GB2148462A - Projectile with rotating band - Google Patents

Projectile with rotating band Download PDF

Info

Publication number
GB2148462A
GB2148462A GB08423830A GB8423830A GB2148462A GB 2148462 A GB2148462 A GB 2148462A GB 08423830 A GB08423830 A GB 08423830A GB 8423830 A GB8423830 A GB 8423830A GB 2148462 A GB2148462 A GB 2148462A
Authority
GB
United Kingdom
Prior art keywords
rotating band
base
projectile body
annular groove
projectile
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.)
Granted
Application number
GB08423830A
Other versions
GB2148462B (en
GB8423830D0 (en
Inventor
Dietrich Hoffman
Udo Gotz
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.)
Mauser Werke Oberndorf GmbH
Original Assignee
Mauser Werke Oberndorf GmbH
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 Mauser Werke Oberndorf GmbH filed Critical Mauser Werke Oberndorf GmbH
Publication of GB8423830D0 publication Critical patent/GB8423830D0/en
Publication of GB2148462A publication Critical patent/GB2148462A/en
Application granted granted Critical
Publication of GB2148462B publication Critical patent/GB2148462B/en
Expired legal-status Critical Current

Links

Classifications

    • 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
    • F42B14/064Sabots enclosing the rear end of a kinetic energy projectile, i.e. having a closed disk shaped obturator base and petals extending forward from said base
    • 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
    • F42B14/02Driving bands; Rotating bands

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Toys (AREA)
  • Housing For Livestock And Birds (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Purses, Travelling Bags, Baskets, Or Suitcases (AREA)
  • Tents Or Canopies (AREA)
  • Portable Nailing Machines And Staplers (AREA)

Abstract

A projectile body 8 for rapid fire weapons and high power machine guns has a synthetic rotating band 13 whose base 14 is wider than its projecting top surface, the band being disposed in a jacket for the projectile or in the cup 9 of a cartridge case base. <IMAGE>

Description

SPECIFICATION Projectile body with synthetic rotating band The invention relates to a projectile body, in particular for use in automatic rapid-fire weapons and high power machine guns, with a synthetic rotating band and an annular groove provided in the tail region of the projectile jacket for receiving the synthetic rotating band.
German Offenlegungsschrift 31 42 636 discloses a projectile body with a rotating band made from synthetic material, which in the tail region comprises an annular groove provided with intermediate webs for receiving and anchoring the synthetic rotating band. By means of the intermediate webs which are bent at an angle, which may be provided at their free ends with knurling, good anchorage of the synthetic rotating band on the projectile body is ensured. in this case, apart from possible recesses, the width of the synthetic rotating band corresponds to the width of the annular groove in the projectile body. Due to this, basically the possibilities of attachment of the rotating band to the projectile body are limited.
In a projectile body of the aforementioned type, it is the object of the invention to extend the possibilities of attachment of the synthetic rotating band to a projectile body to improve the range of application of synthetic rotating bands particularly with regard to thermal stress.
This object is achieved according to the invention due to the fact that the base of the synthetic rotating band inserted in the annular groove of the projectile body is wider than the top surface projecting radially from the annular groove. In this case, the width of the base of the synthetic rotating band may be approximately twice or three times that of the projecting top surface. In a particular embodiment of the idea of the invention, the top surface may be a relatively very narrow ring in the case of a base width increased by a multiple of this top surface width.
The basic idea of the invention is the widening of the rotating band base of synthetic rotating bands. In this case it has proved advantageous that consequently the function of a synthetic rotating band is improved essentially above all with respect to high thermal loads. This is a critical advantage especially in high power machine guns with a very high firing rate. A further essential advantage of the synthetic rotating bands according to the invention is the improvement of their range of application. Cartridge chamber dimensions can be provided so that only very narrow rotating bands can be produced. Without the widening of their base, the stability of the synthetic rotating bands on the projectile could only be solved with difficulty and with great technical expenditure.
In a further embodiment of the invention, the base of the synthetic rotating band can be anchored on a synthetic sleeve of a cartridgecase base applied to the projectile body on the rear side. This signifies an advantageous reduction of weight in the case of cartridgecase base ammunition, because due to this the metal cartridge-case base wall can be replaced by a light synthetic material. The base of the synthetic rotating band can be anchored by intermediate webs provided in the annular groove or by radial through holes provided in the annular groove.
One example of the invention is illustrated in the drawings in which: Figure 1 shows a projectile body with a synthetic rotating band according to the invention in section, Figure 2 shows a projectile body with a cartridge-case base wall of synthetic material in section and Figure 3 shows a temperature/time diagram with comparison curves of the conventional projectile body and of the projectile body according to the invention.
An annular groove 3 of relatively great width is located in the tail region of the projectile body 1 in its projectile jacket 2.
Inserted in the annular groove 3 is a synthetic rotating band 4 with a base 5 corresponding to the width of the annular groove. The top surface 6 of the synthetic rotating band 4 projecting radially from the annular groove 3 is substantially narrower than the base 5. In the example, the base is approximately more than twice the width of the top surface 6. The tail portion of the projectile body 1 is closed off by a projectile closing member 7.
In Fig. 2, a cartridge-case base wall in the form of a metal cup 9 for example made from aluminium is fitted onto the tail region of a projectile body 8. The cup 9 comprises radially projecting, bent webs 10, which lie in the form of an annulus on the outer surface of the cup 9. The base 11 of the cup 9 forms an abutment shoulder 1 2 for the synthetic rotating band 13 fitted. In this case, also, the synthetic rotating band 1 3 is provided with a substantial wider base 1 4 with respect to the top surface 15.
The diagram of Fig. 3 shows the two curves 16, 1 7 of the projectile body according to the invention and of the conventional projectile body with a synthetic rotating band in comparison to the temperature/time axis. The lower curve 1 6 corresponds to the normal anchorage 1 8 of the lower half of the projectile 19, whereas the curve 1 7 shows the anchorage 20 according to the invention of the upper half of the projectile 21. As can be seen and as was proved in tests the projectile bodies with an enlarged base of the synthetic rotating band still operate at substantially higher temperatures than is the case with conventionai projectile bodies with a synthetic rotating band. The curves clearly show the respective thermal stress in the unit of time.

