EP0013897A1 - Affût pour mitrailleuse légère - Google Patents

Affût pour mitrailleuse légère Download PDF

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Publication number
EP0013897A1
EP0013897A1 EP80100078A EP80100078A EP0013897A1 EP 0013897 A1 EP0013897 A1 EP 0013897A1 EP 80100078 A EP80100078 A EP 80100078A EP 80100078 A EP80100078 A EP 80100078A EP 0013897 A1 EP0013897 A1 EP 0013897A1
Authority
EP
European Patent Office
Prior art keywords
weapon
axis
mount
pivot axis
rotating ring
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Granted
Application number
EP80100078A
Other languages
German (de)
English (en)
Other versions
EP0013897B1 (fr
Inventor
Kurt Horn
Walter Müller
Adolf Schneider
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Heckler und Koch GmbH
Original Assignee
Heckler und Koch GmbH
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Heckler und Koch GmbH filed Critical Heckler und Koch GmbH
Publication of EP0013897A1 publication Critical patent/EP0013897A1/fr
Application granted granted Critical
Publication of EP0013897B1 publication Critical patent/EP0013897B1/fr
Expired legal-status Critical Current

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Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41—WEAPONS
    • F41G—WEAPON SIGHTS; AIMING
    • F41G1/00—Sighting devices
    • F41G1/38—Telescopic sights specially adapted for smallarms or ordnance; Supports or mountings therefor
    • F41G1/393—Mounting telescopic sights on ordnance; Transmission of sight movements to the associated gun
    • F41G1/3935—Transmission of sight movements to the associated gun
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41—WEAPONS
    • F41A—FUNCTIONAL FEATURES OR DETAILS COMMON TO BOTH SMALLARMS AND ORDNANCE, e.g. CANNONS; MOUNTINGS FOR SMALLARMS OR ORDNANCE
    • F41A19/00—Firing or trigger mechanisms; Cocking mechanisms
    • F41A19/06—Mechanical firing mechanisms, e.g. counterrecoil firing, recoil actuated firing mechanisms
    • F41A19/08—Mechanical firing mechanisms, e.g. counterrecoil firing, recoil actuated firing mechanisms remote actuated; lanyard actuated
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41—WEAPONS
    • F41A—FUNCTIONAL FEATURES OR DETAILS COMMON TO BOTH SMALLARMS AND ORDNANCE, e.g. CANNONS; MOUNTINGS FOR SMALLARMS OR ORDNANCE
    • F41A27/00—Gun mountings permitting traversing or elevating movement, e.g. gun carriages
    • F41A27/06—Mechanical systems
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41—WEAPONS
    • F41A—FUNCTIONAL FEATURES OR DETAILS COMMON TO BOTH SMALLARMS AND ORDNANCE, e.g. CANNONS; MOUNTINGS FOR SMALLARMS OR ORDNANCE
    • F41A27/00—Gun mountings permitting traversing or elevating movement, e.g. gun carriages
    • F41A27/06—Mechanical systems
    • F41A27/18—Mechanical systems for gun turrets
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41—WEAPONS
    • F41H—ARMOUR; ARMOURED TURRETS; ARMOURED OR ARMED VEHICLES; MEANS OF ATTACK OR DEFENCE, e.g. CAMOUFLAGE, IN GENERAL
    • F41H5/00—Armour; Armour plates
    • F41H5/26—Peepholes; Windows; Loopholes
    • F41H5/266—Periscopes for fighting or armoured vehicles

Definitions

  • the invention relates to a mount for receiving light machine weapons, with an upper mount with devices for releasably fastening the weapon to a weapon carrier, with a lower mount with a rotating ring, which is to be attached to a vehicle, so that the upper mount can be rotated around the vertical axis of the rotating ring with the weapon, which can be pivoted about a horizontal pivot axis, with a height and side adjustment lever arranged below the rotating ring, which can be connected to the rotating ring or are operatively connected to the weapon carrier, with a remote trigger for actuating the weapon trigger, and with a sighting device comprising a deflection mirror, the view of which is below the rotating ring and the line of sight is coupled to the pivoting movement of the weapon about the weapon pivot axis.
