EP0376082A1 - Treibspiegel für ein unterkalibriges Geschoss - Google Patents
Treibspiegel für ein unterkalibriges Geschoss Download PDFInfo
- Publication number
- EP0376082A1 EP0376082A1 EP89123176A EP89123176A EP0376082A1 EP 0376082 A1 EP0376082 A1 EP 0376082A1 EP 89123176 A EP89123176 A EP 89123176A EP 89123176 A EP89123176 A EP 89123176A EP 0376082 A1 EP0376082 A1 EP 0376082A1
- Authority
- EP
- European Patent Office
- Prior art keywords
- sabot
- fixing part
- rear fixing
- front part
- carrier
- 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.)
- Withdrawn
Links
- 239000000463 material Substances 0.000 claims abstract description 12
- 238000013016 damping Methods 0.000 claims abstract description 6
- 239000002131 composite material Substances 0.000 claims description 2
- 239000004033 plastic Substances 0.000 claims description 2
- 238000000926 separation method Methods 0.000 abstract 1
- 229910000838 Al alloy Inorganic materials 0.000 description 2
- 239000004952 Polyamide Substances 0.000 description 2
- 238000004026 adhesive bonding Methods 0.000 description 2
- 239000007789 gas Substances 0.000 description 2
- 230000005484 gravity Effects 0.000 description 2
- 238000004519 manufacturing process Methods 0.000 description 2
- 229920002647 polyamide Polymers 0.000 description 2
- 239000004677 Nylon Substances 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 230000001771 impaired effect Effects 0.000 description 1
- 229920001778 nylon Polymers 0.000 description 1
- 239000003380 propellant Substances 0.000 description 1
- 238000007789 sealing Methods 0.000 description 1
- 238000005507 spraying Methods 0.000 description 1
- 230000006641 stabilisation Effects 0.000 description 1
- 238000011105 stabilization Methods 0.000 description 1
Images
Classifications
-
- 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
-
- 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
- F42B14/068—Sabots characterised by the material
Definitions
- the invention relates to a sabot for a sub-caliber projectile, which is segmented, and which has a support part defining a positive-locking zone between it and the projectile, a front part connected to the support part and formed with an air pocket, a rear fixing part connected to the support part and an intermediate the front part and the rear fixing part provided outer part.
- Such a sabot is known from DE 36 25 730 A1.
- the outer part has a fibrous portion that absorbs tensile stress and is connected to the carrier part.
- the fibrous portion has individual parts that extend between a front and a rear fixing area.
- This The sabot consists of a large number of individual parts, the individual parts of the fibrous portion in particular resulting in a considerable amount of assembly work in the production of such a sabot.
- This sabot can be provided with radial projections for rear support.
- the invention has for its object to provide a sabot of the type mentioned, which is simple in design and has relatively few individual parts, so that its manufacture is comparatively simple, and which is not pressed during its movement through an end pipe, but rather improves the flight characteristics is pulled.
- the carrier part has a low weight in relation to the front part
- the rear fixing part has a low weight in relation to the front part or to the carrier part and consists of a damping material.
- the front part connected to the carrier part preferably consists of a specifically heavier material than the carrier part.
- the carrier part can bpsw. from one Be aluminum alloy.
- the connection between the front part and the support part can bpsw. done by screw elements.
- the connection of the rear fixing part to the carrier part can be done by gluing, spraying or the like. respectively.
- the rear fixing part preferably has two concentric collars which are connected to one another by means of connecting ribs.
- Such a fixing part is simple to implement and can be mechanically firmly connected to the carrier part in a simple manner.
- the outer collar of the rear fixing part is preferably surrounded by a retaining ring which determines the caliber of the sabot.
- This retaining ring preferably consists of a material that is gentle on the weapon barrel.
- the front part of the sabot may be surrounded by a second retaining ring which determines the caliber of the sabot.
- This second retaining ring can consist of the same material as the retaining ring provided on the rear fixing part.
- the outer part of the sabot is preferably designed as a tubular sleeve.
- the tubular outer part serves to protect the weapon barrel and at the same time for stabilization purposes.
- FIG. 1 shows a sabot 10 cut longitudinally on one side and a projectile 12 shown in sections
- the sabot 10 has a carrier part 14 which forms a positive-locking zone 16 between it and the projectile 12.
- the carrier part 14 consists, for example, of an aluminum alloy.
- a fixing part 18 is connected at the rear to the carrier part 14, for example by gluing.
- the fixing part 18 can consist of a polyamide.
- the fixing part 18 has an outer collar 20 and an inner collar 22, which are arranged coaxially and are connected to one another by connecting ribs 24. From Fig. 2 it can also be seen that the fixing part 18 is divided into segments. The carrier part 14 is also segmented accordingly. The rear fixing part 18 is formed on its outer circumference with a circumferential groove 26 in which a retaining ring 28 is provided.
- a front part 30 is connected to the carrier part 14, for example by screw elements 32, the front part 30, which is segmented like the holding part 14, made of a specifically heavier material than the carrier part 14, so that the center of gravity S (see FIG. 1 ) is displaced far forward from the middle area of the sabot 10, so that a so-called sabot 10 results.
- the front part 30 is formed on its outer circumference with a circumferential groove 34 in which a second retaining ring 36 is arranged.
- the retaining rings 28 and 36 determine the caliber of the sabot 10.
- the front part 30 is formed with an air pocket 38, which is used for the targeted use of the air flowing in after leaving a gun barrel.
- the carrier part 14 is shaped in such a way that there is a gas pressure receiving surface 40 which passes through during the launch, ie during the passage the gun barrel is exposed to the propellant gases.
- An outer part 42 which is designed as a tubular sleeve and is held on the bow side by a ring element 44, extends between the front part 30 and the rear fixing part 18.
