Patent Abstract:
A fuze for a projectile having a firing chain has an interrupter for interruption of the firing chain. The interrupter is configured to snap from a safe position to an armed position when unlocked. A locking device is disposed to lock the interrupter in the safe position and to unlock the interrupter by way of an unlocking movement. The fuze is rendered compact and reliable in that the unlocking movement of the locking device is an axial movement.

Full Description:
CROSS-REFERENCE TO RELATED APPLICATION 
     This application is a continuation, under 35 U.S.C. §120, of copending international application No. PCT/EP2009/007659, filed Oct. 27, 2009, which designated the United States; this application also claims the priority, under 35 U.S.C. §119, of German patent application No. DE 10 2008 053 990.2, filed Oct. 30, 2008; the prior applications are herewith incorporated by reference in their entirety. 
    
    
     BACKGROUND OF THE INVENTION 
     Field of the Invention 
     The invention relates to a fuze for a projectile having a firing chain and an interrupter for interruption of the firing chain. 
     Projectiles such as artillery projectiles, mortar shells or direct projectiles normally have a fuze with a firing chain which, in its armed position, comprises two or more firing charges arranged one behind the other. The last of these firing charges, the booster, directs its firing energy at a main charge, which is arranged in the projectile body of the projectile, in order to transmit firing energy to fire the main charge. 
     In order to interrupt the firing chain it is known from U.S. Pat. No. 4,691,634 for an interrupter to be provided which moves one of the firing charges such that they are not arranged directly one behind the other when in the safe state, such that this charge cannot be struck and, in addition, cannot transmit firing energy any further. In order to arm the fuze, this firing charge is moved by the interrupter such that the charges are arranged directly one behind the other, thus allowing the firing charges to be fired successively. 
     SUMMARY OF THE INVENTION 
     It is an object of the invention to provide a fuze for a projectile which overcome the above-mentioned disadvantages of the heretofore-known devices and methods of this general type and which provides for a reliable fuze for a projectile, which can be designed to be particularly compact. 
     With the foregoing and other objects in view there is provided, in accordance with the invention, a fuze for a projectile having a firing chain, comprising:
         an interrupter disposed for interruption of the firing chain;   the interrupter being configured to snap from a safe position to an armed position upon being unlocked; and   a locking device for locking the interrupter in the safe position and for unlocking the interrupter by an unlocking movement, the unlocking movement being an axial movement of said locking device.       

     In other words, the objects of the invention are achieved with an interrupter for interruption of the firing chain that is designed to snap from a safe position to an armed position when unlocked, and with a locking device, or locking means, for locking the interrupter in a safe position and for unlocking the interrupter by an unlocking movement which, in accordance with the invention, is an axial movement. 
     That is, the invention proposes that the unlocking movement of the locking device be an axial movement. An “axial movement” in this context is a movement that has a vector component in the axial direction. The axial direction is the intended flight direction of the projectile, which is also defined by the longitudinal axis of the device. The use of the axial direction for the unlocking movement allows the fuze to be designed to be very compact in the radial direction, and is therefore suitable for small-caliber projectiles. In particular, the axial movement is directed only in the axial direction, with respect to the interrupter. 
     The interrupter advantageously supports a firing charge which, when the firing chain is interrupted, that is to say in the safe position, is sufficiently far away from a following firing charge that relaying is impossible, that is, safely prevented. The snap-action of the interrupter to its armed position results in the interrupter moving digitally from its safe position to its armed position, such that transitions are avoided by the very rapid movement of the interrupter. This digital behavior of the interrupter and its position resulting from this either in the safe position or in the armed position, but not in an intermediate position, make it possible to achieve a high safety level. Furthermore, the fuze can be used both for fast and for slow projectiles, without special settings. The snap-action may be an unrestrained movement, which is braked to a minor extent only by friction losses. 
     In the armed position, the locking device expediently engages in a closed cutout in the interrupter, for example a hole through the interrupter, and in particular does not project beyond the interrupter in the radial direction. The locking means can therefore be considered to be mounted in the interrupter. A bolt which engages in a recess in the interrupter is particularly suitable. The interrupter is advantageously a rotor. The movement of the rotor from the safe position to the armed position is a rotary movement about a rotation axis. 
