GB2248914A - Self-loading hand weapon - Google Patents

Self-loading hand weapon Download PDF

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Publication number
GB2248914A
GB2248914A GB8312455A GB8312455A GB2248914A GB 2248914 A GB2248914 A GB 2248914A GB 8312455 A GB8312455 A GB 8312455A GB 8312455 A GB8312455 A GB 8312455A GB 2248914 A GB2248914 A GB 2248914A
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United Kingdom
Prior art keywords
firing
weapon
pin
lever
breechblock
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Granted
Application number
GB8312455A
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GB2248914B (en
Inventor
Horst Jakubaschk
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Heckler und Koch GmbH
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Heckler und Koch GmbH
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Publication of GB2248914A publication Critical patent/GB2248914A/en
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Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41WEAPONS
    • F41AFUNCTIONAL FEATURES OR DETAILS COMMON TO BOTH SMALLARMS AND ORDNANCE, e.g. CANNONS; MOUNTINGS FOR SMALLARMS OR ORDNANCE
    • F41A3/00Breech mechanisms, e.g. locks
    • F41A3/64Mounting of breech-blocks; Accessories for breech-blocks or breech-block mountings
    • F41A3/72Operating handles or levers; Mounting thereof in breech-blocks or bolts

Abstract

A self-loading hand weapon, preferably a rifle, with a locking means exhibiting a lever for locking a movable weapon part as a function of the position of another weapon part is characterized by the fact that the lever is a double-arm lever which, with one of its arms, is basically constantly in contact with the movable weapon part and, with its other arm, is in contact with the other weapon part. Consequently, no springs are required for positioning the lever. As shown in Figure 8, the lever 114 is controlled by a cam 54 and serves to lock the rotary breechblock 4 in the appropriate position. In another section of the weapon (Figure 10, not shown) a double-arm lever (135) controlled by a cam (56) serves to lock the firing hammer (66) in the cocked position. <IMAGE>

Description

2243.)14 4 Self-loading hand weapon The invention relates to a
self-loading hand weapon, preferably a rifle, with a locking means exhibiting a lever for locking a movable weapon part as a function of the position of another weapon part. Such locking means are known in various forms. For example, in an automatic rifle the firing hammer which has been recocked after the firing of a round has to be held in its cocked position by a locking means until the breech is again completely closed. Only now is the firing hammer released and then, in automatic mode, immediately strikes again, causing the round to be fired, or if the weapon is set to single fire, it is then possible for the firer to fire the next round by pulling the trigger. In known means of this type the lever is in the form of a singlearm lever which is actuated by a further single-arm lever which is in contact with the breechblock. The two aforementioned levers are connected by springs which ensure that the levers are in contact with each other and that the last-mentioned lever is in contact with the breechblock.
v With such springs there is always the danger that they will break, as a result of which the weapon is rendered unserviceable.
The object of the invention is to create a weapon of the initially depicted kind in which springs are not required for the aforementioned locking means. The object of the invention is achieved in that the lever is a double-arm lever which, with one of its arms, is basically constantly in contact with the movable weapon part and, with its other arm, is in contact with the other weapon part.
1 0 The advantage of the invention is that the lever is forced in its position by the two weapon parts such that, even without the presence of a spring, the position of the lever is always defined with sufficient accuracy either to lock or to release the weapon part which is to be locked. An important advantage of the invention is tha t owing to the absence of springs in the locking means the motions which have to be executed can be performed at virtually any operating speeds. By contrast, arrangements with springs are generally only fully operative within a restricted range of the operating speed, and the operating speeds achievable with springs are limited to maximum values because the spring must also accelerate its own mass when extending.
In particular, the movable weapon part which is to be locked and released may be a firing hammer of the weapon. The movable weapon part may also 4 be a breechblock, in particular a basically cylindrical breechblock of the weapon containing a cartridge chamber and being disposed such that it can pivot in a part of the weapon which is rigid with the barrel. A weapon with such a breechblock is known from DE OS 28 13 633. This breechblock must assume precisely defined positions for loading a cartridge and for firing a round. In one and the same weapon it is possible to provide locking means according to the invention both for the firing hammer as well as for the breechblock whereby it goes without saying that in this case two double-arm levers must be provided which, in turn, interact with an appropriate other weapon part. However, according to an embodiment of the invention, these two other weapon parts may be coaxial and rigidly connected to each other so that they perform their pivoting or rotating motion in complete synchronism with each other. In this case, these two "other weapon parts" may be formed by two control cams of a single weapon element which are disposed in different planes parallel to each other.
0 In an embodiment of the invention the other weapon part which may also be termed the part controlling the locking means may be guided such that it is basically linearly displaceable. It may, in particular, be a linearly displaceable breechblock. In another embodiment of the invention the other weapon part is mounted such that it can rotate or pivot. The term "pivot" should be understood in this connection to mean that the part which is capable of pivoting may well also be continuously pivoted in the same direction of rotation.
In other embodiments the weapon part which is locked by the locking means may be a breechblock.
In an embodiment of the invention the pivot axis of the double-arm lever is disposed such that the moments acting on the lever try to lift each lever arm off the moving weapon part and off the other weapon part as the latter moves. When the weapon parts in contact with the arms of the lever move, owing to their curved shape they transmit moments which try to lift the corresponding. lever arm off the weapon part which is in contact with it. Consequently, the friction and the wear between the contacting parts is reduced and, thus, the means is suitable in particular also for very high firing rates.
1

Claims (12)

