HK36588A - An airframe having a self-erecting wing structure - Google Patents

An airframe having a self-erecting wing structure

Info

Publication number
HK36588A
HK36588A HK365/88A HK36588A HK36588A HK 36588 A HK36588 A HK 36588A HK 365/88 A HK365/88 A HK 365/88A HK 36588 A HK36588 A HK 36588A HK 36588 A HK36588 A HK 36588A
Authority
HK
Hong Kong
Prior art keywords
airframe
self
wing structure
erecting
erecting wing
Prior art date
Application number
HK365/88A
Inventor
Anthony Ditommaso
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.)
Filing date
Publication date
Application filed by Gen Dynamics Corp filed Critical Gen Dynamics Corp
Publication of HK36588A publication Critical patent/HK36588A/en

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
HK365/88A 1982-02-10 1988-05-19 An airframe having a self-erecting wing structure HK36588A (en)

Applications Claiming Priority (1)

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

Publications (1)

Publication Number Publication Date
HK36588A true HK36588A (en) 1988-05-27

Family

ID=23364680

Family Applications (1)

Application Number Title Priority Date Filing Date
HK365/88A HK36588A (en) 1982-02-10 1988-05-19 An airframe having a self-erecting wing structure

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) ES8308060A1 (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

Also Published As

Publication number Publication date
BE894382A (en) 1983-03-14
IT1149076B (en) 1986-12-03
SE452364B (en) 1987-11-23
ES515721A0 (en) 1983-08-16
FR2521281A1 (en) 1983-08-12
IT8249119A0 (en) 1982-09-15
ES8308060A1 (en) 1983-08-16
DK410182A (en) 1983-08-11
NO150820B (en) 1984-09-10
NO150820C (en) 1985-01-09
JPS6364720B2 (en) 1988-12-13
FR2521281B1 (en) 1986-06-06
NL184340C (en) 1989-06-16
CH661347A5 (en) 1987-07-15
DK153183C (en) 1988-11-14
DK153183B (en) 1988-06-20
GB2115117A (en) 1983-09-01
IL66624A (en) 1986-04-29
AU530408B2 (en) 1983-07-14
SE8205200D0 (en) 1982-09-13
JPS58138998A (en) 1983-08-18
NL184340B (en) 1989-01-16
DE3234269C2 (en) 1985-05-09
CA1190434A (en) 1985-07-16
NL8203531A (en) 1983-09-01
NO823115L (en) 1983-08-11
KR840001706A (en) 1984-05-16
SE8205200L (en) 1983-08-11
DE3234269A1 (en) 1983-08-25
GB2115117B (en) 1985-11-06
KR860000220B1 (en) 1986-03-15

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Legal Events

Date Code Title Description
PC Patent ceased (i.e. patent has lapsed due to the failure to pay the renewal fee)