GR81472B - - Google Patents

Info

Publication number
GR81472B
GR81472B GR74442A GR840174442A GR81472B GR 81472 B GR81472 B GR 81472B GR 74442 A GR74442 A GR 74442A GR 840174442 A GR840174442 A GR 840174442A GR 81472 B GR81472 B GR 81472B
Authority
GR
Greece
Prior art keywords
projectile
flow range
speed flow
separation
circular groove
Prior art date
Application number
GR74442A
Other languages
Greek (el)
Inventor
H Becker
G Dr Glotz
J Dr Bocker
J Leeker
W Simon
J C Sauvestre
P Montier
Original Assignee
Rheinmetall Gmbh
France Etat Armement
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 Rheinmetall Gmbh, France Etat Armement filed Critical Rheinmetall Gmbh
Publication of GR81472B publication Critical patent/GR81472B/el

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
    • 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
    • F42B10/32Range-reducing or range-increasing arrangements; Fall-retarding means
    • F42B10/38Range-increasing arrangements
    • 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
    • F42B12/20Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect of high-explosive type
    • F42B12/22Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect of high-explosive type with fragmentation-hull construction
    • F42B12/24Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect of high-explosive type with fragmentation-hull construction with grooves, recesses or other wall weakenings
    • 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
    • F42B14/061Sabots for long rod fin stabilised kinetic energy projectiles, i.e. multisegment sabots attached midway on the projectile

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Fluid Mechanics (AREA)
  • Physics & Mathematics (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Testing Of Engines (AREA)
  • Mechanical Pencils And Projecting And Retracting Systems Therefor, And Multi-System Writing Instruments (AREA)
  • Investigating Or Analyzing Materials By The Use Of Ultrasonic Waves (AREA)
  • Investigating Strength Of Materials By Application Of Mechanical Stress (AREA)
  • Carbon And Carbon Compounds (AREA)
  • Pharmaceuticals Containing Other Organic And Inorganic Compounds (AREA)
  • Organic Low-Molecular-Weight Compounds And Preparation Thereof (AREA)
  • Saccharide Compounds (AREA)
  • Other Air-Conditioning Systems (AREA)
  • Memory System Of A Hierarchy Structure (AREA)
  • Tires In General (AREA)
  • Compositions Of Macromolecular Compounds (AREA)
  • Heterocyclic Carbon Compounds Containing A Hetero Ring Having Nitrogen And Oxygen As The Only Ring Hetero Atoms (AREA)
  • Steroid Compounds (AREA)
  • Toys (AREA)
  • Portable Nailing Machines And Staplers (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Buildings Adapted To Withstand Abnormal External Influences (AREA)

Abstract

The point portion (15) of a reduced calibre projectile (10) has a discontinuous contour in the form of a circular groove (20). Thereby, a boundary layer is determined between a supersonic speed flow range and a subsonic speed flow range; thereby it is possible to eliminate perturbations due to the flow during the separation of the sabot segments, not shown, of the projectile (10).
GR74442A 1983-04-23 1984-04-17 GR81472B (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE19833314750 DE3314750A1 (en) 1983-04-23 1983-04-23 AGENT FOR IMPROVING THE RELEASE BEHAVIOR OF DRIVING CAGE SEGMENTS FROM A RIFLE BULLET FOR THE PIPE ARM

Publications (1)

Publication Number Publication Date
GR81472B true GR81472B (en) 1984-12-11

Family

ID=6197165

Family Applications (1)

Application Number Title Priority Date Filing Date
GR74442A GR81472B (en) 1983-04-23 1984-04-17

Country Status (14)

Country Link
EP (1) EP0123266B1 (en)
JP (1) JPS61500076A (en)
KR (1) KR850000664A (en)
AT (1) ATE30081T1 (en)
AU (1) AU557827B2 (en)
BR (1) BR8406813A (en)
DE (2) DE3314750A1 (en)
DK (1) DK155857C (en)
ES (1) ES287013Y (en)
GR (1) GR81472B (en)
IN (1) IN161067B (en)
PT (1) PT78472B (en)
TR (1) TR22229A (en)
WO (1) WO1984004380A1 (en)

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2241309B (en) * 1986-02-20 1992-02-05 Royal Ordnance Plc Projectiles and components therefor
DE4007103A1 (en) * 1990-03-07 1991-09-12 Rheinmetall Gmbh Sabot for sub-calibre projectile
DE4022462A1 (en) * 1990-07-14 1992-01-16 Diehl Gmbh & Co Solid air-launched underwater projectile - has core with shortened front protected by ballistic cap
EP0774105B1 (en) * 1995-06-07 2000-03-08 Raytheon Company Aerodynamically stabilized projectile system for use against underwater objects
DE69606951T2 (en) * 1995-06-07 2000-11-16 Raytheon Co FULL-CALIBAR FLOOR FOR USE AGAINST UNDERWATER TARGETS
WO1996041114A1 (en) * 1995-06-07 1996-12-19 He Holdings, Inc., Doing Business As Hughes Electronics Gyroscopically stabilized projectile system for use against underwater objects