  1. The embodiment of the invention described in Claim 7 has the advantage
    that the quick releasing and locking of the firing hammer is possible.
    The embodiment of the invention described in Claim 8 is characterized by the fact that the locking of the breechblock in the firing position and in the loading position can reliably take place within a very short space of time, whereas known locking cams which are disposed on the switch- wheel and which come into engagement with the star wheel of the Geneva gear are not able to lock the breechblock within such a short space of time.
    Specimen embodiments of the invention are described and explained below with reference to the drawings in which:
    Fig. 1 is a side view, partially broken off, of the parts of an automatic rifle which are important-with regard to the invention; Fig.
  2. 2 is a top view in the direction of arrow II in Fig. 1; Fig.
  3. 3 is a front view in the direction of arrow III in Fig. 1; Fig. 4 is a rear view in the direction of arrow IV in Fig. 2; Fig. 5 is a section on line V-V in Fig. 2; Fig. 6 is a section on line VI-VI in Fig. 2; Fig. 7 is a section on line VII-VII in Fig. 2; Fig. 8 is a section on line VIII-VIII in Fig. 2, turned through 18C; Fig. 9 is a longitudinal section through the receiver with the cylindrical breechblock, turned through 1800 and thus in the same orientation as shown in Fig. 8; Fig. 10 is a section on line IX-IX in Fig. 2, likewise turned through 18C; Fig. 11 is a graphic representation; Fig. 12 is a side view corresponding to Fig. 8, but partially in section and broken off; Fig. 13 is a view of the firing pin in the direction of arrow XIII in Fig. 12, broken off; Fig. 14 is a detail of a modif ied embodiment; Fig. 15 is a side view of the firing pin; Fig. 16 is a view of the firing pin in the direction of arrow XVI in Fig. 15; Fig. 17 is a section on line XVI1-XVII in Fig. 15; Fig. 18 to 20 are details of the movable dog and of a guide pin of a coulisse; Fig. 21a to f are the operating principle of the coulisse.
    Fig. 3 is enlarged in comparison with Fig. 1 and 4 to 8.
    Fig. 2 is enlarged by a factor of 1.17 in comparison with Fig. 1 and 3 to 7.
    The embodiment shown in the drawings is an automatic rifle suita,ble for firing caseless cartridges.
    As shown in Fig. 9, a part 2 which is rigidly connected to a barrel 1 contains a cylindrical hole 3 whose axis 31 is perpendicular to the barrel axis and intersects the barrel axis. Mounted in this hole 3 is a cylindrical breechblock 4 which is rotatable about the axis 31 of the hole 3. The drawing shows this breechblock in the firing position. In this firing position a cartridge chamber 9 in the breechblock 4 aligns with the bore 5 of the barrel 1. The cartridge chamber 9 is symmetrical with respect to a transverse centre plane of the rifle on which the axis of the barrel 1 is perpendicular and in which the axis of the breechblock 4 lies. A caseless cartridge 14 in the cartridge chamber 9 consists of a propellant body 8 with projectile 7 projecting at the front. on either side of the aforementioned transverse centre plane the cartridge chamber 9 which has an approximately rectangular clear cross section exhibits stop faces 10 which project into the clear cross section and which come into contact with corresponding counter-faces 11 of the propellant body 8, thereby fixing the position of the cartridge 14 in the cartridge chamber 9. The cartridge 14 shown in Fig. 9 is supported on two diagonally opposite stop faces 10, and the propellant body 8 is recessed in a (in Fig. 9) lefthand end region in the region of the other two diagonally opposite corners in such a way that these recesses accommodate the stop faces (not shown in Fig. 9) for a cartridge which is introduced into the cartridge chamber in the opposite direction, i.e. whose projectile would then point to the right, with the result that the cartridge shown in Fig. 9 is not hindered from assuming its shown position.
    On the side of the hole 3 opposite the barrel 1 a firing pin 21 is mounted in a hole 22 of an insert 23 (Fig. 12) which is inserted into the part 2, and the longitudinal axis of the firing pin 21 aligns with the bore of the barrel 1. The firing pin 21 is provided with a stop shoulder 24 on its side facing away from the breechblock 4. The stop shoulder 24 comes up against a stop face 25 of the insert 23 after the propellant body of the cartridge has ignited. The contact of the stop shoulder 24 on the aforementioned stop face creates a seal which largely prevents the escape of combustion gases. The firing pin 21 is normally in the position shown in Fig. 1 in which its front end which acts on a detonating compound of the cartridge when firing is not penetrating the hole 3. This is also the case even when, with the weapon uncocked, the firing hammer 66 is up against the firing pin 21. To ignite a cartridge, the firing pin 21 is struck to the front, i.e. to the left in Fig. 1, by the firing hammer 66.
    To load the weapon after firing a round, the breechblock 4 is turned through 900 in a clockwise direction in Fig. 9 (in an anticlockwise direction in Fig. 7) so that the cartridge chamber 9 is perpendicular to the axis of the bore 5 and one of the open ends of the cartridge chamber is facing upwards towards a magazine 31 which is disposed above the barrel 1 of the weapon and extends parallel to said barrel. This magazine 31 is a bar magazine in which the cartridges 14 are arranged such that they are perpendicular to the direction of fire and the tips 33 of the projectiles 7 point towards the barrel axis. The cartridge 14 which is in first place in the magazine (last place when viewed in the direction of fire) aligns with the cartridge chamber 9 in the breechblock 4 when the latter is in the loading position. A shaft 12 is machined into the part 2 on the side opposite the magazine 31. In the other figures the cartridges 14 are shown in a somewhat simplified representation. Fig. 9 differs in scale somewhat from the other figures; Fig. 9 itself is not strictly to scale. In the other figures the part 2 has, in places where it would obstruct clarity, been partially omitted entirely, and partially only indicated by a few outlines.
    A Geneva gear is used, among other things, to drive the breechblock 4. This Geneva gear comprises grooves 35 which are worked into the end face of the cylindrical breechblock 4 facing the observer in Fig. 7; there are four such grooves 35 which are disposed radially,separated by an angle of 900 from each other and which run into the outer cylindrical surface.
    Mounted in the part 2 at an angle of 45' to the right below the rotation axis 3' of the breechblock 4 as viewed in Fig. 7, and outside the hole 3, but closely juxtaposed to it, is a shaft 40 whose rotation axis runs parallel to the rotation axis 5' of the breechblock 4. Beginning at the right-hand outer end, i.e. from the side facing the observer in Fig. 1, the following parts are mounted on the shaft 40 such that they cannot turn:
    A flat circular disc 42 which is mounted coaxially on the shaft 40 (Fig. 1); in the viewing direction of Fig. 1 behind the circular disc 42 a first constant diameter cam 44 which deviates only slightly from a circular form and exhibits only a slight eccentricity in relation to the shaft 40, see Fig. 5. Behind the first constant diameter cam 44 there is a second constant diameter cam 46, see Fig. 6, which basically has the form of a circular disc, but which is mounted on the shaft 40 such that it is relatively eccentric, namely at about the centre between its centrepoint and its outer limit.
    Behind the second constant diameter cam 46 there is a circular disc 48 which is coaxial with the shaft 40 and which can only be clearly seen in Fig. 2 and which bears on its rear side two pins 50 and 51 intended for engaging the grooves 35, see Fig. 2 and 7. In the firing position shown in all figures with the firing hammer cocked and retained by the sear, the pins 50 and 51 are outside the grooves 35. The pins 50 and 51 are at an equal distance from the axis of the shaft 40, but they are not exactly diametrically opposed, but form together an angle of about 145' which is open towards the breechblock 4 whereby the pins 50 and 51 are at an equal distance from the rotation axis of the breechblock 4. They are at a distance away from the outer ends of the grooves 35 which are nearest to them and point downwards and towards the right respectively in Fig. 7. The circular disc 48 with the pins 50 and 51 is in close proximity to the parallel side wall of the part 2. The shaft 40 penetrates the part 2, and at its end region which projects beyond the side face of the part 2 facing away from the observer in Fig. 1, said side face being at the top in Fig. 2 and facing the observer in Fig. 4, the shaft 40 bears, as shown in Fig. 2 in a direction from bottom to top and once again rigidly connected to it, first of all a control disc 54 (Fig. 2) for indirectly locking the breechblock, followed by a disc 56 whose edge forms a release cam, and a circular disc which is coaxially connected to the shaft 40 and which, on its outward-pointing side visible in Fig. 4, bears a projection 59 which interacts with a spring-mounted dog 230 (which is formed by a leaf spring) of a knob 175 which is coaxial with the circular disc 58 and is disposed in Fig.
  4. 4 in front of the disc 58, said interaction taking place such that the user of the weapon can, by turning the knob 175 in an anticlockwise direction as viewed in Fig. 4, turn the circular disc 58 and thus the shaft 40.
    This knob 175 is made slightly stiff so that it is not turned when, during normal operation of the breech which is still to be described, the shaft 40 turns in an anticlockwise direction as viewed in Fig. 4. If, on the other hand, this knob is made to turn easily, then it can also be turned during the rotational movement of the shaft 40, but it is subjected only to an extremely low torque with the result that the rotating of this knob, for example in the case of continuous fire, does not represent any danger to the firer. The knob 175 may, in particular, be mounted such that it latches.
    The above-described parts rigidly connected to the shaft 40 as well as the shaft 40 itself together form a rotating gyrating mass or a flywheel which makes it possible to store kinetic energy in this flywheel, said energy then being delivered from the flywheel to carry out the loading operation. In particular, this flywheel is suitable for storing kinetic energy which is supplied to it over a relatively short space of time and for retransmitting the energy over a relatively long space of time.
    The weapon in the specimen embodiment is a gas-operated weapon whose gas piston (not shown) acts on the (in Fig. 1) right-hand end of a control rod 60. Immediately after a round has been fired the gas pressure forces the control rod 60 to the left as viewed in Fig. 1. The control rod 60 is mounted on the circular disc 42 by means of a joint 61 which is also engaged by a link 62. In the firing position shown in Fig. 1, this joint 61 is not at top dead centre, but about 30' from it in a clockwise direction. Therefore, as a result of the gas pressure the movement of the control rod 60 means inevitably that the circular disc 42 and with it the shaft 40 together with all parts attached thereto are set in rotation, said rotation, as viewed in Fig. 1, taking place in a clockwise direction. The arrangement is such that the gas drive for the control rod 60 is finished before the joint 61 has reached bottom dead centre, i.e. basically that position in which the control rod 60 has moved furthest downwards (in relation to the direction of fire). As soon as the gas pressure ends there is no external drive for the flywheel arrangement formed by the shaft 40 and the parts connected to it; however, as a result of the kinetic energy stored in this flywheel arrangement it continues to turn in a clockwise direction as viewed in Fig. 1 at least until the joint 61 has again assumed the position shown in Fig. 1.
