GB1581779A - Spin stabilized projectile - Google Patents
Spin stabilized projectile Download PDFInfo
- Publication number
- GB1581779A GB1581779A GB3436577A GB3436577A GB1581779A GB 1581779 A GB1581779 A GB 1581779A GB 3436577 A GB3436577 A GB 3436577A GB 3436577 A GB3436577 A GB 3436577A GB 1581779 A GB1581779 A GB 1581779A
- Authority
- GB
- United Kingdom
- Prior art keywords
- projectile
- base
- barrel
- joint
- spin
- 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
Links
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
- F42B14/02—Driving bands; Rotating bands
-
- 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
- F42B10/34—Tubular projectiles
Description
(54) A SPIN STABILIZIED PROJECTILE
(71) We, RHEINMETALL Gesellschaft mit beschränkter Haftung, of Ulmenstrasse 125, 4 Dusseldorf 1, German Federal
Republic, a Company organised and existing under the laws of the German Federal
Republic, do hereby declare the invention for which we pray that a Patent may be granted to us, and the method by which it is to be performed, to be particularly described in and by the following statement:
This invention relates to a spin stabilized projectile of annular construction having a propulsive base bearing against the rear end of the projectile and connected therewith whereby, after the cartridge charge has been fired the base and the projectile separate after leaving the barrel of the weapon.
According to this invention there is provided a spin stabilized annular projectile having a propulsive base bearing against the rear end of the projectile and connected thereto through a joint which holds during normal handling but which breaks due to shear forces occurring on firing due to spin acceleration imparted by the barrel and acting through a guide ring on the projectile.
With such a connection between the projectile and the base, the projectile is particularly simple and light weight requiring no special machining operations over and above the usual machining required for projectiles. The separation of the projectile and the base is generally reliable, since after the projectile has been fired the projectile and the base are no longer in any way mechanically connected, even when still in the barrel. Due to the rapid braking of the base by air resistance no further parts which may induce jump errors are separated froin the projectile.
The projectile due to the moderate overall weight for a given propulsive charge may have a very high initial velocity enabling a long flat trajectory to be obtained.
An embodiment according to the invention is shown by way of example in the accompanying drawing which is a longitudinal section.
As shown a projectile 2 is of annular form with a conical tapered part 2b and a cylindrical bore 2c and bears through an end surface 2a against a shoulder 6a of a propulsive base 6. The projectile 2 has a barrel guide ring 4 of sintered iron positioned in a peripheral groove.
Between the end 2a and shoulder 6a is provided a jointing agent or adhesive which gives a reliable joint for handling purposes between the projectile 2 and the base 6, but which is broken as a result of the shear force occurring during spin acceleration when the projectile is fired. These shear forces occur because only the projectile 2 has a guide ring 4, so that the twist is only transmitted through the projectile 2. The base 6, due to rotational inertia, tends to lag behind the twist imparted to the projectile 2.
The joint between the projectile and the base is sheared whilst both are still within the barrel of the weapon so that the base 6 separates from the projectile 2 as soon as they both leave the barrel. To prevent the end 2a and shoulder 6a from binding or seizing, the adhesive has anti-seizing or anti-binding properties. The jointing agent may be soft solder.
Due to friction between the contact surfaces of the projectile 2 and the base 6 after the soft-soldered joint has sheared, the solder melts and acts as a lubricant between the two parts to prevent binding or seizing between the surfaces of the parts. If the projectile 2 and the base 6 are interconnected by an adhesive, then this should also have anti-binding and anti-seizing properties. This can be achieved by the addition of suitable compounds to the adhesive.
WHAT WE CLAIM IS:
1. A spin stabilized annular projectile
**WARNING** end of DESC field may overlap start of CLMS **.
Claims (6)
1. A spin stabilized annular projectile having a propulsive base bearing against the rear end of the projectile and connected thereto through a joint which holds during normal handling but which breaks due to shear forces occurring on firing due to spin acceleration imparted by the barrel and acting through a guide ring on the projectile.
2. A projectile in accordance with Claim 1, wherein the projectile rear end engages a shoulder on the base through the joint.
3. A projectile in accordance with Claim 1 or 2, wherein the projectile and the base are interconnected by an adhesive.
4. A projectile in accordance with Claim 1 or 2, wherein the projectile and the base are interconnected by soft-solder.
5. A projectile in accordance with any preceding claim, wherein the joint is adapted to reduce binding or seizing of the surfaces after breaking.
6. An annular projectile constructed and arranged to function substantially as herein described with reference to the accompanying drawings.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE19762642187 DE2642187A1 (en) | 1976-09-20 | 1976-09-20 | RING STABILIZED RING FLOOR |
Publications (1)
Publication Number | Publication Date |
---|---|
GB1581779A true GB1581779A (en) | 1980-12-17 |
Family
ID=5988331
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB3436577A Expired GB1581779A (en) | 1976-09-20 | 1977-08-16 | Spin stabilized projectile |
Country Status (6)
Country | Link |
---|---|
CA (1) | CA1094387A (en) |
DE (1) | DE2642187A1 (en) |
FR (1) | FR2365097A1 (en) |
GB (1) | GB1581779A (en) |
IT (1) | IT1086134B (en) |
SE (1) | SE7709966L (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2130691A (en) * | 1982-11-24 | 1984-06-06 | Mauser Werke Oberndorf | Projectile with a tubular body |
Families Citing this family (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
NL7908989A (en) * | 1979-12-13 | 1981-07-16 | Eurometaal Nv | METHOD FOR MANUFACTURING A PROJECTILE WITH A TUBULAR BODY |
NL8100698A (en) * | 1981-02-12 | 1982-09-01 | Christiaan Cornelis Van Der Wi | BULLETS, GARNETS AND ROCKETS, EQUIPPED WITH A STRAIGHT TAPE CONTINUOUS CHANNEL. |
Family Cites Families (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CH6313A (en) * | 1893-01-09 | 1893-08-15 | Karl Krnka | New bullet for firearms |
FR801218A (en) * | 1935-05-01 | 1936-07-30 | Sagem | Forcing Belt Artillery Projectile |
BE556258A (en) * | 1956-03-30 | |||
US3769912A (en) * | 1970-10-23 | 1973-11-06 | W Friend | Spin-stabilized projectiles |
CA956179A (en) * | 1971-06-17 | 1974-10-15 | Her Majesty The Queen In Right Of Canada As Represented By The Minister Of National Defence Of Her Majesty's Canadian Government | Tubular projectile |
-
1976
- 1976-09-20 DE DE19762642187 patent/DE2642187A1/en not_active Ceased
-
1977
- 1977-08-16 GB GB3436577A patent/GB1581779A/en not_active Expired
- 1977-08-29 IT IT2703577A patent/IT1086134B/en active
- 1977-08-31 FR FR7726416A patent/FR2365097A1/en not_active Withdrawn
- 1977-09-06 SE SE7709966A patent/SE7709966L/en not_active Application Discontinuation
- 1977-09-08 CA CA286,316A patent/CA1094387A/en not_active Expired
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2130691A (en) * | 1982-11-24 | 1984-06-06 | Mauser Werke Oberndorf | Projectile with a tubular body |
Also Published As
Publication number | Publication date |
---|---|
SE7709966L (en) | 1978-03-21 |
FR2365097A1 (en) | 1978-04-14 |
IT1086134B (en) | 1985-05-28 |
DE2642187A1 (en) | 1978-03-23 |
CA1094387A (en) | 1981-01-27 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
PS | Patent sealed | ||
PCNP | Patent ceased through non-payment of renewal fee |