Claims (7)

1. Projectile body, in particular for use in automatic rapid fire weapons and high power machine guns, with a synthetic rotating band and an annular groove provided in the tail region of the projectile jacket for receiving the synthetic rotating band, wherein the base of the synthetic rotating band inserted in the annular groove in the projectile body is wider than the top surface projecting radially from the annular groove.
2. Projectile body according to claim 1, wherein the width of the base of the synthetic rotating band is approximately two to three times greater than the projecting top surface.
3. Projectile body according to claim 1, wherein the top surface of the synthetic rotating band is a relatively narrow ring in the case of a base width enlarged by several times this top surface width.
4. Projectile body according to any one of claims 1 to 3, wherein the base of the synthetic rotating band is anchored on a metal cup of a cartridge-case base fitted to the projectile body on the rear side.
5. Projectile body according to any one of claims 1 to 4, wherein the base of the synthetic rotating band is anchored by intermediate webs provided in the annular groove, which intermediate webs are bent at an angle with respect to the base of the annular groove.
6. Projectile body according to any one of claims 1 to 5, wherein the base of the synthetic rotating band is anchored by radial through holes provided in the annular groove.
7. A projectile body substantially as herein described with reference to the accompanying drawings.
GB08423830A 1983-09-21 1984-09-20 Projectile with rotating band Expired GB2148462B (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE19833334023 DE3334023A1 (en) 1983-09-21 1983-09-21 BULLET BODY WITH PLASTIC GUIDE BAND

Publications (3)

Publication Number Publication Date
GB8423830D0 GB8423830D0 (en) 1984-10-24
GB2148462A true GB2148462A (en) 1985-05-30
GB2148462B GB2148462B (en) 1988-05-25

Family

ID=6209617

Family Applications (1)

Application Number Title Priority Date Filing Date
GB08423830A Expired GB2148462B (en) 1983-09-21 1984-09-20 Projectile with rotating band

Country Status (6)

Country Link
CH (1) CH669452A5 (en)
DE (1) DE3334023A1 (en)
GB (1) GB2148462B (en)
IT (2) IT1176713B (en)
NL (1) NL8402606A (en)
SE (1) SE459125B (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2195419A (en) * 1985-03-26 1988-04-07 Diehl Gmbh & Co A projectile
US4754707A (en) * 1986-09-16 1988-07-05 Diehl Gmbh & Company Projectile