- This ring element 44 can be a sealing element, which can also be provided or instead of the second retaining ring 36 for determining the caliber of the sabot 10.
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Investigating Strength Of Materials By Application Of Mechanical Stress (AREA)
- Testing Of Engines (AREA)
- Vibration Dampers (AREA)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE3843968A DE3843968A1 (de) | 1988-12-24 | 1988-12-24 | Treibspiegel fuer ein unterkalibriges geschoss |
DE3843968 | 1988-12-24 |
Publications (1)
Publication Number | Publication Date |
---|---|
EP0376082A1 true EP0376082A1 (de) | 1990-07-04 |
Family
ID=6370315
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP89123176A Withdrawn EP0376082A1 (de) | 1988-12-24 | 1989-12-14 | Treibspiegel für ein unterkalibriges Geschoss |
Country Status (3)
Country | Link |
---|---|
US (1) | US4964342A (enrdf_load_stackoverflow) |
EP (1) | EP0376082A1 (enrdf_load_stackoverflow) |
DE (1) | DE3843968A1 (enrdf_load_stackoverflow) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2709821A1 (fr) * | 1993-09-08 | 1995-03-17 | Rheinmetall Gmbh | Sabot pour un projectile sous-calibré. |
WO2007057116A1 (de) * | 2005-11-18 | 2007-05-24 | Rheinmetall Waffe Munition Gmbh | Segmentierter zweiflansch-treibkäfig |
Families Citing this family (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5183961A (en) * | 1991-12-09 | 1993-02-02 | Olin Corporation | Extended charge cartridge assembly |
US5479736A (en) * | 1994-01-06 | 1996-01-02 | Cerberus Institute For Research And Development, Inc. | Augmented service pistol and ammunition weapons system |
DE19625273A1 (de) * | 1996-06-25 | 1998-01-15 | Bundesrep Deutschland | Faserverstärkter Treibkäfig |
DE102008029395A1 (de) * | 2008-06-23 | 2009-12-24 | Rheinmetall Waffe Munition Gmbh | Treibkäfiggeschoss |
Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
BE784548A (fr) * | 1972-05-13 | 1972-10-02 | Kopsch Paul J | Projectile a sabot perdu. |
US3834314A (en) * | 1972-12-29 | 1974-09-10 | Aai Corp | Puller sabot ammunition with slip seal |
EP0029107A1 (de) * | 1979-11-09 | 1981-05-27 | Rheinmetall GmbH | Treibkäfig für ein unterkalibriges Geschoss |
Family Cites Families (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB131034A (en) * | 1918-03-28 | 1919-08-21 | Leonard Godfrey Pinney Thring | Improvements in or relating to Subcalibre Projectiles. |
US2998778A (en) * | 1945-08-02 | 1961-09-05 | Charles E Hablutzel | Sabot retainer |
DE3021914A1 (de) * | 1980-06-11 | 1983-09-08 | Deutsch Franz Forsch Inst | Unterkalibergeschoss mit treibring |
EP0152492B1 (de) * | 1984-01-31 | 1987-12-23 | Rheinmetall GmbH | Munition-Einheit für Rohrwaffen |
AT388452B (de) * | 1984-10-24 | 1989-06-26 | Voest Alpine Ag | Unterkalibriges wuchtgeschoss |
DE3625730A1 (de) * | 1986-08-04 | 1988-02-18 | Rheinmetall Gmbh | Treibkaefig mit einem werkstoffverbund fuer ein unterkalibriges wuchtgeschoss grossen laenge/durchmesser-verhaeltnisses |
-
1988
- 1988-12-24 DE DE3843968A patent/DE3843968A1/de active Granted
-
1989
- 1989-12-06 US US07/446,998 patent/US4964342A/en not_active Expired - Fee Related
- 1989-12-14 EP EP89123176A patent/EP0376082A1/de not_active Withdrawn
Patent Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
BE784548A (fr) * | 1972-05-13 | 1972-10-02 | Kopsch Paul J | Projectile a sabot perdu. |
US3834314A (en) * | 1972-12-29 | 1974-09-10 | Aai Corp | Puller sabot ammunition with slip seal |
EP0029107A1 (de) * | 1979-11-09 | 1981-05-27 | Rheinmetall GmbH | Treibkäfig für ein unterkalibriges Geschoss |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2709821A1 (fr) * | 1993-09-08 | 1995-03-17 | Rheinmetall Gmbh | Sabot pour un projectile sous-calibré. |
US5481981A (en) * | 1993-09-08 | 1996-01-09 | Rheinmetall Gmbh | Sabot for a subcaliber projectile |
WO2007057116A1 (de) * | 2005-11-18 | 2007-05-24 | Rheinmetall Waffe Munition Gmbh | Segmentierter zweiflansch-treibkäfig |
Also Published As
Publication number | Publication date |
---|---|
DE3843968C2 (enrdf_load_stackoverflow) | 1991-10-02 |
DE3843968A1 (de) | 1990-07-05 |
US4964342A (en) | 1990-10-23 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
PUAI | Public reference made under article 153(3) epc to a published international application that has entered the european phase |
Free format text: ORIGINAL CODE: 0009012 |
|
17P | Request for examination filed |
Effective date: 19900421 |
|
AK | Designated contracting states |
Kind code of ref document: A1 Designated state(s): CH DE FR GB LI |
|
17Q | First examination report despatched |
Effective date: 19910805 |
|
STAA | Information on the status of an ep patent application or granted ep patent |
Free format text: STATUS: THE APPLICATION IS DEEMED TO BE WITHDRAWN |
|
18D | Application deemed to be withdrawn |
Effective date: 19921006 |