Patent Grant
7063020
1. Field of the Invention
The technical scope of the invention is that of ammunition able to destroy targets heavily protected by a wall, for example of concrete.
2. Description of the Related Art
It is known, namely by U.S. Pat. No. 6,186,072 to define a piece of ammunition incorporating a perforating body whose inertia ensures its passage through thick protective walls. This ammunition encloses an explosive or incendiary charge that is ignited during perforation or after perforation of the wall.
The perforating body of this ammunition incorporates a solid insert embedded in the material forming the body.
This insert is made of a dense and mechanically strong alloy, chosen, for example among the refractory materials and their alloys (tungsten, tantalum, uranium).
The material forming the body is constituted by steel cast around an insert.
This ammunition has the drawback of being complicated to manufacture. It is firstly tricky and costly to produce a large diameter (over 90 mm), dense core which has high mechanical properties (density of over 13, limit of elasticity of over 1000 Mega Pascals) in a reproducible manner. Indeed, these materials are implemented in powder form using compression techniques.
Secondly, it is costly to cast a steel body around such a core, whose mechanical characteristics risk being deteriorated by the casting operation.
In fact, the material of the insert described in U.S. Pat. No. 6,186,072 fulfils only a ballast function and does not have any true perforating capacity.
It is the purpose of the invention to propose a perforating ammunition that does not suffer from such drawbacks.
Thus, the ammunition according to the invention is of an easier manufacture.
Moreover, the ammunition according to the invention enables the perforation of a concrete-armored target whatever the angle of impact on the target.
Thus, the invention relates to a perforating ammunition comprising a penetration body delimiting an internal cavity closed by a base, ammunition wherein the penetration body is made of a material having a limit of elasticity greater than or equal to 1200 Mega Pascals and incorporates a front nose comprising at least one insert integral with the nose, insert made of a material with high mechanical properties, denser than that of the body and arranged in a housing opening outside of the body.
According to a first embodiment of the invention, the inserts are organized into segments arranged radially around an axial extension of the body, such segments being made integral with the body by linking means.
The linking means may comprise at least one ring surrounding the inserts.
This perforating ammunition may also comprise a nose made of a dense alloy arranged at the end of the axial extension of the body and incorporating a rear surface pressing on the segments.
According to another embodiment of the invention, each insert may be constituted by a substantially cylindrical bar housed in a bore of the penetration body.
The perforating ammunition may thus comprise a single axial insert comprising a front nose extending the penetration body.
This ammunition may then comprise a propellant powder charge enabling the insert to be ejected out of the penetration body.
According to another embodiment, the ammunition may comprise at least one crown of bars evenly spaced around an axis of the penetration body.
It may thus comprise two crowns of bars evenly spaced around an axis of the penetration body.
The ends of the bars may be flush with an external surface of the penetration body.
The ends of the bars may, on the contrary, project out of the penetration body.
Each bar may have its axis inclined with respect to the axis of the penetration body.
The ends of the bars of a crown and another crown and/or an axial bar may lie substantially in the same plane.
The internal cavity may enclose at least one explosive charge.
The invention will become more apparent from the following description of the different embodiments, such description made with reference to the appended drawings, in which:
a and 1b show a first embodiment of a piece of ammunition according to the invention,
a, 4b and 4c show a fourth embodiment of a piece of ammunition according to the invention,
a and 5b show a variant of this fourth embodiment,
a and 6b show another variant of this fourth embodiment,
a and 7b show longitudinal sections of two other embodiments of the ammunition according to the invention.
With reference to
This ammunition may be an air-to-ground bomb or else a missile or a missile warhead. It will be of a diameter of over 100 mm and a length of around 1.5 m.
According to operational needs, it may comprise a rear part (not shown) incorporating a propellant imparting a given range and velocity to it.
It may also, where need be, comprise a guiding/piloting module.
The internal cavity 3 encloses an explosive charge 5 able to be ignited by a fuse 6 placed in the vicinity of the base 4. The fuse will be designed so as to ensure the detection of passage through a wall and then to ignite the explosive charge once passage has been made through this wall. Such fuses are well known to the Expert. Reference may be made, for example, to U.S. Pat. No. 5,255,608, which describes such a fuse.