    The free end of the long lever arm of a cocking means 65 is connected to the joint 64 of the link 62 facing away from the link 61. The purpose of the cocking means 65 is as follows: The firing hammer 66 of the weapon shown in its, cocked state in Fig. 1 must, after it has performed its striking action during which it moves in a clockwise direction as viewed in Fig. 1, be brought by the cocking means 65 back into the cocked position through an anticlockwise pivoting movement against the force of the firing spring 67 which is in the form of a spiral spring. The firing hammer 66 is held in the cocked position with the weapon ready to fire by a catch 68 of a trigger lever 70 which is pivot-mounted about a barrel-rigid pivot pin 69 and which engages a notch 72. Connected to the trigger lever 70 at a joint 73 is a trigger bar 74 which, when it is moved forwards, swings the catch 68 downwards out of the region of the notch 72, thus allowing the firing hammer 66 to strike. The weapon is, as far as it is shown, set up merely for continuous firing. Continuous fire is ended when the trigger bar 74 is moved to the rear again so that the firing hammer 66 is once again caught by the catch 68. of course, it may also be convenient to design the weapon for firing individual rounds and short bursts of fire with a defined number of rounds; such measures are known and do not relate to the present invention. The trigger bar 74 is connected to a trigger to be actuated by the firer. This connection is not shown.
    The cocking means 65 is mounted on a pivot pin 75 which runs parallel to the shaft 40 and is held in the part 2, and this pivot pin 75 also serves for the pivot mounting of the firing hammer 66. The cocking means 65 consists basically of an approximately U-shaped metal part, both legs of which 265 and 267 are connected by a yoke 270 which can be seen in section in the partially broken-off Fig. 1. The leg 267 is in close contact with the directly adjacent leg 78 of the firing hammer 66 and exhibits two ring-segment-shaped, axially symmetrical recesses 272 which are engaged by two projections 274 which are integral with the leg 78 of the firing hammer 66. The width of the projections 274 in the circumferential direction is smaller than the angle of the recesses 272; more specifically, the angle of the recesses 272 is about 900 greater than the width of the projections 274, measured in degrees. The angle of the recesses 272 is, thus, so great that the edge of these recesses does not come into contact with the projections on the cocking means 65 when the cocking means 65, after cocking the firing hammer, has again reached the position shown in Fig. 1 and the firing hammer 66 now strikes. The cocking of the firing hammer 66 against the force of the firing spring 67 begins when, starting from the position shown in Fig. 1, the circular disc 42 has covered only a few degrees and, as shown in Fig. 11, the circular disc 42 is still in the acceleration phase. Thus, no sudden shock will act via the link 62 on the flywheel arrangement. There is also a certain reduction of the acceleration imparted to the cocking means 65 through the braking force exerted on the control rod 60 by the flywheel as its accelerates. This reduces the occurrence of heavy shock-like loading.
    In the specimen embodiment, the gas pressure ends approximately at the same time as the firing hammer 66 is cocked. At this time the breechblock 4 has, as will be described later, also been turned through 90' in a clockwise direction as viewed in Fig. 7. The energy for this rotational movement of the breechblock 4 is taken directly from the gas pressure moving the control rod 60. The operations which, after completion of the cocking of the firing hammer 66, still have to be performed before the weapon is again ready to fire or, in the case of continuous fire, until the next round can be fired automatically are, however, performed exclusively by the kinetic energy stored in the flywheel arrangement after the gas pressure has ended.
    At the rear end region of the control rod 60 which is formed by a plate there is in close proximity to the joint 61 a diagonally downward projecting lug 80 which, immediately before the circular disc 42 reaches the position shown in Fig. 1, comes into contact with a lug 81 of a locking lever 82 and pivots the latter against the force of a spiral spring 83 in an anticlockwise direction as viewed in Fig. 1 so that a longer lever arm 84 of the locking lever 82 is swung into the path of.a non-undercut stop face 85 on the control rod 60, thereby preventing a further movement of the control rod 60 to the left, thus ending the rotation of the flywheel arrangement. As soon as the movement of the control rod 60 to the left has come to rest and, therefore, no more force is acting on the front end of the long lever arm 84, the locking lever 82 is pivoted back again into the position shown in Fig. 1 by the spiral spring 83 and the weapon is now ready to fire the next round.
    The locking lever 82 is pivot-mounted on a hinge pin 86 mounted in the part 2, whereby likewise pivot-mounted on said hinge pin directly behind the locking lever 82 in Fig. 1 is a first control plate 88, see also Fig. 5, which has a large hook-shaped cutout 89 wherebytwo parallel side faces 90 and 91 of this cutout 89 are separated by a distance equal to the diameter of the first constant diameter cam 44. When the first constant diameter cam 44 rotates the first control plate 88 is thus pivoted slightly about the hing pin 86. Pivot-mounted on a pivot shaft 93 in an area above the hinge pin 86 and slightly more forward in the direction of fire is a second control plate 95 which is immediately behind the first control plate 88 in the viewing direction of Fig. 1 and 5 and which exhibits a recess 96 in the form of a relatively short slot with two parallel side faces 97 and 98 which are directed slightly downwards from the horizontal towards the front, and the second constant diameter cam 46 is disposed in the recess 96, its diameter being equal to the distance between the faces 97 and 98. The rear end 94 of the second control plate 95 is attached approximately in the middle area of a bell crank 99 by means of a pivot shaft 100. Pivotmounted in the lower end region of the bell crank 99 on a joint 101 is a link 102 whose front turning joint is formed by a hinge pin 103 which is rigid with the barrel and is disposed in the part 2. The hinge pin 103 is slightly lower than the hinge pin 101. The link 102 has an upward sweep in order.to leave room for the cocking means 65. When the two constant diameter cams 44 and 46 rotate the front upper free end 105 of the bell crank 99 performs a coupling motion whose path corresponds approximately to the curve 106 shown in Fig. 6, and during the execution of such a motion the end 105 of the bell crank 99 pushes a cartridge from the magazine 31 into the cartridge chamber which in this instant is in a position turned through 900 with respect to Fig. 9.
    If the weapon is to be equipped with a rounds counter for bursts of fire of, for example, three rounds each, then A three-tooth switch-wheel 108 can be pivot-mounted about the stationary hinge pin 103 of the link 102, and this switch-wheel 108 is switched one step further by a lug 109 on the second control plate 95 on each upwards movement of the second control plate 95. As already mentioned, the provision of a rounds counter is nota subject of the present invention.
    As can be seen from Fig. 7, starting from the position shown in Fig. 1, the shaft 40 first of all performs a rotation through about 150 in a clockwise direction until the pin 50 comes into engagement with the downward-pointing groove 35, causing the rotational movement of the breechblock 4 in an anticlockwise direction. After a further rotation of the shaft 40 through about 900 the rotational movement of the breechblock 4 is completed and the pin 50 leaves the groove which is now pointing forwards. After a further rotation of the shaft 40 through about 1200 the pin 51 comes into engagement with the downward-pointing groove; after a further rotation of 90 the renewed rotation of the breechblock 4 through a further 90' is completed and after a further rotation of the shaft through about 150 the pins 50 and 51 have again reached the position shown in Fig. 7. During one complete revolution of the shaft 40 the breechblock 4 is turned twice through 90 in an anticlockwise direction. Following the initial rotation through 900 the longitudinal direction of the cartridge chamber 9 is vertical and aligns with the cartridge 7, 8 which is in first place in the magazine, i.e. furthest to the rear in the direction of fire. This cartridge is 19 - inserted fully into the cartridge chamber by the abovedescribed movement of the end 105 of the bell crank 99. Then the breechblock 4 is, as already explained, turned a second time through 90' in an anticlockwise direction so that the cartridge which has just been inserted is now in the firing position.
    On its side which is visible in Fig. 8 the breechblock 4 exhibits four edge recesses 112 which are at 90' from each other and which extend inwards from the outer cylindrical surface, and the upper end 113 of a double-arm locking lever 114 pivot-mounted about an axis 115 is held in one of the edge recesses 112 of the notch 112 by the fact that the free lower end 116 of the locking lever 114 is, in the position shown, up against a control face 117 of the control disc 54. Disposed opposite the control face 117 on the control disc 54 is a control face 118 whereby the control face 118 occupies a greater circumferential angle than the control face 117. Transitions 119 and 120 of reduced radius are situated between the two control faces 117 and 118 which are cylindrical surfaces of equal radius about the axis of the shaft 40. When, during the rotation of the control disc 54, the end 116 is in contact with these 'transitions 119 and 120, the pins 50 and 51 are at the same time in engagement with the grooves of the breechblock 4 and drive the latter. The edge recesses 112 have approximately the form of a relatively flat "V", both legs of which form an angle of slightly more than 900. In the region of the tip the edge recess is concavely rounded and in the region of the outer ends it is convexly rounded. The locking lever 114 has basically the form of a "C". The form of the edge recesses 112 and of the transitions 119 and 120 is such that the locking lever 114, without much play at its two ends, enables or disables the rotation of the breechblock 4. The moments which are transmitted during the rotation of the control disc 54 from the latter to the lever arm 116 try to lif t the lever arm 116 of f the control disc 54. In addition, the moments transmitted during the rotation of the breechblock 4 from the latter to the lever arm 113 try to lift the lever arm 113 off the breechblock 4. Wear is thereby reduced. As long as the end 116 of the locking lever is in contact with the control faces 117 or 118, the breechblock 4 is locked and is not driven. As soon as the transition 119 comes into the region of the end 116, the drive of the breechblock 4 starts through the engagement of the pin 50 in the adjacent groove 35, and, as a result, the end 113 is forced out of the edge recess 112. As soon as the breechblock 4 nears the loading position the end 113 of the locking lever 114 is again swung into one of the edge recesses 112 by the transition 120 of the control disc 54. After loading, the pin 51 comes into contact with one of the grooves 35 and swings the breechblock 4 into the firing position in which it is turned through 1800 as compared with Fig. 8.
