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EP 0 073 385 B2 |
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NEW EUROPEAN PATENT SPECIFICATION |
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Date of publication and mentionof the opposition decision: |
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31.03.1993 Bulletin 1993/13 |
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Mention of the grant of the patent: |
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12.11.1986 Bulletin 1986/46 |
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Date of filing: 13.08.1982 |
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International Patent Classification (IPC)5: F42B 12/04 |
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Multiple component penetrator projectile
Mehrkomponenten-Wuchtgeschoss
Projectile perforant à parties multiples
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Designated Contracting States: |
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AT DE FR GB NL |
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Priority: |
31.08.1981 US 297902
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Date of publication of application: |
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09.03.1983 Bulletin 1983/10 |
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Proprietor: GTE Products Corporation |
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Wilmington, DE 19801 (US) |
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Inventors: |
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- Kegel, Andrew John
Ulster, Pa. 18850 (US)
- Spencer, James Richard
Payre, Pa. 18840 (US)
- Smith, James Sterrett
Towanda, Pa. 18848 (US)
- Rhodes, Russell Harding
Nonroeton, Pa. 18832 (US)
- Mullendore, James Alan
Towanda, Pa. 18848 (US)
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Representative: Grünecker, Kinkeldey,
Stockmair & Schwanhäusser
Anwaltssozietät |
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Maximilianstrasse 58 80538 München 80538 München (DE) |
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References cited: :
EP-A- 0 051 375 DE-B- 1 208 656 FR-A- 1 231 010 GB-A- 538 268 GB-A- 1 605 153 US-A- 3 888 636
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EP-B- 73 384 DE-B- 2 848 019 FR-E- 75 765 GB-A- 1 514 908 US-A- 2 393 648 US-A- 3 979 234
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[0001] The present invention relates to a multiple component penetrator projectile comprising
a body component and a tail component joined to one end of the body component, the
latter consisting of frangible tungsten material. A penetrator projectile of this
type is shown in EP-A-51375, published 12.05.82, this document being an intermediate
document coming thereby within the provisions of Articles 54(3) and 89 EPC.
[0002] According to the above identified prior art document the body component (mid-section)
consists or a frangible tungsten alloy whereas the tail component consists of a high
strength tungsten alloy or equivalent metal commonly used for armor-piercing projectiles.
[0003] As used herein the term "frangible material" means a material which, under high velocity
impact against a target, will break into small fragments while penetrating the target.
While frangible materials can penetrate light armor and break up into small fragments,
generally they are difficult to machine using conventional machining techniques.
[0004] The multiple component penetrator projectile of the afore identified prior art document
has a cavity in its tail section for a tracer and in some instances such cavities
also can hold a self-destruct mechanism to avoid hazards to friendly personnel, equipment
or installations from projectiles not hitting the target. In the prior art multiple
component penetrator projectile, the tail component consisting of high strength tungsten
alloy or equivalent armor-piercing metal is used in order to permit the defeat of
spaced multiple plate targets as represented. For example, by aircraft or helicopters
equippped with armored cockpits or other protected components.
[0005] In FR-E-75765 there is known a multiple component penetrator projectile comprising
a body component and a tail component joined to one end of the body component. the
latter consisting of a high hardness metal for instance sinter tungsten carbide and
the tail component consisting of a high density metal for instance sinter tungsten
or uranium 238.
[0006] Furthermore, in FR-A-1 231 010 there is disclosed a multiple component penetrator
projectile of which the tail component consists of tungsten alloy with a high content
of tungsten or a material with at least the density of the body but less expensive
and more machinable.
[0007] It is the object of the present invention to provide a multiple component penetrator
projectile such that it provides flexibility in manufacture and overcomes some of
the problems associated with the prior art and constitute an advancement in the art.
[0008] The above object of the present invention is achieved by the invention as claimed
in claim 1.
[0009] Preferred embodiments of further improvements of the claimed invention are defined
in the subclaims.
[0010] Some ways of carrying out the invention are described below in detail with reference
to drawings which illustrate several preferred embodiments, in which:
Figures 1, 2 and 3 show longitudinal cross- sectional views of projectiles according
to the present invention.