     The fuze is advantageously designed such that, before carrying out the unlocking movement, the interrupter first of all must be unlocked, controlled by the projectile firing process, before the unlocking movement can be carried out. For this purpose, the fuze advantageously has a means for unlocking the interrupter, controlled by the projectile firing process, in addition to the locking means for further unlocking. A double-bolt system is particularly suitable for unlocking controlled by the projectile firing process. During the unlocking process controlled by the projectile firing process, the interrupter, and in particular also the locking means, advantageously remains in a position which is unchanged axially with respect to a fuze housing. This allows a separation between firing charges to be kept short, thus making it easier to use insensitive firing explosive. 
     In order to reliably reach a safe arming distance, an escapement mechanism is advantageous in order to delay the unlocking movement of the locking means after the unlocking process controlled by the projectile firing process. The escapement mechanism may be designed in the form of a clock mechanism with an armature, and may have an element which can be moved from a locking position to a released position, in which the interrupter is released, or can be released by one or more further arming measures. This element is expediently a segment, in particular a tooth segment. A radial physical space can be kept small if the segment is arranged at least partially on or under the interrupter in the axial direction. On and under should be understood in the sense of above and below, with above being the nose of the projectile. 
     The axial physical space of the fuze can be kept compact if the locking means is mounted in the interrupter and, in particular, when in the safe position, engages in a recess in a component which is fixed to the housing, and, in the armed position, is moved out of the recess. The component which is fixed to the housing may be a cover or cover panel, and is expediently mounted such that it cannot move with respect to a housing of the fuze. The locking means is advantageously mounted in the interrupter both in the safe position and in the armed position, thus making it possible to keep the space required for the locking means small. The locking means expediently also carries out the snap-action movement. 
     In accordance with an added feature of the invention, the snap-action movement is be spring-powered. The snap action movement can be carried out with a particularly high safety level if it is powered by centrifugal force. The required centrifugal force can be produced by the projectile spinning during flight. 
     A particularly efficient unlocking procedure for the interrupter can be carried out if the locking means is held in its locking position by an escapement mechanism, expediently by a segment. The escapement mechanism can thus release the locking means as it unwinds, thus unlocking the rotor. In the unlocked state, the locking means is advantageously inserted into a recess in an escapement mechanism, in particular into a recess in a segment of the escapement mechanism. If the recess has a ramp, then the locking means can slide from its locking position to its released position. The locking means expediently slides into the recess. The ramp allows the locking means to be moved out of the recess, thus making it possible to achieve a high freedom of movement for the locking means and the interrupter. 
     In a further advantageous embodiment of the invention, an element, in particular a segment, of an escapement mechanism is designed to also carry out at least a part of the snap-action movement to the armed position with the interrupter. This makes it possible to ensure that the elements which carry out the snap-action movement have a high mass, which is useful for high reliability when carrying out the snap-action movement, particularly when this is a snap-action movement powered by centrifugal force. The joint snap-action movement of the interrupter can be coupled to the segment by the locking means. The joint movement expediently comprises the start of the snap-action movement, such that the segment can pull the interrupter out of a slightly blocked position, if the interrupter is jammed, as is possible after long storage. If the final part of the snap-action movement is carried out by the interrupter on its own and without the segment, the interrupter can carry out a long movement without having to move the segment as well, thus making it possible to achieve a compact movement procedure. 
     In a further advantageous embodiment of the invention, the fuze comprises a double-bolt system for arming when the projectile is fired. The projectile firing acceleration can be used as an arming force, without the interrupter carrying out an axial movement. Axial physical spaces can therefore be made particularly small and the firing charges in the firing chain can be fitted very close to one another, thus making it considerably easier to use insensitive explosive. 
     Furthermore, the fuze expediently comprises an opposing rotary spring in order to pull the interrupter in the direction of its safe position. This counteracts inadvertent movement of the interrupter from its safe position to its armed position, for example if the locking means is defective. 
     The interrupter is expediently locked in its armed position by the opposing rotary spring. This makes it possible to reduce the risk of an unexploded projectile. The double function of the opposing rotary spring makes it possible to save a further component, and to reduce the physical space. 
