The present invention relates to a method in firing artillery projectiles, such as various types of shells, from rifled barrels, for preventing the degree of wear of the barrel from which the projectiles are fired from having a negative effect on the muzzle velocity of the projectiles. The invention also encompasses a number of artillery projectiles or shells designed according to said method, and a method of manufacturing these.
When firing with modern ammunition containing propellant with a high energy content, the barrels from which the ammunition is fired are subject to very heavy wear, and long before the barrel wear has reached a level where the barrel ought to be rejected (reject stage) this wear has a detrimental effect on the muzzle velocity (Vo) of the projectiles fired from the barrel. The problem is well-known to engineers in the field and there are several different methods available for determining the barrel wear. According to one of these methods Δd25, the increase in diameter due to wear is determined in millimeters over the lands of the barrel rifling at a point 25 mm forward of the origin of the rifling, that is to say where the rifling commences, whilst another, older method relies on determining something called the “kontrisse displacement”, which involves determining the forward creep of the origin of the rifling in the barrel resulting from wear. The barrel lands are introduced with successively rising end faces inclined in relation to the axis of the barrel, and it is against these end faces that bands of the projectiles or shells must be rammed home in the actual loading operation, so that the bands in this so-called ram-home position afford an effective propellant gas obturation forward in the barrel. When the propellant charge of the projectile is then ignited, the propellant gases thereby formed behind the projectile will force the projectile forwards in the barrel under simultaneous deformation of the band, the angular twist of the barrel rifling imparting a rotation to the projectile. In conventional loading, however, the actual ram-home position of the projectiles is primarily defined by factors other than simply the position of the origin of the barrel rifling, and this applies especially in so-called cartridge ammunition, in which the case position defines the position of the cartridge and hence of the projectile in the barrel. In such cartridge ammunition the projectile and the cartridge case containing the propellant charge are in fact normally united with one another up to the point of firing, when the propellant gases formed by ignition of the propellant charge force the projectile out of the case. It is therefore primarily the position of the case in the loading or chamber position of the barrel which normally defines the overall position of the round in the barrel and because this case position is protected from the hot propellant gases by the cartridge case it will be subject to substantially less wear than the actual barrel.
The aforementioned measuring methods for determining the barrel wear therefore imply a determination of the barrel wear which most rapidly affects the muzzle velocity of the projectiles fired from the barrel, namely that which occurs at the actual origin of the rifling, that is to say in direct proximity to the ram-home position of said projectiles in the barrel for firing. Since the projectiles, as previously indicated, are when firing normally always rammed home in the same position in the barrel designed to bring the band of the shell into proper contact against the barrel rifling, that is to say the origin of the rifling, in a new barrel, the forward creep of the origin of the rifling in the barrel, that is to say away from the ram-home position of the projectiles, in fact means that in a worn barrel, in which the origin of the rifling has been shifted forwards in the barrel, i.e. away from the ram-home position, a gap will initially be formed between the band of the projectile and the inside of the barrel before the projectile has begun to move forwards in the barrel, which on firing of the propellant charge of the projectile results in a leaky ram-home position and a forward leakage of propellant gas past the band, which therefore in turn has a negative effect on the gas pressure behind the projectile, thereby resulting in a lower projectile muzzle velocity than intended. This gas leakage will obviously be sealed off as soon as the projectile begins to move forwards and its band reaches the new wear position for the origin of the rifling, but the gas leakage will still be so great that in a Bofors 40 mm automatic anti-aircraft gun using conventional projectiles or shells a reduction in the muzzle velocity Vo of approximately 3% or about 30 m/sec can already be expected after 700 rounds, despite use of the best possible wear protection additives of the titanium dioxide type. For the same gun firing armour-piercing shells, a 5% reduction in the Vo gives an 8% lower armour penetration.
The present invention now affords a solution to this problem in that it outlines a general principle for maintaining the design muzzle velocity (Vo) of a new barrel for a certain type of projectile or shell, even in a worn barrel. The invention can then in turn be divided up into a number of different methods for embodying this principle, some of which inherently means that limited modifications will have to be made to the projectiles or shells used in the application of the invention. These modifications, however, are not so comprehensive that they cannot be made both to exiting stocks of projectiles or shells and ones newly produced.
The invention is therefore characterized in that the obturation between the rifled inside of the barrel used in firing and the shell band on the projectile or shell thrust into the ram-home position in the barrel is rendered independent of the degree of wear of the barrel used for firing.
