IL42229A - Sabot projectile with pivoting vanes - Google Patents

Sabot projectile with pivoting vanes

Info

Publication number
IL42229A
IL42229A IL42229A IL4222973A IL42229A IL 42229 A IL42229 A IL 42229A IL 42229 A IL42229 A IL 42229A IL 4222973 A IL4222973 A IL 4222973A IL 42229 A IL42229 A IL 42229A
Authority
IL
Israel
Prior art keywords
vanes
projectile
sabot
axis
support means
Prior art date
Application number
IL42229A
Other languages
Hebrew (he)
Other versions
IL42229A0 (en
Original Assignee
Oerlikon Buehrle Ag
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 Oerlikon Buehrle Ag filed Critical Oerlikon Buehrle Ag
Publication of IL42229A0 publication Critical patent/IL42229A0/en
Publication of IL42229A publication Critical patent/IL42229A/en

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
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42BEXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B14/00Projectiles or missiles characterised by arrangements for guiding or sealing them inside barrels, or for lubricating or cleaning barrels
    • F42B14/06Sub-calibre projectiles having sabots; Sabots therefor

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Investigating Strength Of Materials By Application Of Mechanical Stress (AREA)
  • Testing Of Engines (AREA)
  • Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Rotary Pumps (AREA)

Claims (6)

42229/2 WHAT IS CLAIMED IS:
1. A sabot projectile comprising support means, vanes pivotably secured to said support means, said vanes in a first position forming a substantially pyramidvshaped sabot the peak of which (as seen in direction of light)points rearwardly, and which after pivoting about an axis into a second position form a substantially resistance-free guide mechanism, the said supporting means being fixed to a tail pipe characterised thereby that the said pyramid formed by the vanes is of larger diameter than the projectile and tightly bears against the inside of a firing barrel, said vanes in the first position tightly bearing against one another under the action of the gas pressure of the propellent charge, and further characterised thereby that at the outside of the tail pipe there is provided a propelling charge being positioned behind the vanes in the first position thereof.
2. The sabot projectile as defined in claim 1 wherein said vanes are substantially planar and upon assuming their second position form together with the support means a T-guide mechanism.
3. The sabot projectile as defined in claim 1, wherein said vanes are sections of cylindrical surfaces and said vanes, upon assuming their second position, form together with the support means a T-guide mechanism.
4. The sabot projectile as defined in claim 3, wherein the axis of the cylindrical surface defined by each vane and the projectile axis are located at the same side of the vanes.
5. The sabot projectile as defined in claim 3, wherein the axis of the cylindrical surface formed by each vane and the 42229/2 projectile axis is located at opposite sides of the vanes ·
6. The sabot projectile as defined in claim 1, wherein the diameter of the projectile reduces towards the rear thereof. P. 0. Box 33116, TEL-AVIV Attorneys for Applicant -9a-
IL42229A 1972-05-10 1973-05-09 Sabot projectile with pivoting vanes IL42229A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CH692472A CH552189A (en) 1972-05-10 1972-05-10 DRIVING MIRROR FLOOR.

Publications (2)

Publication Number Publication Date
IL42229A0 IL42229A0 (en) 1973-10-25
IL42229A true IL42229A (en) 1976-07-30

Family

ID=4317193

Family Applications (1)

Application Number Title Priority Date Filing Date
IL42229A IL42229A (en) 1972-05-10 1973-05-09 Sabot projectile with pivoting vanes

Country Status (7)

Country Link
US (1) US3845922A (en)
BE (1) BE799206A (en)
CH (1) CH552189A (en)
DE (1) DE2321746C3 (en)
FR (1) FR2183847B1 (en)
IL (1) IL42229A (en)
IT (1) IT987267B (en)

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2637461C2 (en) * 1976-08-20 1982-07-15 Messerschmitt-Bölkow-Blohm GmbH, 8000 München Tail unit for a missile
DE3933100A1 (en) * 1988-12-19 1990-06-28 Diehl Gmbh & Co CONTROL UNIT FOR A SUB-CALIBRATE ARROW FLOOR
FR2721702B1 (en) * 1994-06-28 1996-08-14 Luchaire Defense Sa Device for deploying a projectile fin.
FR2768809B1 (en) * 1997-09-24 1999-10-15 Giat Ind Sa LARGE CALIBER LONG RANGE FIELD ARTILLERY PROJECTILE
US9212877B2 (en) * 2012-07-05 2015-12-15 The United States Of America As Represented By The Secretary Of The Army Retention system for a deployable projectile fin

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CH493819A (en) * 1968-07-11 1970-07-15 Oerlikon Buehrle Ag Twist-free projectile with launch tube

Also Published As

Publication number Publication date
IT987267B (en) 1975-02-20
FR2183847A1 (en) 1973-12-21
DE2321746A1 (en) 1973-11-22
CH552189A (en) 1974-07-31
BE799206A (en) 1973-08-31
IL42229A0 (en) 1973-10-25
DE2321746C3 (en) 1978-04-13
DE2321746B2 (en) 1977-08-18
FR2183847B1 (en) 1976-09-10
US3845922A (en) 1974-11-05

Similar Documents

Publication Publication Date Title
GB1434034A (en) Method and equipment for forming a single cloud of radar reflecting chaff within the atmosphere
GB1364728A (en) Launching tube for a missile
GB1470821A (en) Artillery projectile fin assembly
IL42229A (en) Sabot projectile with pivoting vanes
GB1422987A (en) Projectile tail units
GB1351666A (en) Practice ammunition
GB1367755A (en) Irritant-gas projectile
EP0048644B1 (en) Vaned projectile of the arrow type
DE60022509D1 (en) DEVICE FOR SHOOTING SHOTS FROM A ROCKET
GB1452626A (en)
US5029530A (en) Cartridge case for a cased telescoped ammunition round
US4404887A (en) Recoil reducer
US2423453A (en) Projectile
ES449468A1 (en) Assembly for launching a projectile
US2485870A (en) Rocket target
US3009393A (en) Missile launcher
GB714747A (en) Improvements in projectiles containing an explosive in the form of a hollow charge
SE7603849L (en) EMPLOYEE DEVICE
CN2276624Y (en) Shell-less bullet
FR2008535A1 (en) Stabilised missile propulsion system
FR2038806A5 (en) Rocket assisted projectile or gun boosted - rocket
RU2034230C1 (en) Anti-hail rocket
FR2290648A1 (en) Projectile launching equipment - has braking propellant with ballast behind gunpowder charge
GB1153590A (en) Improvements in or relating to a Launcher for use in the Firing of Surface-Stabilised Rockets
GB746206A (en) Improvements relating to rocket motors