GB683484A - Ammunition projectile - Google Patents

Ammunition projectile

Info

Publication number
GB683484A
GB683484A GB3499/50A GB349950A GB683484A GB 683484 A GB683484 A GB 683484A GB 3499/50 A GB3499/50 A GB 3499/50A GB 349950 A GB349950 A GB 349950A GB 683484 A GB683484 A GB 683484A
Authority
GB
United Kingdom
Prior art keywords
casing
web
ball
projectile
balls
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
GB3499/50A
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.)
BRANDT SOC NOUV ETS
Original Assignee
BRANDT SOC NOUV ETS
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 BRANDT SOC NOUV ETS filed Critical BRANDT SOC NOUV ETS
Publication of GB683484A publication Critical patent/GB683484A/en
Expired legal-status Critical Current

Links

Classifications

    • 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
    • F42B12/04Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect of armour-piercing type
    • F42B12/10Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect of armour-piercing type with shaped or hollow charge
    • F42B12/12Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect of armour-piercing type with shaped or hollow charge rotatably mounted with respect to missile housing
    • CCHEMISTRY; METALLURGY
    • C07ORGANIC CHEMISTRY
    • C07DHETEROCYCLIC COMPOUNDS
    • C07D499/00Heterocyclic compounds containing 4-thia-1-azabicyclo [3.2.0] heptane ring systems, i.e. compounds containing a ring system of the formula:, e.g. penicillins, penems; Such ring systems being further condensed, e.g. 2,3-condensed with an oxygen-, nitrogen- or sulfur-containing hetero ring
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42BEXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B15/00Self-propelled projectiles or missiles, e.g. rockets; Guided missiles

Abstract

683,484. Self-propelled missiles. SOC. NOUVELLE DES ETABLISSEMENTS BRANDT. Feb. 10, 1950 [Feb. 15, 1949], No. 3499/50. Classes 9(i) and 9(ii), A spin-stabilized projectile with at least one part so arranged that it does not partake o f t h e rotary motion has a casing having an inertia such that the product of the inertia and the speed of rotation is sufficient to stabilize the projectile, while the non-rotary part is mounted freely in the casing and bears against the casing through a rear pivot. Fig. 1 shows a projectile for use against armour plate and the like having a casing 1 divided into two compartments by a web 2. The forward compartment 3 houses a hollow charge in a frusto - conical container 5 closed by a cap 6, a liner 8 fitting the cavity in the charge. The container 8 bears against the web 2 through a pivot comprising two .bearing blocks 10, 11 mounted respectively in the container 5 and the web 2. The blocks are of tungsten carbide or other hard material and are brazed in mountings 12, 13 respectively of mild steel or other material of sufficient plasticity to protect the blocks from shock. The container 5 is centred by ball-bearings, the. front bearing comprising balls 14 housed between bearing surfaces 15, 17. The balls 14 also bear against a cylindrical surface 18 of the container and a coaxial surface 19 of the casing. In the rear guidebearing, balls 20 are housed in a cup 21 projecting from the web 2. By a suitable choice of diameters for the balls 14, 20, the tendency of the hollow charge to rotate in the opposite direction to the casing may exactly compensate the tendency to direct rotation due to friction of the ball-bearings and the abutment pivot. The projectiles may be fired from a rifled gun, the casing then being provided with a driving band 57 and the rear compartment containing an explosive, incendiary, smoke-producing or propellent charge. Alternatively the projectile may be fired as a rocket, the rotation being produced by suitably inclined nozzles. In Fig. 1 the rear compartment contains a propellent charge comprising coaxial cylindrical sticks of powder 24, 25, 26, 27 supported between a shoulder 28 of the casing and a nozzle-carrying member 29 by gratings 33, 35. The outermost cylinder 24 is slit along its length to facilitate insertion in the casing. A coating 32 of thermoplastic resin adhering to the metal and powder may be interposed between the cylinder 24 and the casing 1. The gratings 33 and 35 have projections engaging between the cylinders 25, 26, 27. The grating 33 bears through a ball 37 against the web 2, the cup seating for the ball being surrounded by a baffle 38a stuffed with grease. The rear grating houses a ball 39 bearing against an adjusting screw 42 and a baffle 43a surrounding the ball seating is stuffed with grease. Heat insulating material may be applied to the surfaces of the cylinders contacting the projections 36. The nozzles 45 are fitted into openings in the member 29 with their longitudinal axes Y-Y so inclined that as the propellent gases emerge they cause the projectile to rotate. An axial nozzle 47 is closed by a disc 48 of Cu or Al, which is blown out when the pressure exceeds a maximum value. A safety spider 49 prevents the complete ejection of the disc. An electric primer 60 is embedded in a pellet 61 of black powder housed between the web 2 and the forward grating 33. When the primer is fired by means of lead wires (not shown) passing between the propellent sticks and out through a nozzle,. the propellant is ignited by the pellet 61. As the propellant burns; the grease protects the balls 37, 39 from the flames while the cylinder 24 burns only on its inner surface. The total gas pressure may be controlled by using a highly exothermicpropellant and easily eroded nozzles, e.g. low-carbon steel or by so shaping the propellant that the combustion surface decreases as a function of time. The nozzles may be formed in the end closure of the casing 1. The hollow charge may be replaced by a self-guiding device or by lifting surfaces. The hollow charge may be given an initial rotation in the opposite sense from that of the casing 1.
GB3499/50A 1949-02-15 1950-02-10 Ammunition projectile Expired GB683484A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR985015T 1949-02-15