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR454822A (en) * 1912-09-26 1913-07-16 Robert Abbott Hadfield Breast Piercing Projectile Hats Improvements
FR493570A (en) * 1916-10-16 1919-08-13 Bento Caeiro Method and device for increasing the range of projectiles
US2373883A (en) * 1942-10-30 1945-04-17 Clyde B Ferrel Shell structure
FR1206606A (en) * 1951-11-07 1960-02-10 Tech De Rech S Ind & Mecanique Fletched projectile
US3672304A (en) * 1970-03-30 1972-06-27 Lockheed Aircraft Corp Special purpose firearms projectile
DE2323244C3 (en) * 1973-05-09 1979-04-19 Rheinmetall Gmbh, 4000 Duesseldorf Wing-stabilized sub-caliber bullet
US4405100A (en) * 1981-02-20 1983-09-20 The United States Of America As Represented By The Secretary Of The Navy Turbulence generator for maximizing configuration tolerances of free flight ordnance
SE444983B (en) * 1981-09-09 1986-05-20 Bofors Ab OVEN ENDAMAL EXTENSIBLE WINDOW STABILIZED AMMUNITION UNIT

Also Published As

Publication number Publication date
DE3466593D1 (en) 1987-11-05
DK155857C (en) 1989-10-02
TR22229A (en) 1986-10-09
ATE30081T1 (en) 1987-10-15
DK544884D0 (en) 1984-11-15
ES287013Y (en) 1986-06-16
PT78472A (en) 1984-05-01
KR850000664A (en) 1985-02-28
DK544884A (en) 1984-11-15
EP0123266A1 (en) 1984-10-31
BR8406813A (en) 1985-03-19
WO1984004380A1 (en) 1984-11-08
DE3314750A1 (en) 1984-10-25
IN161067B (en) 1987-09-26
PT78472B (en) 1986-03-20
AU2822484A (en) 1984-11-19
JPS61500076A (en) 1986-01-16
DK155857B (en) 1989-05-22
ES287013U (en) 1985-11-16
EP0123266B1 (en) 1987-09-30
AU557827B2 (en) 1987-01-08

Similar Documents

Publication Publication Date Title
DE3261740D1 (en) Stage of a gas turbine jet engine with air cooling means for the turbine rotor disc
IT8319318A0 (en) SYSTEM FOR REGULATING THE SPEED OF AN ENGINE.
JPS538855A (en) Condensing heat transmission wall
IT8322993A0 (en) METER OF THE INITIAL SPEED OF A PROJECTILE.
DE3273111D1 (en) Method and arrangement for the continuous running speed control of brushless d.c.motors
DE3378998D1 (en) Helicopter engine control with rotor speed decay anticipator
GB2090384B (en) Gun-launched variable thrust ramjet projectile
FR2521639B1 (en) HIGH PERFORMANCE PROPELLER PROPULSION ENGINE
DE3860591D1 (en) CENTRIFUGAL COMPRESSOR WITH AERODYNAMIC VARIABLE DIFFUSER GEOMETRY.
DE3376349D1 (en) Method for controlling the idling speed of a combustion engine
GB2070139B (en) Inlet cowl for supersonic aircraft engine
DE3466593D1 (en) Projectile with sabot
DE3261947D1 (en) Connection between the casing and the rear part of a sabot for a projectile
ES8707607A1 (en) Propulsion means for reducing the base drag.
DE3373004D1 (en) Turbine wheel having buckets or blades machined into the outer circumference of the wheel
IT8421823A1 (en) Integrated acceleration thruster stetoreactor missile propulsion assembly
FR2582798B1 (en) PROXIMITY ROCKET FOR ARTILLERY PROJECTILE OF THE TYPE WITH REDUCTION OF AERODYNAMIC PULL TRAIL
EP0398839A3 (en) Helicopter control with multiple schedule rotor speed decay anticipator
IT1151233B (en) PROCEDURE FOR PILOTING A LOW SPEED MISSILE, WEAPON AND MISSILE PLANT FOR IMPLEMENTING THE PROCEDURE
DE3373119D1 (en) High speed supersonic impulse turbine
EP0371505A3 (en) Linear driving apparatus
FR2387671A1 (en) Aerodynamic profile for arrow or discus - has helical groove around shaft or peripheral surface to produce rotation and reduced resistance
SE8504049D0 (en) ARRANGEMENT SPEED LIMIT
ES507880A0 (en) IMPROVEMENTS INTRODUCED IN A COMBUSTION ENGINE OF TWO TIMES WITH DISTRIBUTION OF THE SUCTION OF TWO DISC SHIRT VALVES.
JPS5738271A (en) System for controlling winder with taping function