  • a known mount of this kind (rear mount of the SPz "Marder", soldier and technology 6/1971, page 332)
  • the weapon is attached to a returnable carriage which is mounted on a cradle, which in turn is mounted in two with the cover plate of the mount welded pedestals is pivotally mounted about a horizontal axis.
  • a sighting periscope is provided for sighting, which comprises two angle mirrors, the upper one of which is coupled to the height adjustment lever via a linkage adjustable for height adjustment.
  • the manufacturing outlay for the entire arrangement is relatively high, because the height transmission from the leveling lever to the angle mirror must be very precise, because the smallest angle errors already lead to a considerable deviation of the line of sight from the axis of the soul, so that the accuracy is reduced too much.
  • the elevation range In order to use a mounted on such a support weapon in both the ground fighting as well as for anti-aircraft defense, the elevation range must reach 15 ° from the horizontal down and at least 50 0 upwards about.
  • aggravation works against air defense, where the target is as long as it is in the range of the weapon ends, moves very quickly, that the possible observation area through the sighting device is severely restricted.
  • Such a directional mount which allows a rapidly moving target to be pursued with the weapon, is known, for example, from DE-AS 20 64 133.
  • the object of the present invention is to improve a carriage of the type mentioned in such a way that on the one hand the effort for the sighting device is significantly reduced and on the other hand a large field of vision is achieved with the weapon being freely movable.
  • the sighting device is constructed as a rigid unit with fixed deflecting mirrors and can be swiveled about a sight axis parallel to the horizontal swivel axis of the weapon, that it is fastened to an aperture which is rotationally symmetrical about the swivel axis of the sight Surface area has that a further pivot axis parallel to the sight axis is rigidly connected to the screen, about which a handlebar is pivoted, the other end of which is articulated to the weapon or the weapon carrier, the sight axis, the weapon pivot axis, the further axis and the handlebar linkage form the corner points of a parallelogram.
  • At least one end of the handlebar is fastened detachably, and the upper mount is arranged eccentrically to the rotating ring and equipped with a hatch within the rotating ring.
  • This embodiment has the advantage that after opening the hatch the handlebars can be easily released and the carriage can be used in the same way as is possible with the known carriage according to DE-AS 20 64 133. With this type of application, flying targets can be fought much better and more effectively than when using a crest mount.
  • the eccentric arrangement of the upper carriage to the rotating ring creates space for the hatch. The shooter can take this place comfortably because by using a carriage according to DE-AS 20 64 133 the weapon ends in the area of the weapon pivot axis and no parts of the weapon carrier or weapon protrude beyond the weapon pivot axis to the rear.
  • the aperture carrying the sighting device can be designed differently. For example, it can have the shape of a quarter ball. In a preferred embodiment of the invention, however, the diaphragm is designed as a roller diaphragm and has the shape of a zy lindersegmentes on. The horizontal sight axis and the axis of the cylinder coincide.
  • the visor device * is preferably attached to the panel in such a way that it can be removed towards the inside of the vehicle or installed from inside the vehicle.
  • Target markings such as crosshairs or the like
  • a rear sight is attached before the sight into the sighting device and a front sight is attached.
  • this has the advantage that the shooter does not have to move around if the rear sight and front sight are designed in the same way as the weapon-specific sight. Since the rear sight is easily accessible inside the vehicle, in a further embodiment it can be arranged to be adjustable and can be moved to different distances.
  • the roller screen is preferably arranged relative to the other parts of the mount so that in the lowest position it is approximately flush with the surface of the lower mount. This has the advantage that it is largely protected against earth bombardment in the lowest position.