Publications (1)

Publication Number Publication Date
GB683484A true GB683484A (en) 1952-11-26

Family

ID=9537117

Family Applications (1)

Application Number Title Priority Date Filing Date
GB3499/50A Expired GB683484A (en) 1949-02-15 1950-02-10 Ammunition projectile

Country Status (6)

Country Link
US (1) US2623465A (en)
BE (1) BE493685A (en)
CH (1) CH283465A (en)
FR (1) FR985015A (en)
GB (1) GB683484A (en)
NL (1) NL90798C (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1111066B (en) * 1958-02-10 1961-07-13 Rheinmetall Gmbh Twist-stabilized shaped charge projectile
DE977712C (en) * 1957-03-03 1968-08-08 Franz Rudolf Dipl-Ing Thomanek A missile-powered missile equipped with a lined shaped charge
GB2162927A (en) * 1977-10-27 1986-02-12 Bayern Chemie Gmbh Flugchemie A solid rocket propulsion system

Families Citing this family (33)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2865168A (en) * 1952-07-09 1958-12-23 Alex Deutsch Fuel burning reaction motor powered hydraulic and electric power unit
DE1142536B (en) * 1952-08-12 1963-01-17 Charlotte Vogt Geb Petersen Rotationally symmetrical hollow explosive charge
NL180360B (en) * 1952-09-15 1900-01-01 Konstantin Andreevich Lavrenti DEVICE FOR RECOVERY OF VIDEO INFORMATION FROM A MAGNETIC BAND.
DE1005874B (en) * 1953-05-19 1957-04-04 Bofors Ab Rocket engine, preferably for rocket projectiles
DE1012540B (en) * 1953-09-28 1957-07-18 Ludwig Bucklisch Shaped charge projectile
US2939275A (en) * 1954-02-24 1960-06-07 Unexcelled Chemical Corp Solid-fuel rocket type motor assemblies
US2877504A (en) * 1954-08-02 1959-03-17 Phillips Petroleum Co Method of bonding propellant grain to metal case
US2923126A (en) * 1955-02-17 1960-02-02 Soc Tech De Rech Ind Propulsion system
US2981188A (en) * 1955-10-10 1961-04-25 Henry S Lipinski Spin-stabilized projectile with nonrotating shaped charge
NL211988A (en) * 1955-11-10
US2956400A (en) * 1957-06-05 1960-10-18 Curtiss Wright Corp Internal-ribbed exhaust nozzle for jet propulsion devices
US3724216A (en) * 1957-06-13 1973-04-03 Us Navy Combined rocket-ram-jet aircraft
US2911912A (en) * 1957-06-27 1959-11-10 United Aircraft Corp Roll control means
US3000306A (en) * 1958-01-09 1961-09-19 Gen Dynamics Corp Solid propellant propulsion system
US3029734A (en) * 1958-10-02 1962-04-17 Phillips Petroleum Co Separation of stages in a staged rocket
US3008379A (en) * 1958-11-07 1961-11-14 Curtiss Wright Corp Low dispersion missile and launching structure
US3072055A (en) * 1959-08-03 1963-01-08 Ross Sidney Gun launched, terminal guided projectile
US3095163A (en) * 1959-10-13 1963-06-25 Petroleum Res Corp Ionized boundary layer fluid pumping system
US3067681A (en) * 1960-01-04 1962-12-11 Telecomputing Corp Guided missile