The penetration body 2 comprises a front nose 2a extended by a rear cylindrical part 2b delimiting the internal cavity 3.
This body is made of a material with high mechanical properties, that is, a material whose limit of elasticity is greater than or equal to 1200 Mega Pascals. 35NCD16 type steel may be used, for example.
According to the invention, the front nose 2a comprises inserts 7 made of a denser material than that of the body 2. These inserts are made of a dense material with high mechanical properties. A material with a density of 17 or more having a limit of elasticity greater than or equal to 1000 Mega Pascals will be chosen. A tungsten alloy with a high limit of elasticity obtained by sintering may, for example, be used. The bars may also be made of depleted uranium or tantalum.
The inserts 7 are here in the form of segments arranged around a cylindrical axial extension 8 of the body 2.
Thus, each segment is in contact with the body 2, firstly at the axial extension 8 and secondly with a shoulder 9 of the body 2. The free space surrounding the axial extension 8 thus constitutes a housing for the inserts.
Each insert 7 is also in contact with two other adjacent inserts. The insert assembly thus forms the nose cone part of the front nose 2a of the penetration body 2.
The inserts 7 are made integral with the body by a linking means comprising at least one ring 10 surrounding the inserts 7. This ring will be made of steel. It will be housed in a groove 11 formed by the juxtaposition of notches on each insert.
The ammunition 1 also incorporates a nose 12 also made of a dense alloy. This nose is fastened at one end 14 of lesser diameter carried by the axial extension 8 of the body 2. The nose 12 comprises a rear surface 13 pressing on the inserts 7.
The nose 12 is fastened on end 14, for example, by threading. It enables the shock upon impacting a target to be transferred to the different inserts 7.
Thus, the ammunition according to the invention associates a nose cone of substantial diameter (over 90 mm) having a high perforating capability with a steel body whose only purpose is to carry the explosive charge and hold the perforating inserts together.
The inserts are reasonable in dimension (sections being of around 2000 mm2 to 6000 mm2) enabling them to be manufactured using sintering techniques already implemented for artillery fin-stabilized projectiles.
Thanks to the design of the ammunition according to the invention, it is also possible to improve a piece of ammunition after a phase in storage by replacing the inserts 7 initially provided by inserts having improved mechanical properties.
This embodiment differs from the previous one only in the structure of the front nose 2a.
Here, the front nose 2a comprises an axial bore 15 inside which an insert 7 is positioned that is in the form of a substantially cylindrical bar made of a denser material than that of the body 2.
The front nose 16 of this insert is cone-shaped that extends the penetration body 2.
This insert 7 will thus have a diameter of around 30 to 40 mm for a penetration body of a diameter of 90 mm. Its manufacture is thereby made easier. The implementation of a tungsten alloy with high mechanical properties (limit of elasticity greater than or equal to 1000 Mega Pascals) enables this nose to be given perforating properties rather than being used simply as ballast. The perforating capabilities of the ammunition are thus improved for a given mass.
The ammunition shown in.
This insert 7 comprises an internal cavity 17 inside which a propellant powder charge 18 is arranged.
A device 19 enabling the ignition of this charge is housed in the body 2. It is connected by a wire link 20 to the fuse 6.
The latter will then incorporate a timer module or a proximity detection module (connected to an antenna not shown integral with the nose cone of the body 2) which will enable the ignition of the propellant charge 18 to be triggered before impacting on a target and at a distance from said target of around 3 to 4 calibers.
The propellant charge 18 will ensure the ejection of the insert 7 out of the penetration body 2. It will thus be propelled towards the target. The speed differential between the insert 7 and the body 2 will be of around 200 m/s. Such an arrangement enables the perforation capabilities of the ammunition to be improved without necessarily increasing its velocity.
The insert will ensure the piercing of an initial hole in the target, the penetration body will then impact the target in this initial hole.
a, 4b and 4c show another embodiment of a perforating ammunition according to the invention.
This embodiment differs from the previous ones only in the structure of its perforating head 2a which here comprises several bars 7a, 7b, 7c crimped into bores arranged in the body of the nose 2a.