  • the roller screen can be cast, for example, as a cast piece made of armored steel in order to obtain the desired bullet resistance even when bombarded with hard core bullets.
  • the roller screen consists of a base body made of light metal or a similar material and a jacket, and optionally end plates made of rolled armored steel.
  • This embodiment not only has the advantage of a lower weight, but also the advantage of a higher * or are the angle mirror of the sighting device Suitability for use at shelling, because when rolled with hard core bullets the rolled armored steel sheet poses less than with an armored steel casting.
  • the jacket is at a distance from the base body and / or the surface of the base body facing the jacket has recessed pockets or chambers.
  • the jacket can spring somewhat and deform inwards, thereby reducing the amount of throwing on the edge of the bombardment crater, so that jamming of the diaphragm relative to the part of the lower mount that is opposite with a small gap * is largely excluded.
  • a weapon is used, the functions of which can be set by the trigger distance of the trigger.
  • the remote deduction is provided with adjustable travel limiters. This means that the desired functions can be set at any time without additional effort on the operating and transmission elements.
  • these devices are located at the highest point of the vehicle on the one hand and therefore have a good effectiveness, on the other hand they are completely safe outside the firing range and can neither disturb nor be destroyed when the weapon is used.
  • these additional devices are built on a protective hood, and they are supplied with power from the interior of the vehicle via cables. This embodiment is particularly advantageous if the protective hood is easily removable in order to be able to comfortably meet military operating conditions, such as for example in the case of air defense.
  • the cables are therefore guided around the rotating ring and wound up in a resilient manner, and there is one stop each to limit the rotation of the rotating ring is provided, which results in a limitation to ⁇ approx. 180 °. This creates a full turning circle and there are no blind spots.
  • the cable enables reliable and interference-free transmission of the supply current of lights and turn signals as well as of speech currents or HF currents, for example to the antenna of a radio, which is also constructed as an additional device.
  • the stops can be designed in different, known ways. In a preferred embodiment of the invention, they are attached to the rotating ring and cooperate with fixed stop bolts.
  • the stop preferably has three latching positions, and when it strikes a first stop bolt, it can be pivoted into an outer latching position in which it interacts with the second stop bolt, whereas it can be pivoted back into the middle latching position when the first stop bolt is moved back .
  • the stop bolts are arranged so that in each case the first stop pin at the end of ⁇ 180 ° - is arranged swiveling range and the second stopper bolt a certain further rotation limited to, for example, 15 ° to 30 0th
  • the shooter After passing through the free area of, for example, ⁇ 180 °, the shooter thus has a noticeable stop stop, which he can pass over until it hits the second stop bolt, if this is necessary.
  • this takes account of all practical requirements and, on the other hand, the power supply via cable is possible without any problems.
  • the cable is guided over the rotating ring and the cable end unwound from the rotating ring is wound on a spring-driven reel or unwound from it in the opposite direction of rotation.
  • the Cover also the weapon from the side.
  • * is preferably provided with a flap which can be actuated from the inside and through which the magazine of the weapon can be exchanged by the gunner located inside the vehicle.
  • a receptacle 11 is attached, which is designed in the manner of a frame.
  • a roller screen 12 is pivotally mounted about a sighting axis 13, which coincides with the cylinder axis of the roller screen 12 and is aligned horizontally, that is to say parallel to the plane of the rotary ring 5.
  • a recess is machined into the roller cover 12, into which the sighting device 3 is inserted from below with the interposition of a seal 14.
  • the sighting device 3 is constructed as a so-called angle mirror with two fixed deflecting mirrors 15 and 16.
  • a grain 17 is assigned to the upper deflecting mirror 15 and is fixedly attached to the outer, radial surface of the roller screen 12.
  • the lower, inner deflecting mirror 16 is assigned a rear sight 18, which is arranged in front of an inspection opening 19, which, together with the lower end of the sighting device 3, is surrounded by padding 20.