The basic principle behind the invention is therefore that the position of the band of the projectiles or shells, used in firing, in relation to the origin of the rifling, that is to say where the barrel rifling begins, must be rendered independent of the origin of the rifling in the barrel, the position of which varies according to the degree of barrel wear, and the obturation between the band of each projectile must thereby be completely sound even in heavily worn barrels.
A first method for fulfilling this basic principle means that the ram-home position in the barrel of the projectiles or shells used for firing is not fixed once and for all at the time the barrel is manufactured, as is normally the case, but is instead made to vary according to the actual position of the origin of the rifling in the barrel for each round fired. This means, therefore, that the ram-home position for the shells or projectiles is successively shifted forwards in the barrel according to its degree of wear. In purely practical terms this development of the invention means that the shells or projectiles are rammed home to the point of contact between the band of the projectile or shell and the origin of the rifling, which is independent of the origin of the rifling in the barrel, the position of which varies according to the degree of barrel wear.
If cartridge ammunition is then used for firing, that is to say ammunition in which the shell or the projectile is united during the loading sequence with a cartridge case containing the propellant charge, the elements will have to be rammed home with such force that the projectile or the shell is, if necessary, already detached from the cartridge case at the time of ramming home, that is to say before its propellant charge has been ignited, and the propellant charge is prevented from escaping in the barrel chamber position before it is ignited in that it comprises, for example, so-called multi-hole propellant manufactured in larger pieces or in that the constituent smaller particles of propellant are vacuum-packed. The requirement according to the invention is that the band of the shell or the projectile must already form effective obturation against the origin of the rifling before firing, whilst the case position of the charge casing in the barrel must be unchanged even in the case of a worn barrel. In the case of worn barrels, therefore, both the projectile and the cartridge case will already have separated from one another before the cartridge propellant was ignited. This is because, as stated previously, any degree of wear caused by the position of the cartridge in the barrel is of far less significance than the barrel wear and the axial creep of the origin of the rifling that varies according to this.
Effect can also be given to the basic idea behind the invention by firing shells or projectiles provided with slightly deformable bands, the position of which in a longitudinal direction has been adjusted in order to afford a perfect obturation against the origin of the rifling, even in heavily worn barrels and where the material of the band is so adjusted that when loading in slightly worn barrels the band is sufficiently deformed by the origin of the rifling to give the same ram-home position as in the case of the worn barrel.
According to this variant, therefore, the ram-home position of the individual projectile or shell in the barrel can be maintained unaltered regardless of the degree of barrel wear, whilst obtaining the desired obturation between the band of the shell or the projectile and the origin of the rifling in any worn state of the barrel.
According to a development of the variant of the invention above projectiles provided with a relatively lightly deformed forward band adapted to heavily worn barrels and a rear, more conventional band adapted to slightly worn barrels are used for firing in both worn and entirely new barrels. The idea behind this design is that in slightly worn barrels the forward band, when said projectile is actually rammed home, will be sufficiently deformed to allow the rear, more conventional band to assume a correct position relative to the origin of the rifling. Similarly, the forward band will assume the initial, direct obturation function in heavily worn barrels.
The next step in the development of the invention involves providing the projectiles or shells used for firing with bands which are displaceable in the longitudinal direction of each shell and the position of which in the longitudinal direction when ramming home the projectile or the shell in the barrel from which it is to be fired is adapted to a position that varies according to the degree of barrel wear. In shells with displaceable bands, the bands are therefore in the initial position in their longitudinally more forward position, following which the degree of barrel wear when ramming the shell home in the barrel adjusts the position of the moveable band to the degree of wear through direct contact between the moveable band and the origin of the rifling. In the case of a new barrel, therefore, the resistance of the band against the origin of the rifling will shift the band towards it rear position in the firing direction of the shell, whilst the band remains in its forward position in the case of heavily worn barrels. In the case of shells with moveable bands of the type characteristic of the invention, a perfect obturation is therefore always achieved against the origin of the rifling, regardless of the barrel wear.
A further development of the projectiles with displaceable band further means that their band is divided up into at least two different bands, at least one of which, arranged closest to the front end of the projectile or shell in its firing direction, is displaceable within a limited range in the longitudinal direction of the projectile. One of these two bands, therefore, the forward, displaceable band, will in its forward position serve for an adjustment to heavily worn barrels, whilst in its rear position together with the other band, the fixed band, it is adapted to less worn barrels.
