Patent Application
20230116071
The invention relates to a sabot of a sub-caliber KE munition or of a sub-caliber KE penetrator. The invention relates in particular to a sabot consisting of several, at least two, preferably three, sabot segments. The sabot or the sabot segments are constructed such as to have a push-pull function. A part located in front of a pressure flange of the sabot accelerates the projectile by means of pressure, and a part located behind it accelerates the projectile by means of traction.
A sabot of a sub-caliber KE penetrator fulfills several functions. For example, the sabot must seal an annular gap remaining between the projectile and the tube wall of a weapon barrel, so that the propellant gases can be effectively used to drive the projectile. In addition, the sabot guides the projectile in the weapon barrel so that it follows towards the tube bore axis without lateral deflections and thus as precisely as possible. In the case of highly sub-calibered projectiles, the sabot must support the projectile during acceleration in the weapon barrel, whereby the force introduced into the projectile via the sabot is distributed over a larger area of the projectile length. In the case of a punctiform introduction of force under the effect of inertial forces, the projectile would otherwise collapse or tear off.
The sabot and the projectile separate after passing the muzzle. A terminal ballistic effect is produced solely by the projectile as a flying projectile. Detachment before the muzzle takes place due to the fact that the sabot consists of multiple parts. The sabot is divided into a plurality of segments which, starting from the tip, detach radially from the projectile as soon as they are no longer held together by the tube wall. The necessary driving force is generally generated by an air pocket which is exposed to the dynamic pressure by the ambient air.
In practice, there are pure push sabots or pure pull sabots. The pressure flange of the sabot is located either behind or in front of the actual sabot. In order to realize as low a sabot mass as possible, both push and/or pull sabots are shape-optimized. In addition, high-strength materials are used. As a result, the material is stressed to a high degree, as uniformly as possible.
DE 198 43 787 C1 discloses a sub-caliber KE projectile with a penetrator and a segmented central sabot, which comprises two supports arranged axially one behind the other. It is provided that a front and a rear air pocket are designed such that the dynamic pressure resulting during flight of the KE penetrator results in a common force application point. This common force application point should lie within a partial region in which a sleeve cover and a sabot are glued to one another and have a distance from a rear end of the sabot. This is intended to prevent the penetrator from oscillating.
A segmented sabot can also be gathered from DE 199 44 376 B4. It has a front first support and a second rear support arranged at an axial distance behind the first one. A releasable sabot for a sub-caliber projectile can be gathered from DE 103 20 194 A1. It has a plurality of sabot segments.
DE 10 2013 006 498 A1 discloses a sabot projectile which is characterized in that a narrow segmented steel disk is used as the guide element, which is connected in a form-fitting and/or force-fitting manner to a segmented, hollow cylindrical trim part made of plastic on the side facing the guide sabot. Typical for high-performance KE munitions are sabots in which a pressure flange lies approximately in the center of the elongated, arrow-like flying projectile. A part of the sabot lying in front of said pressure flange accelerates the projectile by means of pressure, and a part lying behind it accelerates the projectile by means of traction. In addition, a propellant pressure acts on the pull part, while the push part is free of external loads. Such sabots are also referred to as push-pull sabots.
The conventional push-pull sabots are designed to be very rigid on the rear of the sabot. This shortens the interaction time during detachment; however, because of this high rigidity, these sabots have a low damping effect. This results in lateral disturbances (detachment shocks) being transmitted directly onto the projectile during the detachment process. If this load is asymmetrical, an external transmission onto the flying projectile is problematic, as a result of which the projectile can be excited to oscillate.
DE 10 2019 125 128.1, which was not a prior document, relates to a sabot which is designed such as to have a push function, on the one hand, and a pull function, on the other, whereas these functions act or are present independently of one another. As a result of this design, there is a separation of the push and pull functions at the sabot. In order to separate the function, the sabot is divided or separated into sabot parts such that at least one sabot part takes over the pull function and at least one further sabot part takes over the push function. The sabot parts are in turn connected to a projectile by means of a positive connection. A positive connection between the sabot parts can be dispensed with, however. Preferably, the sabot parts are, however, mechanically separated from one another so that there is no positive connection between them. In that case, the sabot is a multi-part sabot. Alternatively, however, a mechanical connection between the sabot parts can be provided, whereby the sabot is a single-part sabot in case of a division of the functions. This reduces the mass of the sabot.
The object of the invention is to make the detachment process of a sabot smoother, such as to reduce an initial oscillation of the flying projectile.
The object is achieved by the features of claim 1. Preferred embodiments can be found in the dependent claims.
A segmented releasable sabot is known from DE 39 20 254 C2, which consists among other things of at least two sabot segments with adjacent plane-parallel segment separation surfaces. Here, there is a reference that, the lower the sabot mass and especially the lower the mass moment of inertia of the sabot segments about their rear rolling edge, the faster the detachment process and the lower the kinetic energy loss of the penetrator. To this end, the penetrator has a constriction with a rear rolling edge. The sabot segments are in turn provided with a corresponding shaping in this region.