[0011] Frangible materials are known. In addition, frangible alloys of tungsten are known,
such as 98W-2Ni, 97W-2.1 Ni-0.9Fe, and 90W-10Mo and tungsten doped with about400 ppm
of nickel. All of these materials will penetrate a target such as a 2" (5 cm) thick
steel armor plate, when fired at a high velocity such as from an anti-tank gun, then
break into small fragments while penetrating or exiting from the plate. Such materials,
while exhibiting the desired frangibility, have a tendency to form cracks when cavities
are machined into the tail of the penetrator for tracer or self- destruction mechanisms.
The cracks can cause premature fragmentation.
[0012] "Heavy alloys" are that class of two phase multi-component tungsten alloys containing
nickel and at least one other metal and in which one phase is essentially tungsten
and the other phase is a solid-solution of nickel, tungsten and the other metal or
metals. It has been found that the heavy alloys are suitable for forming the tail
component of a penetrator where a cavity is to be machined into the tail component.
These heavy alloys have a density of at least about 16.7 grams/cc, therefore these
alloys containing at least about 88% tungsten and the balance being nickel and other
metals such as copper, molybdenum, iron, titanium and the like. A particularly preferred
alloy is 97.3W-1.35Ni-1.35Fe.
[0013] The projectiles of the present invention have multiple components of different materials.
With particular reference to Fig, 1, a cross section of penetrator 10 is shown comprising
a body component 12, and a tail component 14 containing a tracer cavity 16. Nose component
18 is of the same material as the body component 12 and can be either fabricated in
one section comprising both the body component 12 and nose portion component 18 or
if desired the pieces can be fabricated separately and the nose component 18 can be
joined to one end of body component 12. The method of joining the components can be
brazing, inertial welding and the like. The tail component 14 is similarly joined
to the opposite end of body component 12. Frangible materials as indicated in claim
1 are used for the body portion 12 and nose component 18. Each of these materials
will penetrate the targets up to about 2" (5 cm) thick steel and will break into small
pieces upon exiting the target.
[0014] The tail portion is the heavy alloy as previously described having a density of at
least 16.7 grams/cc.
[0015] With particular reference to Fig. 2 a cross section of a penetrator 20 having three
segments is shown. Body component 22 is a frangible material. The nose component 24
is a tungsten base alloy such as 98W-2Ni, 97W-2.1 Ni-0.9Fe or 90W-10Mo. Tail component
26 is essentially identical to the tail portion of Fig. 1, that is, it is a machinable
heavy alloy. The penetrator 20 also contains a tracer cavity 28.
[0016] With particular reference to Fig. 3 there is provided a penetrator 30 having four
separate segments. Body component 32 is made of the aforementioned annealed tungsten
or tungsten containing 400 ppm of nickel. The tail component 34 and one section 36
of the nose component 38 are made of the machinable heavy alloy. A second section
40 extends from the first section 36 to serve as a windscreen and is a lighter weight
material such as aluminium or a ceramic material. The nose component 38 thus is comprised
of a first section 36 which is machined to enable attachment of the second section
40 which serves as a windscreen. The cavity 42 is shown in the tail component 34.
[0017] While there has been shown and described what are at present considered the preferred
embodiments of the invention, it will be obvious to those skilled in the art that
various changes and modifications may be made therein without departing from the scope
of the invention as defined by the appended claims.
1. A multiple component penetrator projectile (10, 20, 30) comprising a nose component
(18, 24, 38), a body component (12, 22, 32) and a tail component (14, 26, 34) joined
to one end of said body component, said body component consisting of a frangible tungsten
material selected from
tungsten alloys selected from the group consisting of 96% W-2% Ni; 97% W-2.1% Ni-0.9%
Fe; and 90% W-10% Mo, and
tungsten doped with about 400 parts per million of nickel,
said tail component (14, 26, 34) consisting of a machineable two-phase, multi-component
tungsten alloy containing nickel and at least one other metal and in which one phase
is essentially tungsten and the other phase is a solid solution of nickel, tungsten
and the other metal or metals, the density of said two-phase, multi-component tungsten
alloy being at least 16.7 grams/cm3.
2. A penetrator projectile according to claim 1, wherein said nose component (18,
24, 38) generally has a conical shape extending from the opposing end of the body
component (12, 22, 32), said nose component having the same composition as the body
component or consisting of a material different than said body component.
3. A penetrator projectile according to claim 2, wherein said nose component (18,24,38)
is comprised of a first section (36) and a second section (40), the first section
being a machinable tungsten portion joined to the end of the body component opposite
to the tail component and the second portion being a low density portion joined to
and extending from the first section and having a different composition than said
first section.