This projectile variant having a displaceable forward band and a fixed rear band can then in turn be augmented by a ductile, that is to say plastically deformable, intermediate part, which whilst limiting the displacement of the movable band in slightly worn barrels also gives rise to an improved propellant gas obturation against the inside of the barrel. In a heavily worn barrel the ductile intermediate part at the same time ensures that the forward displaceable band maintains an obturation position as far forward as possible against the origin of the rifling. The ductile intermediate part might in turn be composed of a deformable copper or copper-nickel alloy or a heat-resistant plastic.
According to yet another variant of the invention, the band of the projectile or shell is given as entirely new design with a lip seal, which is angled rearwards in the firing direction of the projectile or the shell and is at least to some extent plastically deformable. This band design therefore differs radically from the plane, annular circumferential surface of the conventional band, which lies radially somewhat outside the actual circumferential surface of the projectile or shell, and which is virtually adapted to the inside of the barrel solely by dent of the fact that the barrel rifling lands break through the parts of the band situated outside the circumferential surface of the projectile. The new type of band now proposed having a lip seal, which is angled rearwards in the firing direction, provides a band which directly adjusts to barrels with differing degrees of wear, whilst the outer flank of the lip seal will afford the same deformability as the annular circumferential surface of the more conventional bands, in order to allow the lands of the barrel rifling to impart the helical twist of the rifling to the projectile in the form of its rotation, in just the same way as with conventional bands. A ductile pure copper or a suitable copper alloy having the same characteristics is proposed as a suitable material for the aforementioned lip seal. According to a further development of the invention, the rear-facing flanges of said lip seal in the firing direction of the projectile may be supported, for example, by a tubular support member in the shape, for example, of a deformable copper tube, which gives the lip seal a greater deformability in that this tubular component comprises an inner cavity giving it a substantially greater deformation area.
All aspects of the invention have now been defined in the following patent claims and will merely be described somewhat further with reference to the drawings attached, in which
a on a large scale shows the ringed part of
b on a large scale shows the ringed part of
a shows a detail of the shell according to
b shows a detail of the shell according to
a shows a detail of a further variant of the shell according to
b shows the same variant as 9a loaded in a worn barrel
a in cross section shows the function of an entirely new type of shell band in a new barrel
b in cross section shows the function of the band according to
In the drawings discussed below, some different parts appear in many or all figures and for practical reasons these have been given the same reference numerals in all figures regardless of the scale to which they are drawn in the various figures or how much can be seen of the part in question from the respective figure.
These reference numerals common to all figures are:
The shell 1 illustrated in
The shell 1 shown in
In
Referring now to
a and 9b the in turn illustrate a further variant of the band having a fixed band part 20 and moveable band part 19. A third band part 21 is then arranged between moveable band part 19 and the fixed band part 20. This third band part 21 is made from a ductile, plastically deformable material and its dual function is to ensure that the forward band part 19 affords a satisfactory gas-tight obturation against the inside of the barrel and through its own compression to further improve this gas-tight obturation, at all times regardless of the degree of wear of the particular barrel (5a, 5b) used for firing.
a and 10b further illustrate yet another development of the invention, according to which the outside diameter of the band 22 of the shell 1 has been made adjustable to both new and worn barrels. According to the invention this flexibility is achieved in that the band is designed with a lip seal 23, which is angled rearwards in the firing direction of the shell, whilst the band is entirely made of a material which is to some degree plastically deformable and sufficiently ductile when fired through the barrel to allow the lands of the barrel rifling to form grooves therein and to give the shell the desired rotation in its trajectory. As is shown in
The idea behind this variant of the invention is therefore that, when the shell is rammed home in the barrel, the worn position of the origin of the rifling will force the band 33 back along the splined grooves/the lands 34 to the position that best corresponds to the worn position of the barrel.
The fact that the band must be displaceable, but that a certain limited resistance should be required for this displacement, therefore represents an element of the invention.
The shell 26 shown in
The general method of producing banded, explosive shells by screwing two shell parts together, in which the band is first pressed onto one of the shell halves, represents a distinct simplification of the otherwise complicated fitting of the actual band. The method is therefore suitable for all types of shells that can be manufactured in two halves.
Number | Date | Country | Kind |
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0600554-0 | Mar 2006 | SE | national |
Filing Document | Filing Date | Country | Kind | 371c Date |
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PCT/SE2007/000145 | 2/19/2007 | WO | 00 | 2/19/2009 |