    As can be seen in Fig. 8, the outer end of the firing pin 21 is engaged via a single-arm lever 126 by a helical spring 124 which retracts the firing pin. When the firing hammer 66 is released, whereby it turns in an anticlockwise direction as viewed in Fig. 8, the end face 76 of the yoke of the firing hammer which is formed basically by a U-shaped plate strikes against the outer end 130 of the firing pin 21.
    on the side of the part 2 visible in Fig. 10 a catch lever is mounted on the pivot pin 73 which, at its end facing the firing hammer 66, bears a catch 137 which is held in engagement with a support surface 138 of the firing hammer as long as the end 140 of the catch lever 135 facing away from the catch 137 is forced radially outwards, viewed from the shaft 40, by the release cam 142 of the disc 56.
    The release cam 142 exhibits two are-shaped cam sections 142', 142" of different radius with a gradual transition 143 between the two radii and an abrupt change 144 of radius which allows the catch lever 135 to swing in a clockwise direction when, after the firing of a round, the shaft 40 1 has performed its above-described revolution and has again assumed its position as shown in Fig. 1. Under the force of the firing spring 67 the firing hammer 66, through the intermediary of the non-self-locking wedge face pair 1371 (on the catch) and 138, forces the double-arm catch lever 135 out of the latched position and, insofar as the firing hammer is not locked by the catch hook 68, strikes the firing pin 21 to fire the next round. The face 661 of the firing hammer 66 which forms a segment of a cylindrical surface and adjoins the surface 138 glides along the surface 13711 of the catch 137 and exerts a moment on the catch 137 which tries to lift the catch 137 off the surface W..
    As can be seen from FigA, a short single-arm lever 152 is mounted on a shaft 150 parallel to the shaft 40. This lever projects upwards and a link 154 is pivotmounted on it about a pivot axis 155. Pivot-mounted at a joint 156 at its other end, the link 154 bears an ejector 158 which, if the magazine 31 still contains at least one cartridge, is held by the latter in a position which, viewed in the direction of fire, is behind the cartridge which is to be introduced next into the breechblock 4, whereby the ejector is supported on a support surface 21 of the part 2. Above the joint 156 the ejector 158 bears a bent extention 158' which engages a guide shaft 15911 which is limited by blocks 159 and 159'. While the lever 152 is mounted such that it cannot turn on the shaft 150 at the end region of said shaft facing away from the observer in Fig. 4, a single- arm lever 160 is mounted such that it cannot turn in the end region of the shaft 150 facing the observer, said lever 160 exhibiting at its end a slot 164 which is engaged by a pin 162 of a doublearm lever 166.
    One lever arm of this double-arm lever 166 extends between the pin 162 and the hinge pin 168. The other lever arm 170 forms an angle of approximately 1350 with the firstmentioned lever arm. The free end of the lever arm 170 exhibits a groove pin 172 on the side facing away from the observer. If there is a cartridge in the magazine 31, the lever drive chain 158, 154, 152, 160, 166 assumes the position shown in Fig. 4, whereby the groove pin 172 on the lever arm 170 assumes a position near the peripheral edge of the disc 58 without touching the edge of the disc 58. If, on the other hand, there is no cartridge in the magazine 131, the lever drive chain 158, 154, 152, 160, 166 whose drive elements 152 and 160 are rigidly connected to each other is supported on the peripheral edge of the disc 58 via the groove pin 172 under the influence of the force of a tension spring 171. Only when the disc 58 is moved slowly, as is the case during manual actuation of the knob 175, does the groove pin 172 drop into a groove 173 in the disc 58 due to the force of the tension spring 171. Through the intermediary of the groove pin 172 and the lever drive chain the curved guiding of the groove 173 finally causes the movement of the ejector 158 which initially moves into the place of the cartridge 14 shown in Fig. 4, and, owing to the engagement of the extension 1581 in the guide shaft 159'1 as a result of the movement of the joint 156 under the force of the spring 171, the ejector 158 performs a pivoting motion in a clockwise direction so that it is now approximately in the position of the cartridge 14 shown in Fig. 4.
    As long as the groove pin 172 is guided in the first half of the groove173, the further rotational movement of the disc 58 causes the movement of the ejector 158 through the cartridge chamber 9 which is in the loading position. The extension 1581 is no longer in the guide shaft 159'', but has slipped out of it. If there is a cartridge in the cartridge chamber it is ejected. The second half of the groove 173 causes the retracting of the ejector 158 and, with the exit of the groove pin 172 from the groove 173 the lever drive chain again moves back into the initial position and the force of the spring 171 is, as described above, again supported on the edge of the disc 58. During ejecting, an edge 152' of the lever is in contact with an edge 154' of the link 154. These edges limit the pivoting angle between these two parts to approximately 150.
    The automatic rotation of the disc 58 which is initiated when firing takes place at a high angular velocity so that, owing to the inertia of the double-arm lever 166, the groove pin 172 cannot drop into the groove 173, which guarantees that after the magazine has been emptied the ejector 158 automatically does not go into the action position.
    The groove 173 effects a positive and thus reliable drive of the ejector 158 in both directions of movement of the ejector. The groove 173 has the shape shown in Fig. 4 with two adjacent curved sections. The groove 173 is at its shortest distance from the axis of the disc 58 at the point where these two sections come together to form an obtuse angle.
    Cocking by means of the knob 175 is also necessary if a cartridge has failed to fire. When cocking in this manner, the shaft 40 and all parts connected to it are turned by hand in precisely the same manner as takes place automatically after the firing of a round. If, therefore, when cocking, there is still a cartridge in the magazine in the position shown in Fig. 4, this cartridge is pushed by the feeder 105 into the cartridge chamber 9 when cocking the weapon in the above-depicted manner when the breechblock 4 has turned through 90' out of the position in which the cartridge failed when firing the round. The newly introduced cartridge which, in this example, strikes with the tip of its projectile against the tip of the projectile of the failed cartridge pushes the failed cartridge downwards out of the cartridge chamber and ejects it through the hole 12 (Fig. g). If there are no more cartridges in the magazine the failed cartridge is removed by the ejector 158.
    The graph in Fig. 11 shows the relationship between the angular position of the shaft 40 and its angular velocity. The rotation angle 00 in the graph in Fig. 11 corresponds to the firing position of the weapon shown in the figures. The rotation angle is measured in a clockwise direction as viewed in Fig. 1. At a rotation angle of approximately 40' the shaft 40 and thus the flywheel have reached the maximum rotational velocity of approximately 25 degrees/ms, corresponding to a rotational speed of approximately 69 l/sec, corresponding to approximately 4167 llmin. This maximum rotational velocity is, therefore, about twice as high as the rotational speed which would result with a firing rate of 2000 rounds per minute assuming that the shaft 40 rotates at constant velocity without stopping between the individual rounds. Between this maximum value at approximately 40' of the rotation angle and a rotation angle of approximately 70' there is a severe drop in speed of the flywheel which is caused by the loss of energy during the first rotation of the breechblock 4 through 900. The breechblock 4 which is rotatably mounted in the hole 3 in which it moves freely, but still fits snugly and thus seals well, delivers kinetic energy to the flywheel towards the end of its rotational movement through 90' so that the speed of the shaft 40 increases again in the range between approximately 70' and 900 rotation angle. Then there is a gradual fall which, at a rotation angle of approximately 2800, once again exhibits a brief severe drop in speed which is caused by the second rotation of the breechblock 4 through 900 by the Geneva drive. Between 100' and 240' there is also a visible drop in speed which is caused by the loss of energy of the flywheel as a result of inserting a cartridge into the cartridge chamber which is in the loading position. The kinetic energy still present at a rotation angle of 360 corresponding to an angular velocity of the flywheel of approximately 10'/ms is consumed by the control rod 60 being braked by means of the locking lever 84. Such an excess of energy at the end of a complete revolution is useful in order to be able to overcome any strong resistances of the mechanism to motion which may be caused, for example, by wear or also fouling.
    In order, however, largely to rule out such fouling, the breech mechanism including the loading Mechanism of the weapon and the magazine are preferably fully encapsulated.
    only in Fig. 3 is it indicated that the parts of the weapon shown in the drawing are disposed inside a housing 180 which also exhibits the mounting for the knob 175.
    Most of the various discs and levers of the described specimen embodiment consist of sheet steel which, in most cases, has a thickness of 1 mm. In order to make reliable joint connections with such relatively thin steel, these connections are often effected by fol ding one steel part around the other steel part connected by the joint. This can be seen particularly clearly by comparing Fig. 1 and Fig. 5 taking the example of the locking lever 82 whose horizontal side pointing downwards in Fig. 1 is adjoined by a tab which is bent over to the rear and is again bent at the top around the end of the first control plate 88 which is hinge- mounted on the hinge pin 86. This tab which belongs to the locking lever 82 is identified in Fig. 5 by the reference character 82'. In cases where further such folds are visible in the drawings these are likewise identified by a correspondingly modified reference character.