Each bar 7a, 7b, 7c is cylindrical and the axis of its bore is parallel to the axis 21 of the perforating head 2a.
Bars 7a and 7b are thus split into two concentric crowns surrounding the axis 21 of the perforating head. A bar 7c, moreover, occupies a bore coaxial to the head 2a (see also
Around the axial bar 7c there is thus a first crown or median crown comprising eight bars 7b evenly spaced around the axis 21 and a second crown or external crown comprising sixteen bars 7a evenly spaced around the axis 21.
The diameters of the peripheral bars 7a are here smaller than those of the median bars 7b. The diameters of the different bars may be identical or different according to the organization of the perforating head. The aim is to obtain the high global density for the perforating head. The diameters of the bars may be between 10 mm and 30 mm.
The ends of the different bars are machined such that they are flush with an external cone-shaped surface of the front nose 2a (see
Once again, the bars are made of a dense material, for example a tungsten alloy obtained by sintering. Because of the reduced diameter of the bars, a material having even higher mechanical properties may be adopted, for example a tungsten alloy whose limit of elasticity is greater than or equal to 1500 Mega Pascals. The body of the head 2a is made of steel.
This embodiment enables a front nose 2a with a high density to be easily obtained. It is, in fact, easier to produce dense bars of reduced diameter (of around 10 mm to 30 mm) than to produce a front nose of large diameter (over 150 mm) of such a sintered material.
Moreover, it would be tricky to manufacture an ammunition body 2 made entirely of sintered tungsten and comprising a solid front part connected to a thin rear part delimiting a cavity 3.
It is naturally possible for a different number and arrangement to be envisaged for the bars.
a and 5b show another embodiment which differs from the previous one only in the shape of the bars 7.
According to this embodiment, the ends of bars 7a and 7b protrude outside the penetration body 2. Each bar thus comprises a nose 22 extending out of the cone-shaped external surface of the front nose 2a.
This results in a higher engaging capacity of the front nose 2a during impact upon a target at an incidence.
The axes of bars 7a, 7b and 7c are, once again, all parallel with axis 21 of the ammunition.
a and 6b show another embodiment analogous to that of
Thus, the bars 7a of the external crown have an axis 23a inclined at an angle α of around 20° to 30°.
The bars 7b of the median crown have an axis 23b inclined at an angle β of around 10° to 15°.
This arrangement also makes it easier for the front nose 2a to engage the target during an impact at an incidence.
With respect to the previous embodiment, this embodiment improves the engagement capabilities without increasing the mass or diameter of the bars 7.
a shows another embodiment analogous to that of
Such an embodiment provides for the simultaneous embrittlement of the target at several points of impact. Perforation is thereby improved.
b shows an embodiment analogous to that of
The number of simultaneous points of impact on the target is thus multiplied.
It would naturally be possible to similarly prolong the inclined bars such as shown in
The ends of the bars of the external crown 7a and of the median crown 7b may be placed in the same plane whilst leaving the end of the bar 7c either retracted or protruding with respect to the crowns.
Other variants are also possible without departing from the scope of the invention.
It is thus possible for the embodiments in
A propellant charge may thus be provided enabling the axial bar 7c to be ejected before impact on the target. The other bars distributed on the crowns will remain fixed with respect to the front nose 2a.
The explosive charge 5 may also be replaced by a charge of a different nature, for example an incendiary charge or else one or several explosive and/or incendiary sub-munitions ejected after perforation of the target.
| Number | Name | Date | Kind |
|---|---|---|---|
| 3203349 | Schonberg | Aug 1965 | A |
| 3464356 | Wasserman et al. | Sep 1969 | A |
| 3731630 | Muller | May 1973 | A |
| 4108072 | Trinks et al. | Aug 1978 | A |
| 4573412 | Lovelace et al. | Mar 1986 | A |
| 4597333 | Bocker et al. | Jul 1986 | A |
| Number | Date | Country |
|---|---|---|
| 90 18 051 | May 1994 | DE |
| 2 771 496 | May 1999 | FR |
| Number | Date | Country | |
|---|---|---|---|
| 20050109233 A1 | May 2005 | US |
