ES287013Y - Dispositivo para mejorar la conducta de desprendimiento de los segmentos de una jaula propulsora con una bolsa de aire delantera de un proyectil de energia cinetica estabilizado con aletas - Google Patents

Dispositivo para mejorar la conducta de desprendimiento de los segmentos de una jaula propulsora con una bolsa de aire delantera de un proyectil de energia cinetica estabilizado con aletas

Info

Publication number
ES287013Y
ES287013Y ES1984287013U ES287013U ES287013Y ES 287013 Y ES287013 Y ES 287013Y ES 1984287013 U ES1984287013 U ES 1984287013U ES 287013 U ES287013 U ES 287013U ES 287013 Y ES287013 Y ES 287013Y
Authority
ES
Spain
Prior art keywords
segments
detachment
fins
behavior
improve
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
ES1984287013U
Other languages
English (en)
Spanish (es)
Other versions
ES287013U (es
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.)
Rheinmetall Industrie AG
Direction General pour lArmement DGA
Original Assignee
Rheinmetall GmbH
Direction General pour lArmement DGA
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, Direction General pour lArmement DGA filed Critical Rheinmetall GmbH
Publication of ES287013U publication Critical patent/ES287013U/es
Application granted granted Critical
Publication of ES287013Y publication Critical patent/ES287013Y/es
Expired legal-status Critical Current

Links

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
    • 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
    • F42B10/32—Range-reducing or range-increasing arrangements; Fall-retarding means
    • F42B10/38—Range-increasing arrangements
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42—AMMUNITION; BLASTING
    • F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B12/00—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material
    • F42B12/02—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect
    • F42B12/20—Projectiles, 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
    • F42B12/22—Projectiles, 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
    • F42B12/24—Projectiles, 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
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42—AMMUNITION; BLASTING
    • F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B14/00—Projectiles or missiles characterised by arrangements for guiding or sealing them inside barrels, or for lubricating or cleaning barrels
    • F42B14/06—Sub-calibre projectiles having sabots; Sabots therefor
    • F42B14/061—Sabots 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)
  • Investigating Or Analyzing Materials By The Use Of Ultrasonic Waves (AREA)
  • Mechanical Pencils And Projecting And Retracting Systems Therefor, And Multi-System Writing Instruments (AREA)
  • Investigating Strength Of Materials By Application Of Mechanical Stress (AREA)
  • Organic Low-Molecular-Weight Compounds And Preparation Thereof (AREA)
  • Carbon And Carbon Compounds (AREA)
  • Pharmaceuticals Containing Other Organic And Inorganic Compounds (AREA)
  • Saccharide Compounds (AREA)
  • Memory System Of A Hierarchy Structure (AREA)
  • Buildings Adapted To Withstand Abnormal External Influences (AREA)
  • Portable Nailing Machines And Staplers (AREA)
  • Toys (AREA)
  • Other Air-Conditioning Systems (AREA)
  • Tires In General (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Steroid Compounds (AREA)
  • Heterocyclic Carbon Compounds Containing A Hetero Ring Having Nitrogen And Oxygen As The Only Ring Hetero Atoms (AREA)
  • Compositions Of Macromolecular Compounds (AREA)
ES1984287013U 1983-04-23 1984-04-18 Dispositivo para mejorar la conducta de desprendimiento de los segmentos de una jaula propulsora con una bolsa de aire delantera de un proyectil de energia cinetica estabilizado con aletas Expired ES287013Y (es)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE19833314750 DE3314750A1 (de) 1983-04-23 1983-04-23 Mittel zum verbessern des abloeseverhaltens von treibkaefigsegmenten von einem wuchtgeschoss fuer die rohrwaffe

Publications (2)

Publication Number Publication Date
ES287013U ES287013U (es) 1985-11-16
ES287013Y true ES287013Y (es) 1986-06-16

Family

ID=6197165

Family Applications (1)

Application Number Title Priority Date Filing Date
ES1984287013U Expired ES287013Y (es) 1983-04-23 1984-04-18 Dispositivo para mejorar la conducta de desprendimiento de los segmentos de una jaula propulsora con una bolsa de aire delantera de un proyectil de energia cinetica estabilizado con aletas

Country Status (14)

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

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 (de) * 1990-03-07 1991-09-12 Rheinmetall Gmbh Treibkaefig
DE4022462A1 (de) * 1990-07-14 1992-01-16 Diehl Gmbh & Co Luftverbringbares unterwasser-projektil
JP3065669B2 (ja) * 1995-06-07 2000-07-17 レイセオン・カンパニー 水中の目標に対して使用するための航学力学的に安定した弾丸システム
JPH10501883A (ja) * 1995-06-07 1998-02-17 エイチイー・ホールディングス・インコーポレーテッド・ドゥーイング・ビジネス・アズ・ヒューズ・エレクトロニクス 水中の目標に対して使用するための全口径弾丸
KR970705001A (ko) * 1995-06-07 1997-09-06 완다케이. 델슨-로우 수중 물체에 사용하기 위한 자이로스코프식으로 안정화된 발사체 시스템

