CH378734A - Tail fin for projectiles, e.g. B. Missiles - Google Patents

Tail fin for projectiles, e.g. B. Missiles

Info

Publication number: CH378734A
Authority: CH; Switzerland
Prior art keywords: missiles; projectiles; tail fin; fin; tail
Prior art date: 1959-04-13

Application number

CH340560A

Other languages

German (de)

Inventor

Bertil Olsson Olof

Original Assignee

Bofors Ab

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.)

1959-04-13

Filing date

1960-03-26

Publication date

1964-06-15

1960-03-26 Application filed by Bofors Ab filed Critical Bofors Ab

1964-06-15 Publication of CH378734A publication Critical patent/CH378734A/en

Classifications

- 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
- F42B10/16—Wrap-around fins
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C9/00—Adjustable control surfaces or members, e.g. rudders
- B64C9/02—Mounting or supporting thereof
- 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

Landscapes

Engineering & Computer Science (AREA)
Physics & Mathematics (AREA)
Fluid Mechanics (AREA)
General Engineering & Computer Science (AREA)
Aviation & Aerospace Engineering (AREA)
Superstructure Of Vehicle (AREA)
Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
Mutual Connection Of Rods And Tubes (AREA)

CH340560A 1959-04-13 1960-03-26 Tail fin for projectiles, e.g. B. Missiles CH378734A (en)

Applications Claiming Priority (1)

Application Number	Priority Date	Filing Date	Title
SE350259		1959-04-13

Publications (1)

Publication Number	Publication Date
CH378734A true CH378734A (en)	1964-06-15

Family

ID=20262267

Family Applications (1)

Application Number	Title	Priority Date	Filing Date
CH340560A CH378734A (en)	1959-04-13	1960-03-26	Tail fin for projectiles, e.g. B. Missiles

Country Status (6)

Country	Link
US (1)	US3058422A (en)
BE (1)	BE589608A (en)
CH (1)	CH378734A (en)
DE (1)	DE1147514B (en)
GB (1)	GB869410A (en)
NL (2)	NL101734C (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number	Priority date	Publication date	Assignee	Title
DE102015004702A1 (en) *	2014-12-11	2016-06-16	Mbda Deutschland Gmbh	rudder system

Families Citing this family (13)

* Cited by examiner, † Cited by third party
Publication number	Priority date	Publication date	Assignee	Title
SE331242B (en) *	1969-05-14	1970-12-14	Bofors Ab
US3782668A (en) *	1970-09-25	1974-01-01	Us Army	Ramp forward of control fin
US4203569A (en) *	1977-10-17	1980-05-20	Bei Electronics, Inc.	Fin and nozzle unit for a free-flight rocket
US4717093A (en) *	1985-08-12	1988-01-05	Grumman Aerospace Corporation	Penguin missile folding wing configuration
US4691880A (en) *	1985-11-14	1987-09-08	Grumman Aerospace Corporation	Torsion spring powered missile wing deployment system
JP3781311B2 (en) *	1995-12-01	2006-05-31	株式会社小松製作所	Aircraft wing device
US6092264A (en) *	1998-11-13	2000-07-25	Lockheed Martin Corporation	Single axis fold actuator and lock for member
CN102774494A (en) *	2012-07-06	2012-11-14	北京林业大学	Aircraft folding rudder capable of stretching automatically
CN104677199B (en) *	2015-01-21	2016-07-13	浙江理工大学	A single-drive multi-folding rudder surface synchronous unfolding mechanism
WO2017143501A1 (en) *	2016-02-22	2017-08-31	SZ DJI Technology Co., Ltd.	Foldable multi-rotor aerial vehicle
CN106839897B (en) *	2017-01-03	2019-01-15	北京临近空间飞行器系统工程研究所	A kind of straight-line helix unfolded wing mechanism
CN109405669A (en) *	2018-08-31	2019-03-01	江西洪都航空工业集团有限责任公司	A kind of Quick Release aerofoil automatic locking mechanism
CN109253667A (en) *	2018-08-31	2019-01-22	江西洪都航空工业集团有限责任公司	A kind of Missile Folding rudder face longitudinal direction unfolding mechanism

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number	Priority date	Publication date	Assignee	Title
LU31733A1 (en) *	1951-11-07
NL104379C (en) *	1955-10-20		Brandt Soc Nouv Ets
US2923241A (en) *	1957-09-09	1960-02-02	Aerojet General Co	Folding stabilizing fins
FR1191519A (en) *	1958-02-13	1959-10-20	Hotchkiss Brandt	Deploying tail for artillery projectile

0
- NL NL250199D patent/NL250199A/xx unknown
- NL NL101734D patent/NL101734C/xx active
1960
- 1960-03-22 GB GB10116/60A patent/GB869410A/en not_active Expired
- 1960-03-26 CH CH340560A patent/CH378734A/en unknown
- 1960-03-29 DE DEA34339A patent/DE1147514B/en active Pending
- 1960-04-11 US US21285A patent/US3058422A/en not_active Expired - Lifetime
- 1960-04-11 BE BE589608A patent/BE589608A/en unknown

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number	Priority date	Publication date	Assignee	Title
DE102015004702A1 (en) *	2014-12-11	2016-06-16	Mbda Deutschland Gmbh	rudder system
US10006748B2 (en)	2014-12-11	2018-06-26	Mbda Deutschland Gmbh	Rudder system

Also Published As

Publication number	Publication date
NL101734C (en)
NL250199A (en)
BE589608A (en)	1960-08-01
DE1147514B (en)	1963-04-18
GB869410A (en)	1961-05-31
US3058422A (en)	1962-10-16

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