The idea underlying the invention is to provide a sabot consisting of several segments. The sabot itself can consist of at least two, preferably three segments. More than three segments are also possible. These segments have a structural design at their rear ends opposite the shooting direction such that they are almost cylindrical and very thin in terms of wall thickness. In case of an ammunition in the caliber of for example 105 mm, this cylinder shape can be created within the last 20 mm to 30 mm of the sabot. The wall thickness can be approximately 3.5 mm to 4.5 mm. In case of an ammunition in a smaller caliber, the cylindrical region of the sabot is to be selected to be shorter and the wall thickness to be correspondingly smaller. In case of an ammunition in a larger caliber, the cylindrical region of the sabot should be longer and the wall thickness thicker. At these ends, the sabot or the sabot segments roll over the projectile during detachment.
These special ends have a low degree of flexural rigidity. Due to this flexibility, the ends designed in this way can reduce impulsive forces occurring between the sabot and the projectile. As a result, an additional rolling edge on the penetrator can be dispensed with during production while improving the detachment of the sabot or the sabot segments and the projectile or penetrator. The advantages resulting from this construction are, inter alia, that a lower initial oscillation is achieved and thus an optimization of the dispersion pattern.
The sabot or the sabot segments are moreover constructed such as to assume a push-pull function.
A sabot with a push-pull function comprising a plurality of sabot segments is proposed. The sabot or the sabot segments are characterized by having a structural design at an end opposite the shooting direction such that a low degree of flexural rigidity is achieved at said end. At this end, the sabot has a cylinder shape (a kind of tiny tail) which has a low degree of flexural rigidity such that impulsive forces are reduced and the sabot rolls off during detachment. A sabot with three sabot segments is preferred. The sabot or the sabot segments have a part located behind a pressure flange as a push part, and a part located in front of the pressure flange as a pull part. In order to optimize the shape and weight, the part located behind the pressure flange and the part located in front of the pressure flange have recesses. The recesses are introduced between braces, or braces remain between the recesses. The sabot or the sabot segments have pockets which are integrated in the part located behind the pressure flange.
The invention is to be explained in more detail with reference to an embodiment with a drawing.
The drawing shows:
In
The sabot 1 or the sabot segments 1.1, 1.2, 1.3 are characterized in that they are designed as a push-pull sabot or push-pull sabot segments. A part 3 of the sabot segments 1.1, 1.2, 1.3 (rear part) located behind a pressure flange 2 accelerates the sub-caliber projectile (not shown in greater detail) by means of pressure, and a part 4 (front part) located in front of the pressure flange 2 accelerates it by means of traction. In addition, a propellant pressure acts on the pull part 4, while the push part 3 is free of external loads.
The rear part 3 (push part) and the front part 4 (pull part) are in turn preferably optimized in terms of shape and weight. For this purpose, the front part 4 and the rear part 3 have recesses 5, 6 in the sabot segments 1.1, 1.2, 1.3. Braces 8, 9 remaining between these recesses serve to ensure sufficient rigidity of the sabot 1 or the sabot segments 1.1, 1.2, 1.3.
The sabot 1 or the sabot segments 1.1, 1.2, 1.3 have pockets 7 integrated in the rear part 3.
According to the invention, the sabot 1 or the sabot segments 1.1, 1.2, 1.3 have a structural design at an end 10 opposite the shooting direction such as to be very thin, as some kind of tiny tail. In case of an ammunition in the caliber of for example 105 mm, this cylinder shape (or tiny tail) can be created within the last 20 mm to 30 mm of the sabot 1 or the sabot segments 1.1, 1.2, 1.3. The wall thickness can be approximately 3.5 mm to 4.5 mm. As a result of this design, this special end 10 has a low degree of flexural rigidity. Due to this flexibility, impulsive forces occurring between the sabot 1 or the sabot segments 1.1, 1.2, 1.3 and the projectile or penetrator (not shown in greater detail) can be reduced. The homogenization of the detachment forces of all sabot segments 1.1, 1.2, 1.3 also reduces the initial oscillation of the projectile. A so-called detachment edge 11 is introduced between the sabot segments 1.1, 1.2, 1.3.
A receptacle of the projectile (not shown in greater detail) is denoted by 12. Projectile and sabot 1 are connected to one another via an indicated threaded connection.
The mode of operation is as follows:
As a result of the propellant gases, the sabot 1 or the sabot segments 1.1, 1.2, 1.3 together with the projectile are driven through a weapon barrel (not shown in greater detail). The weapon barrel is responsible for guiding the projectile in the weapon barrel. The sabot 1 and the projectile separate after passing the muzzle, and the sabot segments 1.1, 1.2, 1.3 separate after passing the muzzle. The necessary force is generated by the dynamic pressure in the pockets 7 of the sabot 1 or the sabot segments 1.1, 1.2, 1.3 when these pockets 7 are exposed to ambient air. The sabot 1 or the sabot segments 1.1, 1.2, 1.3 roll over the projectile during detachment. Due to the low flexural strength of the ends 10 of the sabot 1 or of the sabot segments 1.1, 1.2, 1.3, the detachment forces of the sabot 1, i.e., of all sabot segments 1.1, 1.2, 1.3, are homogenized.
| Number | Date | Country | Kind |
|---|---|---|---|
| 10 2020 115 703.7 | Jun 2020 | DE | national |
| Number | Date | Country | |
|---|---|---|---|
| Parent | PCT/EP2021/064791 | Jun 2021 | US |
| Child | 18081786 | US |