    In the specimen embodiment the disc 42 has a diameter of approximately 50 mm; the first constant diameter cam 44 is almost a circular disc of approximately 41 mm diameter; the eccentrically mounted second constant diameter cam 46 has a diameter of about 25 mm; the disc 48 has a diameter of about 38 mm; the disc 56 has a diameter of about 35 mm, and the disc 58 has a diameter of about 69 mm. The parts which have just been mentioned are parts of the flywheel. The mass moment of inertia of these parts is also joined by the mass moment of inertia of the control disc 54, the shaft 40 and also the pins 50 and 51. There results a total mass moment of inertia of approximately 4 x 10-4 kgm2. With the above- described maximum speed of about 4100 revolutions per minute an energy of about 30 J is thus stored in the flywheel. This energy is sufficient to perform the abovedepicted movement operations without additional drive from the gas piston.
    The firing hammer 66 (Fig. 12) is pivot-mounted on a pin 75 which is disposed in the part 2. A firing spring 67 in the form of a helical spring is, in a manner not shown, tensioned again after the firing of a round by an automatic tensioning means of the weapon. The firing hammer 66 is basically in the form of a U-shape. It exhibits two parallel spaced- apart legs 68 which are connected by means of a yoke 69, and between said legs 68 there is also the firing spring 67. The front end face 76 of the yoke is set back in relation to the front end face of the legs 68. These end faces of the legs 68 form a stop face 77.
    Fig. 12 shows the position of the individual parts with the weapon cocked. The catch 137 which interacts with the support surface 138 of the firing hammer 66 releases the firing hammer 66 in automatic operation of the weapon whenever a new cartridge has been introduced into the cartridge chamber and the breechblock 4 has again assumed its firing position.
    The outer end of the firing pin 21 is indirectly engaged by a helical spring 124 which retracts the firing pin. The spring is disposed on a pin 125 which is rigidly disposed in the part 2, said pin also serving as the pivot pin for a single-arm lever 126 which is formed by a slightly angled plate exhibiting a slot 140 with which the plate engages recesses 128' of the firing pin 21 provided in two opposite sides of the shank 128. Towards the rear end section of the shank 128, i.e. towards the right in Fig. 12, the recesses 1281 are limited by a slightly thicker part 127 of the shank. This slightly thicker part forms shoulders 127' on which the lever 126 is supported by edge areas of the slot 140. The part 127 is made in one piece with the remaining firing pin and is therefore very strong. The spring 124 is not in the path of the combustion gases escaping at this point despite the seal formed by the shoulder 24 and the corresponding stop face, and therefore the spring 124 is subject to little fouling.
    When the firing hammer 66 is released, whereby it turns in an anticlockwise direction as viewed in Fig. 12, the front end face 76 of the yoke of the firing hammer 66 strikes against the outer end 130 of the firing pin 21 and sets the firing pin in motion against the force of the spring 124. Then, after a further travel of approximately 1 mm, the stop face 77 of the firing hammer 66 impacts on a stop 129 which, owing to a certain elasticity of the material forming the firing hammer 66, immediately throws back the firing hammer 66 even before the firing pin 21 has reached the detonating compound of the cartridge. The firing pin 21 which is in a state of free flight from the instant the firing hammer impacts the stop 129 fires the cartridge after a delay time which is determined by the length of its free-flight travel and its velocity and is thrown back with great force by the developing propellant gases, but can no longer reach the firing hammer which has sprung back off the stop 129. The stop shoulder 24 of the firing pin comes into contact with the corresponding stop face of the insert 23. thereby forming a seal for the propellant gases even before the lever 126 has been moved back by the spring 124 into its initial position shown in Fig. 12. Before this seal takes effect, the gases escape which overtake the firing pin on firing and which are quite likely to foul or destroy the functional components disposed behind the firing pin. So that, during this rapid return motion of the firing pin 21, no detrimental influences act on the lever 126, the recesses 1281 parallel to the direction of displacement of the firing pin 21 are made sufficiently long. The (in Fig. 12) left-hand limiting face of the recesses 1281 is likewise to the left of the (in Fig. 12) right- hand face of the stop 129. The stop 129 is formed by a screw nut holding the insert 23 in the part 2.
    When, in the absence of a cartridge, the firing pin 21 strikes on empty space, the lever 126 which comes up against the stop 129 limits the movement of the firing pin towards the left (in Fig. 12) owing to its engaging the part 127 of the firing pin 21.
    The firing hammer 66 which is thrown back against the force of the firing spring 67 through the impact on the stop 129 is, after reaching a reversal point in its motion, accelerated again by the firing spring in the direction of the firing pin 21 which has in the meantime returned to its starting position. However, the firing hammer 66 does not reach the firing pin 21 because the firing hammer 66 is caught by a hammer cocking means which has in the meantime come into action and the firing hammer 66 is moved back into its cocked position shown in Fig. 12.
    Fig. 14 shows a modification in which, instead of the lever 126 and the spring 124, a single leaf spring 150 is provided which, like the lever 126, contains the slot 140. The leaf spring 150 is secured by screws 152 on the part 2.
    Fig. 15, 16 and 17 show the firing pin 21 whereby the recesses 1281 are represented particularly clearly.
    The firing pin 21 has a total length of 22 mm; the shank 128 has over the majority of its length a square cross section of 3.2 mm side length. In the region of the recesses 128' the thickness of the shank 128 visible in Fig. 16 is slightly reduced andis 2.8 mm, in that area. The part 127 which has a larger cross section than the shank 128 exhibits a maximum cross section dimension of 4 mm in the section shown in Fig. 17. The rear end face of the firing pin is spherical and the shoulders 1271 are convexly arched as shown in Fig. 15. The length of the recesses 1281 is 6. 5 mm and the maximum length of the part 127 is 2.5 mm. The remaining dimensions of the firing pin can be taken from Fig. 15 to 17 which are to scale.
    The diameter of the breechblock 4 is 34 mm. The other dimensions can be taken from Fig. 12 which is to scale.
    The stop 129 and the firing hammer 66 are made from the steel alloy 16 MnCr 5 and have a Vickers hardness HV1 660+60.
    The knob 175 is mounted in a bearing bushing 220 (Fig. 3) which is welded into the housing 180. The knob 175 is held by a screw 222 which engages the threaded bore 224 of a wheel 226 which, from inside the housing 180, engages the bore of the bearing bushing 220 with a shaft stub 2.28 exhibiting the threaded bore 224. When the weapon is ready to fire, but is not actuated, the rotation axis of the knob 175 and of the wheel 226 aligns with the axis 3' of the breechblock 4.
    Fig. 18 is a view of the wheel 226 in Fig. 3 from the right, but turned in relation to Fig. 3. Fig. 19 is a section on line XIX-XIX in Fig. 18. Fig. 20 is a view in the direction of arrow XX in Fig. 18, partially broken off. As shown in Fig. 18 and 19, the wheel 226 bears outside its rotation axis a spring-supported dog 230 which is formed by the free end of a leaf spring 300 which is fastened to the wheel 226 by a rivet 302. The dog 230 projects through a hole 304 in the disc-shaped part 306 of the wheel 226. The dog 230 is preloaded by the leaf spring 300 in the direction of the circular disc 58 which is adjacent to the wheel 226 inside the housing 180 and which is coaxial when the weapon is not actuated. If the weapon is to be cocked to unload the weapon or after a cartridge has failed to fire, the knob 175 is turned by hand by the firer so that the direction of rotation of the knob 175 agrees with the normal direction of rotation of the disc 58. The dog 230 then engages a face 238 of the projection 59 running essentially perpendicular to the drawing plane in Fig. 4 and turns the disc 58, as a result of which the above- described cocking operation is effected.
    If, on the other hand, the movement of the weapon parts is intiated by the weapon, for example when firing a round, then this movement must not be transmitted to the above-described cocking means. Owing to the displaceable mounting of the weapon system in the housing (described immediately below) it is not possible during normal operation of the weapon when firing a round for the projection 59 to come into engagement with the dog 230. Nevertheless, it is conceivable that uncontrolled iilfluences may move the actuating part of the cocking means and, during a weapon-iniated loading operation, the projection 59 may collide with the dog 230. In this case, the wedge face 235 of the projection 59 impacts on the dog 230 and pushes it back without any appreciable torque being transmitted to the knob 175.
    The projection 59 exhibits another slanting face 240 whose direction of slope, if one assumes the disc 58 to be horizontal, runs in Fig. 4 approximately from right to left, i.e. points in the direction of fire. This slanting face 240 is provided because the weapon shown is a rifle with a mounted system. The barrel 1 with the part 2 (rigid with the barrel) and all other shown parts in the housing 180 are displaceably guided perpendicular to the drawing plane in Fig. 3 and thus parallel to the longitudinal axis of the barrel. For this purpose, the housing 180 exhibits sliding guides, namely inwardpointing strip-shaped projections 250 which engage parallel longitudinal grooves 252 in the part 2 rigid with the barrel. The barrel-rigid part 2 is supported in the housing 180 by a spring which is not shown. When a round is fired the barrel-rigid part 2 moves backwards opposite to the direction of fire as a result of the recoil and is, after the round has been fired, moved forwards again in the direction of fire by the aforementioned spring. During this backwards movement of the barrel-rigid part 2 the disc 58 also moves, and the shaft 40 which is coaxial with this disc 58 thus no longer aligns with the knob 175 which is fixed on the housing. During the time in which the barrel-rigid part 2 is not in its rest position, but is in a position displaced to the rear as a result of the firing of a round, it would be possible through whatever circumstances for the knob 175 to be turned slightly. As a result, the dog 230 can get into the path executed by the projection 59 during the forwards movement of the barrel-rigid part 2. To ensure that this does not 4 result in any malfunction, the slanting face 240 is provided which ensures that, when during the depicted movement the slanting face 240 of the projection 59 impacts on the dog 230, the latter is pushed back against the force of the spring 300, so that the barrel-rigid part 2 can assume its proper position.