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE10130383A1 (en) * 2001-06-23 2003-01-09 Diehl Munitionssysteme Gmbh Artillery projectile with interchangeable payload

Citations (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB419546A (en) * 1932-07-11 1934-11-14 Terni Ind Elettr Improvements in or relating to armour piercing projectiles
GB573904A (en) * 1943-02-03 1945-12-12 Claude William Denny Improvements in and relating to driving bands for projectiles
GB1092318A (en) * 1964-10-24 1967-11-22 Rheinmetall Gmbh A projectile comprising a driving band pressed into an anuular groove
GB1245906A (en) * 1969-01-20 1971-09-15 Bofors Ab Explosive shell
US3910194A (en) * 1971-02-01 1975-10-07 Hercules Inc Projectile rotating band
GB1512589A (en) * 1975-11-15 1978-06-01 Rheinmetall Gmbh Projectile
GB1541291A (en) * 1976-09-20 1979-02-28 Rheinmetall Gmbh Spin stabilized annular projectile
GB1562021A (en) * 1976-07-09 1980-03-05 Dynamit Nobel Ag Discarding sabot shell
EP0042457A1 (en) * 1978-10-23 1981-12-30 Martin Marietta Corporation Projectile obturator and projectile provided with such an obturator
DE3142636A1 (en) * 1981-10-28 1983-05-11 Mauser-Werke Oberndorf Gmbh, 7238 Oberndorf BULLET BODY WITH A PLASTIC GUIDE TAPE AND METHOD FOR THE PRODUCTION THEREOF
GB2123123A (en) * 1982-07-01 1984-01-25 Honeywell Inc Projectiles
GB2132321A (en) * 1982-12-24 1984-07-04 Mauser Werke Oberndorf Abridgement

Patent Citations (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB419546A (en) * 1932-07-11 1934-11-14 Terni Ind Elettr Improvements in or relating to armour piercing projectiles
GB573904A (en) * 1943-02-03 1945-12-12 Claude William Denny Improvements in and relating to driving bands for projectiles
GB1092318A (en) * 1964-10-24 1967-11-22 Rheinmetall Gmbh A projectile comprising a driving band pressed into an anuular groove
GB1245906A (en) * 1969-01-20 1971-09-15 Bofors Ab Explosive shell
US3910194A (en) * 1971-02-01 1975-10-07 Hercules Inc Projectile rotating band
GB1512589A (en) * 1975-11-15 1978-06-01 Rheinmetall Gmbh Projectile
GB1562021A (en) * 1976-07-09 1980-03-05 Dynamit Nobel Ag Discarding sabot shell
GB1541291A (en) * 1976-09-20 1979-02-28 Rheinmetall Gmbh Spin stabilized annular projectile
EP0042457A1 (en) * 1978-10-23 1981-12-30 Martin Marietta Corporation Projectile obturator and projectile provided with such an obturator
DE3142636A1 (en) * 1981-10-28 1983-05-11 Mauser-Werke Oberndorf Gmbh, 7238 Oberndorf BULLET BODY WITH A PLASTIC GUIDE TAPE AND METHOD FOR THE PRODUCTION THEREOF
GB2123123A (en) * 1982-07-01 1984-01-25 Honeywell Inc Projectiles
GB2132321A (en) * 1982-12-24 1984-07-04 Mauser Werke Oberndorf Abridgement

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2195419A (en) * 1985-03-26 1988-04-07 Diehl Gmbh & Co A projectile
GB2195419B (en) * 1985-03-26 1990-01-10 Diehl Gmbh & Co Projectile
US4754707A (en) * 1986-09-16 1988-07-05 Diehl Gmbh & Company Projectile

Also Published As

Publication number Publication date
NL8402606A (en) 1985-04-16
IT8423189V0 (en) 1984-09-18
IT8422710A1 (en) 1986-03-18
GB2148462B (en) 1988-05-25
CH669452A5 (en) 1989-03-15
GB8423830D0 (en) 1984-10-24
SE8404165D0 (en) 1984-08-21
SE8404165L (en) 1985-03-22
IT8422710A0 (en) 1984-09-18
DE3334023A1 (en) 1985-04-04
SE459125B (en) 1989-06-05
IT1176713B (en) 1987-08-18

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Legal Events

Date Code Title Description
PCNP Patent ceased through non-payment of renewal fee