     A spiral spring is particularly suitable for use as the opposing rotary spring for a rotor. This can be integrated in a compact form in the fuze. The opposing rotary spring is expediently wound around a rotation axis of the interrupter, thus making it possible to design the fuze to be simple. For locking, the rotary spring advantageously engages in an element which is fixed to the housing. It is also good for compactness for the opposing rotary spring to be mounted completely within the interrupter, except for an engagement element for locking engagement. 
     Other features which are considered as characteristic for the invention are set forth in the appended claims. 
     Although the invention is illustrated and described herein as embodied in a fuze for a projectile, it is nevertheless not intended to be limited to the details shown, since various modifications and structural changes may be made therein without departing from the spirit of the invention and within the scope and range of equivalents of the claims. 
     The construction and method of operation of the invention, however, together with additional objects and advantages thereof will be best understood from the following description of specific embodiments when read in connection with the accompanying drawings. While the drawing illustrates one exemplary embodiment of the invention, the drawing and the description contain numerous features in combination, which those of skill in the pertinent art will expediently also consider individually and combine them to make further worthwhile combinations. 
    
    
     
       BRIEF DESCRIPTION OF THE SEVERAL VIEWS OF THE DRAWING 
         FIG. 1  is a partially broken, perspective view of a detail of a fuze of a projectile in the safe position; 
         FIG. 2  is a further partially sectioned perspective view of the detail of the fuze, with a cover fitted; 
         FIG. 3  is a plan view of the fuze in an intermediate position; 
         FIG. 4  is a section through the fuze, taken along the line IV-IV in  FIG. 3 ; and 
         FIG. 5  is a plan view of the fuze in its armed position. 
     
    
    
     DETAILED DESCRIPTION OF THE INVENTION 
     Referring now to the figures of the drawing in detail and first, particularly, to  FIG. 1  thereof, there is shown a partially sectioned perspective illustration of a part of a fuze  2  with a housing  4  which is intended to be attached in its lower area  6  to a body of a projectile. A part of the fuze  2  which is at the front in a direction of flight  8  of the projectile, or is the upper part in the view shown in the figures, has been omitted, in order to illustrate the elements shown in  FIG. 1  better and comprises an upper part of the housing  4 , an impact firing mechanism with a fuze needle for piercing a detonator  10 , and further elements. 
     The fuze  2  is provided with a double-bolt system  12  and with an escapement mechanism  14 , which is designed like a clock mechanism, with a toothed segment  16  and an interrupter  18 , which is arranged on the segment  16  and in which the detonator  10  is mounted. The interrupter  18  and the segment  16  are illustrated in partially sectioned form in  FIG. 1 . The detonator  10  is a part of a firing chain having at least two firing charges, specifically the detonator  10  and a booster, which is not illustrated but is arranged underneath the segment  16  on the center axis of the projectile or of the fuze  2 . 
       FIG. 1  shows the fuze  2  in its safe position. In this position, the detonator  10  is arranged separately from the booster and sufficiently far away from it that relaying to the subsequent booster is reliably prevented in the event of inadvertent detonation of the detonator  10 . An opening above the booster is covered by the segment  16 , and blocks a direct connection between the detonator  10  and the booster. In addition, the segment  16  blocks any movement of the interrupter  18  directly to its armed position, since an element of the interrupter  18 , specifically a depression  20  for holding the detonator  10 , would strike against an edge  22  (see  FIG. 5 ) of the segment  16  if the interrupter  18  were to move to its armed position, thus blocking further movement of the interrupter  18  to the center. 
       FIG. 2  shows a different, partially sectioned detail view of the fuze  2  with a cover panel  24  which is fixed to the housing fitted, likewise in the safe position. The interrupter  18  is shown in a sectioned form, thus providing a free view of an opposing rotary spring  26  and a locking means  28 , or locking device  28 , within the interrupter  18 . The opposing rotary spring  26  is a torsion spring in the form of a spring clip, one of whose limbs is held fixed to the housing in a gap in a shaft  30  about which the interrupter  18  is mounted such that it can rotate. The other limb is held in a slot  32 , as illustrated in  FIG. 1 , in the interrupter  18 , which is in the form of a rotor, and is prestressed torsionally, such that this limb loads the interrupter  18  with a counter-clockwise force, and in the opposite direction to the arming direction  34 . The rotor or interrupter  18  is thus pulled by the opposing rotary spring  26  in the direction of its safe position and is pushed against a stop  36 , which predetermines the safe position. 