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR454822A (fr) * 1912-09-26 1913-07-16 Robert Abbott Hadfield Perfectionnements aux chapeaux de projectiles perce-cuirasse
FR493570A (fr) * 1916-10-16 1919-08-13 Bento Caeiro Procédé et dispositif pour augmenter la portée des projectiles
US2373883A (en) * 1942-10-30 1945-04-17 Clyde B Ferrel Shell structure
FR1206606A (fr) * 1951-11-07 1960-02-10 Tech De Rech S Ind & Mecanique Projectile empenné
US3672304A (en) * 1970-03-30 1972-06-27 Lockheed Aircraft Corp Special purpose firearms projectile
DE2323244C3 (de) * 1973-05-09 1979-04-19 Rheinmetall Gmbh, 4000 Duesseldorf Flügelstabilisiertes Unterkalibergeschoß
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 (sv) * 1981-09-09 1986-05-20 Bofors Ab For ovningsendamal utskjutbar fenstabiliserad ammunitionsenhet

Also Published As

Publication number Publication date
EP0123266A1 (de) 1984-10-31
TR22229A (tr) 1986-10-09
BR8406813A (pt) 1985-03-19
DE3314750A1 (de) 1984-10-25
DK155857B (da) 1989-05-22
DK544884D0 (da) 1984-11-15
DK544884A (da) 1984-11-15
GR81472B (da) 1984-12-11
DE3466593D1 (en) 1987-11-05
KR850000664A (ko) 1985-02-28
PT78472A (en) 1984-05-01
ATE30081T1 (de) 1987-10-15
JPS61500076A (ja) 1986-01-16
WO1984004380A1 (en) 1984-11-08
AU557827B2 (en) 1987-01-08
DK155857C (da) 1989-10-02
EP0123266B1 (de) 1987-09-30
AU2822484A (en) 1984-11-19
PT78472B (en) 1986-03-20
IN161067B (da) 1987-09-26
ES287013U (es) 1985-11-16

Similar Documents

Publication Publication Date Title
US3692425A (en) Compressor for handling gases at velocities exceeding a sonic value
GB1530256A (en) Cooled blade for a gas turbine engine
DE3261740D1 (en) Stage of a gas turbine jet engine with air cooling means for the turbine rotor disc
GB1304678A (da)
US3934410A (en) Quiet shrouded circulation control propeller
ES287013Y (es) Dispositivo para mejorar la conducta de desprendimiento de los segmentos de una jaula propulsora con una bolsa de aire delantera de un proyectil de energia cinetica estabilizado con aletas
ATE14792T1 (de) Treibkaefig fuer unterkalibriges geschoss.
SE8100385L (sv) Ovningsprojektil
JPS5377319A (en) Axial-flow fan
JPS56138499A (en) Compressor structure for turbocharger
JPS5781191A (en) Method and device of improving characteristic of blower or the like
FR2403478A1 (fr) Procede et dispositif pour retarder et/ou reduire les effets de la cavitation autour d'une surface portante hydrodynamique tronquee a l'arriere
ES452096A1 (es) Procedimiento para aprovechar energia de presion de un medioexterior constituido por fluido o fluidos.
GB1087624A (en) Improvements in fluid accelerator or turbine
FR2268954A1 (en) Air-driven turbine in buoy - is designed to turn in same direction both during air blowing and suction phases
LEWIS Comparison of the effect of two damper sizes on the performance of a low-solidity axial-flow transonic compressor rotor(Performance of 20 inch diameter axial-flow transonic compressor rotor with small dampers and comparison with performance of rotor with large dampers)
JPS5234111A (en) Turbine moving blade
JPS54111109A (en) Inlet passage in axial-flow fans
SU533476A1 (ru) Привод дл многошпиндельных пневмогайковертов
ADKINS et al. The hybrid diffuser(for gas turbine engines)
Brooks The T 700 booster engine
JPS5692398A (en) Axial flow fan for cooling for internal combustion engine
POGODIN et al. Use of braking stages for control of turbine speed[Abstract Only]
RU98113695A (ru) Способ изменения формы профиля несущей поверхности летательного аппарата
GB1160201A (en) Turbine-Driven Character With Variable Area Diffuser

Legal Events

Date Code Title Description
MM1K Utility model lapsed

Effective date: 19960506