    In order to guarantee that, when cocking is performed by means of the knob 175, the breechblock 4 which is in the firing position again accurately assumes the firing position after cocking, and also to ensure that the firer cannot inadvertently turn the cocking knob in the wrong direction, there is a coulisse designed for a rotation angle of 3600 disposed between the knob 175 and a part which is rigid with the housing. The coulisse, whose operation is accurately represented in Fig. 21, is provided on a part 320 which surrounds the bearing bushing 220 in the manner of a flange. The coulisse 330 exhibits an inner edge 332 and an outer edge 334, see also Fig. 3. Mounted on the wheel 226 which is rigidly connected to the knob, more specifically on its disc 306, is a pin 340 which is disposed eccentrically in relation to the rotation axis of the wheel 226 and which serves as the mount for a guide arm 342. At its end this guide arm 342 exhibits a guide pin 344 which interacts with the edges 332 and 334 of the coulisse. The guide arm 342 is loaded by a spring 346 so that the guide pin 344 is constantly pressed against the inner edge 332 of the coulisse. The guide arm 342 and its mounting are shown in detail in Fig. 18 to 20. To provide a better view of the guide pin in Fig. 3, the pin 340 is drawn there turned through 122'.
    In the starting position shown in Fig. 21a in which the cartridge chamber aligns with the barrel axis the knob 175 1 is located through the engagement of the guide pin 344 in a recess 348 of the inner edge 332. This acts as a critical load ratchet. If the knob 175 is turned in the correct direction of rotation by the firer, whereby the pin 340 turns in an anticlockwise direction with the disc 306 as viewed in Fig. 21, the guide pin 344 leaves the recess 348 and is brought into the position shown in Fig. 21b. When the knob 175 is turned briskly, the guide pin 344 is directed outwards by an outwards-pointing face 354 of the inner guide edge and finally, as viewed in Fig. 21d, comes against a stop 349 which is formed by the outer coulisse edge 334 and projects more or less radially inwards, as a result of which the rotational movement of the knob is ended. The stop or face area 349 is not exactly radial, but is concavely curved with a radius of curvature which is less than the pivoting radius of the guide pin 344 about the pin 340. Therefore, the inner end 356 of the stop 349 prevents the guide pin 344 from being swung inwards under the force of the spring 346. As soon as the firer releases the knob, however, the wheel 226 can turn back through a fraction of a degree whereby this rotational movement is caused by the spring 346, and the 'guide pin 344 under the load of the spring 346 falls radially inwards through the narrow point 350 between the inner and outer edges of the coulisse into the starting position shown in Fig. 21a. if the firer attempts to turn the knob 175 in the opposite direction, the guide pin 344 is moved slightly out of the recess 348, but it comes up against a support surface 352 of the inner edge 332, as shown in Fig. 21f, thereby effectively preventing incorrect turning of the knob.
    In the specimen embodiment the inner edge 332 forms the "first guide edge" of the patent claims. However, it is also possible to make the arrangement such that the spring 346 presses the guide pin against the outer guide edge and that the stop which terminates the rotational movement is disposed on the inner guide edge. The shape of the guide edges must then be modified accordingly. The centrifugal force acting on the guide pin as a result of the rotational movement of the wheel 226 is of no significance in view of the low angular velocities concerned. The described coulisse can also be used for different rotary drives on a weapon and quite generally for any rotary drives. The advantage of this coulisse lies in its reliable functioning and in the fact that after a predetermined rotation angle, 3600 in the example, it terminates the rotational movement by a clearly perceptible stop. After briefly releasing or reducing the torque on the actuating part, it is possible to recommence the rotational movement.
    With this weapon, by using a simple gear drive it is possible to use a different coulisse with which the rotational movement is terminated after 1800 rotation angle. With such a coulisse the outward and inward projecting projections of the edges 332 and 334 along the circumference are provided twice in total. The rotational movement can also be terminated by the coulisse after an angle of less than 1800. It is also possible, even if not readily applicable in the case of the described weapon, to terminate the rotational movement after unequal angles which add up to 3600, i.e. the projections of the curves 332 and 334 must be provided double and must be arranged such that, for example, the stops take effect after rotation angles of 160 and 2000.
    1 The reference characters in the patent claims are not a restriction, but are intended to facilitate comprehension.
    S-I-) --3c - What is claimed is:- Self -loading hand weapon, preferably rifle, with a locking means exhibiting a lever for locking a movable weapon part as a function of the position of another weapon part, wherein the'lever (114, 135) is a doublearm lever which, with one of its arms, is basically constantly in contact with the movable weapon part and, with its other arm, is in contact with the other weapon part.
    2.
    Weapon as defined in Claim 1, wherein the movable weapon part is a firing hammer (66) of the weapon.
    3. Weapon as defined in Claim 1, wherein the movable weapon part is a basically cylindrical breechblock (4) which contains a cartridge chamber and is disposed such that it can pivot in a part (2) of the weapon which is rigid with the barrel.
    Weapon as defined in any one of the preceding claims, wherein the other weapon part is guided such that it is basically linearly displaceable.
  5. 5. Weapon as defined in any one of Claims 1 to 3, wherein the other weapon part (54, 56) is mounted such that it can rotate or pivot.
  6. 6. Weapon as defined in any one of the preceding clainis, wherein the pivot axis (115, 73) of the double-arm lever (114, 135) is disposed such that the moments acting on the lever try to lift each lever arm off the moving weapon part and off the other weapon part as the latter moves.
    1 2-
  7. 7 --- D Weapon as defined in Claims 2 and 5 with a catch (137) which holds the cocked firing hammer (66) by a support surface (138) until, after firing a round, the breechblock (4) has again reached its firing position, wherein the catch (137) and the support surface (138) are such that the force of the firing spring (67) tries to swing the catch (137) out of engagement with the support surface (138) whereby the double-arm lever (135), one of whose arms is the catch (137) is supported by the end (140) of its other arm on a release cam (142) which is provided on a rotatable disc (126) having a constant direction of rotation, said release cam exhibiting two arc-shaped cam sections (1421, 1421') of different radius with a gradual transition (143) between the two radii on one side and an abrupt change (144Y between the two radii on the other side.
  8. 8. Weapon as defined in Claim 7, wherein the firing hammer (66) exhibits next to the support surface (138) a segment of a cylindrical surface (661), said segment gliding along a surface (13V1) of the catch (137) as the firing hammer strikes.
  9. 9. Weapon as defined in Claims 3 and 5, wherein the breech- block (4) exhibits edge recesses (112) which, through the action of a control disc (54), can be engaged by an end (113) of the double-arm lever (locking lever 114) which is pivot-mounted about a barrel-rigid axis (115) whereby said control disc exhibits two circular control cam sections (117,1118) of equal radius but of different length whereby disposed between said control cam sections are sections (119, 120) which are at a lesser distance from the rotation axis of the control disc.
  10. 10. Weapon as defined in Claim 7, wherein the disc (56) is connected to a switch-wheel (48, 50, 51) of a switchwheel drive which pivots the breechblock (4).
    11. Weapon as defined in Claim 9, wherein the control disc (54) is connected to a switch-wheel (48, 50, 51) of a switch-wheel drive which pivots the breechblock (4).
    Weapon as defined in Claims 7 and 9, wherein the disc (56) and the control disc (54) are rigidly connected to each other.
    - 3q- AMENDMENTS TO THE CLAIMS HAVE BEEN FILED AS FOLLOWS CLAIMS 1. A self-loading hand weapon with locking means comprising a lever for locking a first movable weapon part as a function of the position of another weapon part, wherein the two weapon parts are rigid, and the lever is a rigid double-arm lever which has one arm substantially constantly in contact with the first movable weapon part and has its other arm at least intermittently in contact' with the other weapon part such that during at least part of the movement of the said first movable weapon part the position of the lever is determined solely by non-resilient means.
    2. A weapon according to claim 1, wherein the -first m.-)vab.e weapon part is a firing hammer.
    A weapon according to claim weapon part is a basically cylindrica^.
    whe--e'- tne first movable breeh,,'Loce. containing a 1 E, cartridge chamber and disposed so as to be pivo-able in a part of the weapon which is rigid with the barrel 4. A weapon according to any preceding claim, w-ereJn the said ded such that it is substan--J.ally linearly other weapon part is guL displaceable.
    2,3 5.
    r, wherein the sald A weapon according to any of clairris 1 te 3 other weapon part is rotatably or pivotably---nounted.
    6. A weapon according to any preceding claim, wherein the pivot axis of the double-arm lever is disposed such that the moments acting on the lever try to lift each lever arm ofl the first movable weapon part and off the other weapon part as the latter moves.
    7. A weapon according to claim 2 and clair. 5, including a catch which holds the cocked firing hammer by a support surface until, after firing a round, the first movable weapon part has regainted a firing race are s-jc-hat the position, wherein the ca-,oh and the supporT surl force of the firing spring tries to swing the catcl'-. ouz of engage:7,en-. with the support surface whereby the double-arr- llever, one of whose arms is the catch, is supported by the end of its otner arn. on a o - release cam which is provided on a rotatable disc having a constant direction of a rotation, said release cam comprising two are-shaped cam sections of different radii with a gradual transition between the two radii on one side and an abrupt change between the two radii on the other side.
    8. A weapon according to claim 7, wherein the firing hammer comprises, next to the support surface, a segment of a cylindrical surface, the saidsegment gliding along a surface of the catch as the firing hammer strikes.
    9. A weapon according to claim 3 and claim 5, whereinthe breechblock comprises edge recesses which, through the action of a control disc, can be engaged by an end of the double-arm lever which is pivotally mounted about a barrel-rigid axis, the control disc com prising two circular control can, sections of equal radius but of different length whereby disposed between said control cam sections are sections which are at a lesser distance from the rotation axis -rol disc.
    of the cont 10. A weapon according to claim 7, wherein the rotatable disc is connected to a switch-wheel of a switch-wheel drive which pivots the breechblock.
  11. 11. A weapon according to claim 9, wherein the control disc is connected to a switch-wheel of a switch-wheel drive which pivots the breechblock.
  12. 12. A weapon according to claim 7 and claim 9, wherein the rotatable disc and the control disc are rigidly connected to each other.
GB8312455A 1982-05-08 1983-05-06 Self-loading hand weapon Expired - Fee Related GB2248914B (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE3217469 1982-05-08