4. A penetrator projectile according to claim 3, wherein said second section (40)
is selected from aluminium and ceramics.
1. Mehrkomponenten-Wuchtgeschoß (10, 20, 30) mit einem Vorderteil (18, 24, 38), einem
Rumpfteil (12, 22, 32) und einem Heckteil (14, 26, 34), welches mit einem Ende des
Rumpfteiles verbunden ist, wobei das Rumpfteil aus einem zerbrechbaren Wolframmaterial
besteht, ausgewählt aus
Wolframlegierungen, ausgewählt aus der Gruppe bestehend aus 98 % W-2 % Ni; 97 % W-2,1
Ni-0,9 % Fe; und 90 % W-10 % Mo, und
Wolfram mit einer Dotierung von ungefähr 400 ppm Nickel,
und wobei dieses Heckteil (14, 26, 34) aus einer bearbeitbaren zweiphasigen, Mehrkomponenten-Wolframlegierung
besteht, umfassend Nickel und wenigstens ein weiteres Metall, und in welchem eine
Phase im wesentlichen Wolfram ist, und die andere Phase eine feste Lösung aus Nickel,
Wolfram und dem anderen Metall oder anderen Metallen, und wobei die Dichte dieser
zweiphasigen, Mehrkomponenten-Wolframlegierung wenigstens 16, 7 g/ccm beträgt.
2. Wuchtgeschoß nach Anspruch 1, wobei das Vorderteil (18, 24, 38), welches im wesentlichen
eine sich von dem gegenüberliegenden Ende des Rumpfteiles (12, 22, 32) aus erstreckende
konische Form aufweist, wobei das Vorderteil die gleiche Zusammensetzung wie das Rumpfteil
aufweist oder aus einem Material besteht, welches sich von dem Material des Rumpfteiles
unterscheidet.
3. Wuchtgeschoß nach Anspruch 2, wobei das Vorderteil (18, 24, 38) aus einem ersten
Bereich (36) und einem zweiten Bereich (40) besteht, wobei der erste Bereich ein maschinell
bearbeitbarer Wolframteil ist, welcher mit dem Ende des Rumpfteiles, welches dem Heckteil
gegenüberliegt, verbunden ist, und wobei der zweite Bereich ein Bereich geringerer
Dichte ist, welcher mit dem ersten Bereich verbunden ist und sich von diesem aus erstreckt
und eine von dem ersten Bereich unterschiedliche Zusammensetzung aufweist.
4. Wuchtgeschoß nach Anspruch 3, wobei derzweite Bereich (40) aus Aluminium oder Keramik
besteht.
1. Projectile perforant à parties multiples (10, 20, 30) comportant une partie avant
(18, 24, 38), une partie centrale (12, 22, 32) et une partie arrière (14, 26, 34)
fixée à une extrémité de la dite partie centrale, la dite partie centrale étant réalisée
dans un matériau au tungstène fragile choisi entre des alliages de tungstène choisis
dans le groupe comprenant 98% W - 2% Ni; 97% W - 2,1% Ni - 0,9% Fe; et 90% W - 10%
Mo, et du tungstène dope avec 400 parts environ par million de nickel, la dite partie
arrière (14, 26, 34) comprenant un alliage à base de tungstène usinable à parties
multiples a deux phases, contenant du nickel et au moins un autre métal et sans lequel
une phase est essentiellement du tungstène et l'autre phase est une solution solide
de nickel, tungstène et autre(s) métal ou métaux, la densité du dit alliage à base
de tungstène à parties multiples à deux phases étant au moins égal a 16.7 g/cm3.
2. Projectile perforant selon la revendication 1 dans lequel la dite partie avant
(18, 24, 38) présente généralement une forme conique faisant saillie de l'extrémité
opposée de la dite partie centrale (12, 22, 32), la dite partie avant ayant la même
composition que la partie centrale ou étant dans un matériau différent de celui de
la dite partie centrale.
3. Projectile perforant selon la revendication 2 dans lequel la dite partie avant
(18, 24, 38) comprend une première partie (36) et une seconde partie (40), la première
partie étant une partie en tungstène usinable fixée à l'extrémité de la partie centrale
du côté opposé à la partie arrière, et la seconde partie étant une partie de faible
densité fixée a et faisant saillie de la première partie et présentant une composition
différente de celle de la dite première partie.
4. Projectile perforant selon la revendication 3 dans lequel la dite second partie
(40) est réalisée soit en aluminium soit en céramique.