US3093074A (en) * 1960-01-08 1963-06-11 Foras Joseph De Means for protecting flight vehicles from injury attributable to heat of air friction
NL272938A (en) * 1961-01-05
US3191379A (en) * 1961-03-08 1965-06-29 Ralph M Pierce Propellant grain for rocket motors
FR1327090A (en) * 1962-03-20 1963-05-17 Snecma Improvement to thrusters with several reaction nozzles
US3802345A (en) * 1962-05-02 1974-04-09 Aai Corp Multiple projectile sabot assembly for use in rifled barrel
US3251301A (en) * 1962-09-12 1966-05-17 Lockheed Aircraft Corp Missile and launcher system
US3274772A (en) * 1963-07-16 1966-09-27 Gen Motors Corp Continuously staged rocket construction
US3225694A (en) * 1964-01-20 1965-12-28 Gunnar P Michelson Missile
US3361385A (en) * 1965-04-02 1968-01-02 Bert B. Gould Miniature ballistic rocket
US3372548A (en) * 1965-06-17 1968-03-12 Thiokol Chemical Corp Rocket nozzle
US4063512A (en) * 1966-10-05 1977-12-20 The United States Of America As Represented By The Secretary Of The Air Force Armor penetrating projectile
CH520316A (en) * 1970-02-27 1972-03-15 Oerlikon Buehrle Ag Spin-stabilized missile projectile
US4690350A (en) * 1985-12-19 1987-09-01 Raytheon Company Despinning mechanism
US4796534A (en) * 1988-01-22 1989-01-10 The United States Of America As Represented By The Secretary Of The Army Spinning ramjet vehicle with a non-spinning combustor

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US422636A (en) * 1890-03-04 Shell for high explosives
US1102653A (en) * 1913-10-01 1914-07-07 Robert H Goddard Rocket apparatus.
FR502560A (en) * 1916-08-21 1920-05-19 Procedes Westinghouse Leblanc Aerial torpedo
US1305216A (en) * 1917-12-11 1919-05-27 Clarence Janes Projectile.
US1307607A (en) * 1918-06-13 1919-06-24 Willie A Wilkins Projectile.
FR530223A (en) * 1921-01-27 1921-12-17 Improvements made to projectiles, with a view to increasing the length of their trajectory
GB543739A (en) * 1940-06-07 1942-03-11 Casimir Stanislas Piestrak Improvements in or relating to projectiles
US2441388A (en) * 1942-08-19 1948-05-11 George W Blackinton Projectile
US2519878A (en) * 1946-07-31 1950-08-22 Carold F Bjork Rocket projectile

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE977712C (en) * 1957-03-03 1968-08-08 Franz Rudolf Dipl-Ing Thomanek A missile-powered missile equipped with a lined shaped charge
DE1111066B (en) * 1958-02-10 1961-07-13 Rheinmetall Gmbh Twist-stabilized shaped charge projectile
GB2162927A (en) * 1977-10-27 1986-02-12 Bayern Chemie Gmbh Flugchemie A solid rocket propulsion system

Also Published As

Publication number Publication date
BE493685A (en)
US2623465A (en) 1952-12-30
CH283465A (en) 1952-06-15
FR985015A (en) 1951-07-13
NL90798C (en)

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