GB1304671A - - Google Patents

Info

Publication number
GB1304671A
GB1304671A GB109771A GB109771A GB1304671A GB 1304671 A GB1304671 A GB 1304671A GB 109771 A GB109771 A GB 109771A GB 109771 A GB109771 A GB 109771A GB 1304671 A GB1304671 A GB 1304671A
Authority
GB
United Kingdom
Prior art keywords
shafts
parts
assembly
flaps
jan
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
GB109771A
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 filed Critical
Publication of GB1304671A publication Critical patent/GB1304671A/en
Expired legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42BEXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B10/00Means 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
    • F42B10/02Stabilising arrangements
    • F42B10/14Stabilising arrangements using fins spread or deployed after launch, e.g. after leaving the barrel
    • F42B10/16Wrap-around fins
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42BEXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B12/00Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material
    • F42B12/02Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect
    • F42B12/36Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect for dispensing materials; for producing chemical or physical reaction; for signalling ; for transmitting information
    • F42B12/56Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect for dispensing materials; for producing chemical or physical reaction; for signalling ; for transmitting information for dispensing discrete solid bodies
    • F42B12/58Cluster or cargo ammunition, i.e. projectiles containing one or more submissiles
    • F42B12/62Cluster or cargo ammunition, i.e. projectiles containing one or more submissiles the submissiles being ejected parallel to the longitudinal axis of the projectile

Abstract

1304671 Braking means on projectiles BOFORS AB 8 Jan 1971 [8 Jan 1970] 1097/71 Heading F3A A smoke, gas or illuminating flare or other assembly for separation from a spinning projectile comprises a body 5 provided with a plurality of flaps 3 which are erected under the action of centrifugal force and brake the spinning movement. The flaps comprise two parts 15 and 16 which are wrapped around respective shafts 14 and are integral with one another, or are joined together along edges 15a and 16a. The design of the flaps is such that the total centrifugal loadings on the two parts are equal or differ by less than the resistance to being pulled around the shafts. Additional resistance to pulling around the shafts is provided by spot welding, riveting, soldering and/or adhering the two parts together at points remote from the shafts. The two parts are of the same or different lengths. The body 5 is attached to a parachute 6 and is expelled from the remainder of the assembly by a charge 13. A parachute attached at 11 reduces the axial velocity of the assembly as it separates from the projectile.
GB109771A 1970-01-08 1971-01-08 Expired GB1304671A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
SE00147/70A SE339646B (en) 1970-01-08 1970-01-08

Publications (1)

Publication Number Publication Date
GB1304671A true GB1304671A (en) 1973-01-24

Family

ID=20256110

Family Applications (1)

Application Number Title Priority Date Filing Date
GB109771A Expired GB1304671A (en) 1970-01-08 1971-01-08

Country Status (7)

Country Link
US (1) US3702588A (en)
DE (1) DE2100489C3 (en)
FR (1) FR2075263A5 (en)
GB (1) GB1304671A (en)
IL (1) IL35877A (en)
NL (1) NL7100151A (en)
SE (1) SE339646B (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0182018A1 (en) * 1984-09-27 1986-05-28 Rheinmetall GmbH War head
EP0242180A2 (en) * 1986-04-15 1987-10-21 British Aerospace Public Limited Company Deployment arrangement for spinning body
GB2246420A (en) * 1990-07-13 1992-01-29 Royal Ordnance Plc Surveillance apparatus.