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GB2248914A true GB2248914A (en) 1992-04-22
GB2248914B GB2248914B (en) 1992-09-16

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GB8312455A Expired - Fee Related GB2248914B (en) 1982-05-08 1983-05-06 Self-loading hand weapon
GB8312457A Expired - Fee Related GB2248916B (en) 1982-05-08 1983-05-06 Self-loading hand weapon
GB8312456A Expired - Fee Related GB2248915B (en) 1982-05-08 1983-05-06 Self-loading hand weapon
GB8312454A Expired - Fee Related GB2248913B (en) 1982-05-08 1983-05-06 Hand weapon with firing hammer and firing pin

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GB8312457A Expired - Fee Related GB2248916B (en) 1982-05-08 1983-05-06 Self-loading hand weapon
GB8312456A Expired - Fee Related GB2248915B (en) 1982-05-08 1983-05-06 Self-loading hand weapon
GB8312454A Expired - Fee Related GB2248913B (en) 1982-05-08 1983-05-06 Hand weapon with firing hammer and firing pin

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BE (4) BE896680A (en)
FR (3) FR2671394A1 (en)
GB (4) GB2248914B (en)
IT (4) IT8348255A0 (en)
NL (3) NL8301593A (en)

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB486547A (en) * 1936-12-05 1938-06-07 Sanders Small Arms Ltd Improvements in recoil-operated firearms
GB489752A (en) * 1929-05-01 1938-08-03 Rheinmetall Borsig Ag Improvements in or relating to automatic guns
GB616617A (en) * 1946-08-13 1949-01-25 Brevets Aero Mecaniques Improvements in or relating to automatic firearms
GB693907A (en) * 1949-03-17 1953-07-08 Costruzioni Meccaniche Breda E A percussion safety firing device for automatic guns
GB872975A (en) * 1957-05-24 1961-07-19 Oerlikon Buehrle Ag Improvements in and relating to automatic firearms
GB1026232A (en) * 1961-10-31 1966-04-14 Rheinmetall Gmbh Improvements in or relating to breech mechanism for automatic weapons