     In addition, the interrupter  18  is held in its safe position by the double-bolt system  12  and the locking device or locking means  28 , which is in the form of a bolt. The locking means  28  engages in a conical recess  38  in the cover panel  24  which is fixed to the housing, and is held all round by the interrupter  18 , and is therefore mounted in it, such that the locking means  28  is fixed firmly in the interrupter  18  in the radial direction and tangential direction. In the axial direction, that is to say parallel to the direction of flight  8  but downward, the locking means  28  is blocked by the segment  16  of the escapement mechanism  14 , thus blocking a downward unlocking movement. The locking means  28  locks the interrupter  18  in its safe position by means of this blocking and the engagement in the recess  38  which is fixed to the housing, as well as the mounting in the interrupter  18 . 
     Before the projectile is fired, the components of the fuze  2  are as illustrated in  FIGS. 1 and 2 . In addition to the locking means  28  and the opposing rotary spring  26 , the interrupter  18  is blocked in its safe position by stop  40  on a bolt  42  of the double-bolt system  12 , on which one side  44  of the interrupter  18  rests. A further stop  46  on the bolt  42  blocks the segment  16  analogously in its locking position. 
     When the projectile is fired, powerful acceleration forces act in the direction of flight  8  on all the components of the fuze  2 . Because of their inertia, all the components are forced downward relative to the housing  4 , and in the opposite direction to the direction of flight  8 . Therefore, also the two bolts  42 ,  48  of the double-bolt system  12 , with the bolt  42  being mounted fixed to the housing by means of a ball  50  which engages in a recess  52  in the bolt  42 , and in the axial direction, that is to say parallel to the center axis  62 , which is illustrated in  FIG. 3 , of the fuze  2  and of the projectile. However, the bolt  48  can move freely axially and, driven by its inertia, compresses a spiral spring  54  downward on its way, which spiral spring  54  holds it at the top in its safe position when there is no acceleration on the fuze  2 . 
     During the downward movement of the bolt  48 , the bolt  42  is also forced downward and an incline, which is not illustrated, at the end of the recess  52  in it presses against the ball  50  and into this in the tangential direction against the bolt  48 , which blocks tangential movement of the ball  50 . However, as soon as the bolt  48  has been forced sufficiently far downward that a chamfer  56  comes into the area of the ball  50 , the ball  50  can escape in the tangential direction, and is forced out of the recess  52  by the chamfer on the bolt  42 . As soon as the ball  50  has emerged completely out of the recess  52 , the bolt  42  is also forced downward and its side  46  blocks the ball  50  in the area of the chamfer  56 , as a result of which the bolt  48  is blocked in its lower arming position and cannot be driven upward again by the spiral spring  54 . As a result of the release movement of the bolt  42 , this first of all allows the interrupter  18  to carry out an arming movement which, however, is blocked again by the locking means and, as the process continues, also a release movement of the segment  16 . As soon as the bolt  42  has been forced sufficiently far downward, a latching spring  58  springs into a recess  60 , which forms the stop  40 , in the bolt  42 , and locks this in its lower unlocking position. The unlocking movement of the double-bolt system  12  therefore unlocks the segment  16 , while the interrupter  18  is still locked by the locking means  28 . 
     As the projectile is fired, a spinning movement is impressed on the projectile, in the form of a rapid rotation about its centre axis  62 . This results in a powerful centrifugal force being exerted radially outward on all the elements of the fuze  2 . As can be seen from  FIG. 2  and  FIG. 3 , both the segment  16  and the interrupter  18  are mounted such that they can rotate about a rotation axis  64  within the shaft  30 . These figures also show that the center of gravity of the segment  16  is not located on this rotation axis  64  but well away from it, as a result of which the segment  16  is forced radially outward by the centrifugal force, and is thus forced to carry out a rotary movement in the clockwise direction about the rotation axis  64 . The tooth system  66  on the segment  16  exerts a force on gearwheels  68 ,  70  of the escapement mechanism  14 , which in turn act on an armature wheel  72  and an armature  74  of the escapement mechanism  14 . The armature  74  is moved in a reciprocating manner, analogously to a clock mechanism, and allows the armature wheel  72  to rotate in steps. This rotary movement is transmitted, stepped down, to the segment  16 , which rotates about the rotation axis  64  in the clockwise direction, or arming direction  34 . 