Families Citing this family (24)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
SE353956B (en) * 1971-06-24 1973-02-19 Bofors Ab
US3834312A (en) * 1973-03-14 1974-09-10 Bofors Ab Parachute-borne flare assemblage
FR2260772B1 (en) * 1974-02-08 1976-06-25 France Etat
DE2518645C2 (en) * 1975-04-26 1986-07-17 Rheinmetall GmbH, 4000 Düsseldorf Twist brake for a payload that can be ejected from a twist projectile
US4004514A (en) * 1976-01-20 1977-01-25 The United States Of America As Represented By The Secretary Of The Navy Roll rate stabilized wrap around missile fins
SE416235B (en) * 1976-12-27 1980-12-08 Bofors Ab BRAKE DEVICE FOR ROTATING BODY
IL63885A (en) * 1981-09-20 1988-04-29 Aryeh Ashkenazi Telescopic projectile and apparatus for firing same
DE3422231A1 (en) * 1984-06-15 1985-12-19 Diehl GmbH & Co, 8500 Nürnberg DEVICE FOR AERODYNAMICALLY BRAKING THE ROTATIONAL MOVEMENT OF A BODY
NL192056C (en) * 1985-03-12 1997-01-07 Eurometaal Nv Cylindrical metal holder with rotation brake flaps.
SE460436B (en) * 1986-12-01 1989-10-09 Bofors Ab DEVICE TO REDUCE ROTATION AND AT THE SAME TIME GET A SIDE SPEED OF A ROTATING AMMUNITION UNIT
US5117731A (en) * 1991-11-04 1992-06-02 The United States Of America As Represented By The Secretary Of The Navy Tactical acoustic decoy
CH685069A5 (en) * 1991-12-18 1995-03-15 Contraves Ag Sub-calibre, fin-stabilised projectile which is fired with spin
SE508858C2 (en) * 1997-03-25 1998-11-09 Bofors Ab Fine stabilized grenade
SE508857C2 (en) * 1997-03-25 1998-11-09 Bofors Ab Fine stabilized base bleed grenade
SE518665C2 (en) * 2000-03-21 2002-11-05 Bofors Weapon Sys Ab Fine stabilized artillery grenade
SE521445C2 (en) 2001-03-20 2003-11-04 Bofors Defence Ab Methods for synchronizing the fine precipitation in a finely stabilized artillery grenade and a correspondingly designed artillery grenade
US6745978B1 (en) * 2003-03-24 2004-06-08 At&T Corp. Aerodynamic stabilization of a projectile
US6783095B1 (en) 2003-03-24 2004-08-31 At&T Corp. Deployable flare for aerodynamically stabilizing a projectile
DE102005026070B4 (en) * 2005-06-07 2009-07-09 Diehl Bgt Defence Gmbh & Co. Kg Wing arrangement and missile
US8816261B1 (en) * 2011-06-29 2014-08-26 Raytheon Company Bang-bang control using tangentially mounted surfaces
IL231186A (en) * 2014-02-26 2017-07-31 Israel Aerospace Ind Ltd Fin deployment system
SE540780C2 (en) * 2016-04-06 2018-11-06 Bae Systems Bofors Ab Divisible grenade with parachute
US10466023B2 (en) * 2018-03-28 2019-11-05 Ascendance International, LLC Long range large caliber frangible round for defending against UAV'S
DE102021005973A1 (en) 2021-12-03 2023-06-07 Diehl Defence Gmbh & Co. Kg Projectile with fins that can be swung out without springs

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US17407A (en) * 1857-05-26 Improved projectile for killing whales
US617376A (en) * 1899-01-10 Railroad signal-fusee
US2599703A (en) * 1949-09-02 1952-06-10 Bendix Aviat Corp Lockout warning system for home heating apparatus
DE1159314B (en) * 1962-07-11 1963-12-12 Werner Gohlke Dr Ing Elastic folding tail, especially for flying bodies
US3578796A (en) * 1968-09-25 1971-05-18 Thiokol Chemical Corp Spinning and stabilizing system for solid propellant rocket or missiles

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0182018A1 (en) * 1984-09-27 1986-05-28 Rheinmetall GmbH War head
EP0242180A2 (en) * 1986-04-15 1987-10-21 British Aerospace Public Limited Company Deployment arrangement for spinning body
EP0242180B1 (en) * 1986-04-15 1991-09-04 British Aerospace Public Limited Company Deployment arrangement for spinning body
GB2246420A (en) * 1990-07-13 1992-01-29 Royal Ordnance Plc Surveillance apparatus.

Also Published As

Publication number Publication date
DE2100489B2 (en) 1974-11-28
US3702588A (en) 1972-11-14
DE2100489A1 (en) 1971-07-15
NL7100151A (en) 1971-07-12
SE339646B (en) 1971-10-11
IL35877A (en) 1974-05-16
IL35877A0 (en) 1971-04-28
FR2075263A5 (en) 1971-10-08
DE2100489C3 (en) 1975-07-17

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Legal Events

Date Code Title Description
PS Patent sealed [section 19, patents act 1949]
PE20 Patent expired after termination of 20 years