Family Cites Families (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB136581A (en) * 1917-04-28 1919-12-22 Arthur Trevor Dawson Improvements in or relating to Ordnance Firing Mechanism.
GB210655A (en) * 1923-03-23 1924-02-07 Joseph Declaye Improvements in lock mechanisms for sporting guns
GB381586A (en) * 1931-06-30 1932-10-06 Ceskoslovenska Zbrojovka Akcio Automatic gun
BE471803A (en) * 1946-03-12
US3447526A (en) * 1965-05-03 1969-06-03 Z Jana Svermy Narodni Podnik Cocking device
GB1255924A (en) * 1966-11-29 1971-12-01 Secr Defence Improvements in or relating to cocking mechanisms for guns
BE728733A (en) * 1968-02-26 1969-08-01
ES179136Y (en) * 1972-04-08 1973-07-16 Laurona Armas, S. A. FIRE MECHANISM FOR SEMIAUTOMATIC WEAPONS.
IT1029293B (en) * 1975-04-14 1979-03-10 Benelli P RADIAL PERCUSSION SYSTEM FOR FIREARMS THAT USE SELF-PROPULSION PROJECTS WITH PERIMETER IGNITION
DE2627641C2 (en) * 1976-06-19 1983-11-10 Heckler & Koch Gmbh, 7238 Oberndorf Handle cocking self-loading pistol
DE3165865D1 (en) * 1980-12-18 1984-10-11 Oerlikon Buehrle Ag Apparatus for manually cocking an automatic firearm

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB489752A (en) * 1929-05-01 1938-08-03 Rheinmetall Borsig Ag Improvements in or relating to automatic guns
GB486547A (en) * 1936-12-05 1938-06-07 Sanders Small Arms Ltd Improvements in recoil-operated firearms
GB616617A (en) * 1946-08-13 1949-01-25 Brevets Aero Mecaniques Improvements in or relating to automatic firearms
GB693907A (en) * 1949-03-17 1953-07-08 Costruzioni Meccaniche Breda E A percussion safety firing device for automatic guns
GB872975A (en) * 1957-05-24 1961-07-19 Oerlikon Buehrle Ag Improvements in and relating to automatic firearms
GB1026232A (en) * 1961-10-31 1966-04-14 Rheinmetall Gmbh Improvements in or relating to breech mechanism for automatic weapons

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IT8348255A0 (en) 1983-05-09
GB2248913A (en) 1992-04-22
NL8301594A (en) 1992-04-01
GB2248913B (en) 1992-09-16
FR2671395A1 (en) 1992-07-10
GB2248916B (en) 1992-09-16
BE896681A (en) 1991-12-11
IT8348257A0 (en) 1983-05-09
FR2670280A1 (en) 1992-06-12
BE896679A (en) 1991-12-11
BE896682A (en) 1991-12-11
GB2248914B (en) 1992-09-16
GB2248916A (en) 1992-04-22
NL8301593A (en) 1992-04-01
IT8348256A0 (en) 1983-05-09
GB2248915A (en) 1992-04-22
BE896680A (en) 1991-12-11
IT8348254A0 (en) 1983-05-09
GB2248915B (en) 1992-09-16
NL8301595A (en) 1992-04-01
FR2671394A1 (en) 1992-07-10

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