       FIG. 3  shows an intermediate position of the segment  16  between its locking position, as illustrated in  FIG. 1 , and its released position, as illustrated in  FIG. 5 . This intermediate position is illustrated in a partially sectioned form in  FIG. 4 . The rotary movement of the segment  16  moves a recess  76  toward the locking means  28  as far as a position as illustrated in  FIG. 4 . The locking means  28  is designed to be rounded at the bottom, that is to say toward the segment  16 , advantageously in the form of a ball cup, with this rounded shape sliding into the recess  76  as a result of further movement of the segment  16  on a ramp  78 . The movement of the locking means  28  in the axial direction is produced by the centrifugal force of the interrupter  18  in conjunction with the inclined surface of the conical recess  38 , since the center of gravity of the interrupter  18  is also not located on the rotation axis  64 , and the interrupter  18  is forced in the arming direction  34  by the centrifugal force. The locking means  28  is thus forced against the incline on the conical recess  38 , which forces it downward into the recess  76 . This unlocking movement, which takes place downward in the axial direction  80  relative to the interrupter  18  and is subject to additional lateral components relative to the housing  4  because of the lateral migration within the recess  38 , results in the interrupter  18  being unlocked as soon as the locking means  28  has emerged completely out of the recess  38 . 
     However, the interrupter  18  cannot snap immediately to an armed position on its own even in its state in which it has been unlocked by the locking means, because the interrupter  18  and the segment  16  are coupled by the locking means  28  during their further movement. The interrupter  18  and the segment  16  have to move relative to one another such that the locking means  28  remains within the recess  76 , since the cover panel  24  prevents it from moving upward and out of the segment  16 . As can be seen in  FIG. 3 , the tooth system  66  ends up approximately coincidently with the position in which the locking means  28  has emerged completely out of the recess  38 . This also ends the constriction of the release movement of the segment  16  by the escapement mechanism  14 , and this can snap essentially freely to its released position, driven by centrifugal forces, as is illustrated in  FIG. 5 . This snap-action movement can also be carried out by the interrupter  18 , as a result of which the segment  16  and the interrupter  18  synchronously move through the first part of the snap-action movement of the interrupter  18 . In the situation in which the interrupter  18  is not moved out of its safe position for any inadvertent reason, for example because a critical element has corroded such that it is fixed, then a stop surface  82  on the recess  76  strikes against the locking means  28  and thus forces the interrupter  18  out of its safe position. The interrupter  18  is released from, for example, the seized position, and itself starts to carry out its arming movement in the direction of the armed position. This results in a high degree of reliability against unexploded projectiles. 
     Once the segment  16  has reached its released position, and has partially accommodated the locking means  28 , the segment  26  and the interrupter  18  and, with it, the locking means  28 , carry out the first part of the snap-action movement of the interrupter together, until the segment  16  strikes against a surface  84  of the housing  4 . The segment  16  has reached its final position while, in contrast, the interrupter  18  continues to carry out its snap-action movement. The locking means  28  is in this way guided onto the ramp  78  again, and is pulled out of the recess  76 , with the locking means  28  entering a recess  86  (see  FIG. 2 ) in the cover panel  24 . The recess  86  makes it possible to decouple the movement of the interrupter  18  from the movement of the segment  16 . The interrupter  18  carries out its snap-action movement essentially without impediment, as far as the armed position illustrated in  FIG. 5 . 
     On reaching this armed position, the interrupter  18  strikes against the stop  36 , which therefore predetermines the armed position. The stop  36  is a depression in the cover panel  24 , and is therefore fixed to the housing. In this position, a tab  88  (see  FIGS. 1 and 2 ) on the opposing rotary spring  26  latches into a recess  90  in the cover panel  24 , and thus locks the interrupter  18  in its armed position. The detonator  10  is now on the center axis  62  of the projectile and is arranged in line with the booster, which is located underneath it, thus allowing relaying to take place from the detonator  10  to the booster. The interrupter  18  or rotor, and therefore the fuze  2 , are in their armed position.

Technology Classification (CPC): 5