deploying rocket stabilizers
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 (en) *	1970-09-14	1971-02-15	Gohlke Werner	DEVICE FOR THE THERMAL INFLUENCE OF FLYING GEAR FUNCTIONS.
DE2623562A1 (en) *	1976-05-26	1977-12-08	Basf Ag	PROCESS FOR MANUFACTURING GLYCOLESTERS AND THEIR SUBSEQUENT PRODUCTS
US4351499A (en) *	1979-09-24	1982-09-28	General Dynamics	Double fabric, retractable, self-erecting wing for missle

1982
- 1982-08-23 IL IL66624A patent/IL66624A/en not_active IP Right Cessation
- 1982-09-07 GB GB08225459A patent/GB2115117B/en not_active Expired
- 1982-09-10 NL NLAANVRAGE8203531,A patent/NL184340C/en not_active IP Right Cessation
- 1982-09-13 BE BE0/209001A patent/BE894382A/en not_active IP Right Cessation
- 1982-09-13 SE SE8205200A patent/SE452364B/en not_active IP Right Cessation
- 1982-09-14 FR FR8215514A patent/FR2521281B1/en not_active Expired
- 1982-09-14 CH CH5449/82A patent/CH661347A5/en not_active IP Right Cessation
- 1982-09-14 NO NO823115A patent/NO150820C/en unknown
- 1982-09-14 JP JP57159040A patent/JPS58138998A/en active Granted
- 1982-09-14 DK DK410182A patent/DK153183C/en active
- 1982-09-15 ES ES515721A patent/ES515721A0/en active Granted
- 1982-09-15 CA CA000411465A patent/CA1190434A/en not_active Expired
- 1982-09-15 DE DE3234269A patent/DE3234269C2/en not_active Expired
- 1982-09-15 KR KR8204174A patent/KR860000220B1/en active
- 1982-09-15 AU AU88433/82A patent/AU530408B2/en not_active Ceased
- 1982-09-15 IT IT49119/82A patent/IT1149076B/en active
1988
- 1988-05-19 HK HK365/88A patent/HK36588A/en not_active IP Right Cessation

Also Published As

Publication number	Publication date
DE3234269C2 (en)	1985-05-09
SE8205200L (en)	1983-08-11
NL184340B (en)	1989-01-16
FR2521281A1 (en)	1983-08-12
DE3234269A1 (en)	1983-08-25
KR840001706A (en)	1984-05-16
IT1149076B (en)	1986-12-03
DK410182A (en)	1983-08-11
NO150820B (en)	1984-09-10
NO150820C (en)	1985-01-09
KR860000220B1 (en)	1986-03-15
ES8308060A1 (en)	1983-08-16
GB2115117B (en)	1985-11-06
IL66624A (en)	1986-04-29
DK153183C (en)	1988-11-14
ES515721A0 (en)	1983-08-16
NL8203531A (en)	1983-09-01
CA1190434A (en)	1985-07-16
BE894382A (en)	1983-03-14
SE452364B (en)	1987-11-23
JPS6364720B2 (en)	1988-12-13
NO823115L (en)	1983-08-11
JPS58138998A (en)	1983-08-18
DK153183B (en)	1988-06-20
AU530408B2 (en)	1983-07-14
SE8205200D0 (en)	1982-09-13
NL184340C (en)	1989-06-16
FR2521281B1 (en)	1986-06-06
CH661347A5 (en)	1987-07-15
HK36588A (en)	1988-05-27
GB2115117A (en)	1983-09-01

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