  • the rear sight 18 is attached to an arm 21, which in turn is rigidly attached to the roller cover 12.
  • the rear sight 18 can preferably be adjusted to different distances in a known manner.
  • the arrangement of grain 17, rear sight 18 and deflecting mirrors 15 and 16 is selected such that the outer part of a line of sight 22 is parallel to a line of sight of an inserted weapon 23 '.
  • the receptacle 11 has on its rear, facing away from the muzzle of the weapon 23 and facing the cutout 9, a tubular sleeve 24 in which a tube 25 is rotatably mounted, which is open at the top and a pivot 26 is provided on the lower end face of the is rotatably mounted in a socket 27 of the receptacle 11.
  • a tubular sleeve 24 in which a tube 25 is rotatably mounted, which is open at the top and a pivot 26 is provided on the lower end face of the is rotatably mounted in a socket 27 of the receptacle 11.
  • an arm 28 is attached, at the free end of which there is a weapon pivot axis 29 parallel to the sighting axis 13.
  • the tube 25 is fastened to the tube sleeve 24 in an easily detachable manner by means of a quick-release fastener that can be released by a lever 30.
  • a groove 31 is worked into the tube 25, in which the quick-release fastener engages.
  • a bearing frame 32 can be pivoted about the weapon pivot axis 29, to which the rear end of a support tube 33 is rigidly attached.
  • the support tube 33 is cranked laterally at both ends such that it does not prevent the weapon 23 from being received.
  • a bracket 34 is attached to the support tube 33, which carries receiving and fastening means for the easily releasable fixation of the weapon 23.
  • the upper mount 2 is designed as a parallelogram.
  • two arms 36 are rigidly attached to the roller cover 12, which are connected to one another at their outer end by a crossbar 37 and are additionally stiffened.
  • the crossbar 37 is rotatable about a further pivot axis 38 parallel to the sighting axis 13 and the weapon pivot axis 29, which in turn is arranged at the ends of the arms 36 and is immovable relative to the arms 36, a link 39 is pivotable about the pivot axis 38, which is preferably attached directly to the crossbar 37, for example welded on.
  • the end of the link 39 is pivoted on the support tube 33 about an axis 40 which is rigid relative to the support tube 33 and is otherwise parallel to the axes 13, 29 and 38.
  • the end of the link 39 can be attached to the support tube 33 in an easily detachable manner, whereupon after this connection has been released the link can be pivoted downward about the pivot axis 38 so that it lies approximately parallel to the arms 36. I h this position the arrangement is used as a free-directional carriage for combating airborne targets in the predominantly military use, said sighting device is not in use.
  • the distance between the axes 29 and 40 is equal to the distance between the axes 38 and 13 from each other. Likewise, the distance between the axes 38 and 40 is equal to the distance between the axes 13 and 29,
  • a tube piece 42 is provided within the tube 25, axially displaceable under the action of weight compensation springs 41, which acts on the bearing frame 32 'at a distance from the weapon pivot axis 29 and takes up part of the weight of the weapon 23', to enable the shooter to use the weapon more easily and thus more quickly.
  • the actuating and adjusting members 4 comprise in particular a height adjustment lever 43 which, after releasing a lock, moves upward out of the operating position shown in FIG. 1 is pivotable so that it does not protrude into the vehicle interior.
  • an actuating lever 45 is attached which, when it is pulled up on the handle 44 via an operative connection in the form of a linkage 46 or a Bowden cable 46 ', releases a brake against spring pressure, as a result of which the roller cover 12 is attached to it or all attached parts about the visor axis 13 is pivotable.
  • the brake not shown, is engaged spring-loaded and can be released against the spring action by the actuating lever 45 and the linkage 46 or the Bowden cable 46 '.
  • the brake comprises parts movable on the one hand with the roller cover 12 and parts which are fixed relative to the roller cover 12 and are fastened to the base plate 8 or the rotary ring 5. It is preferably designed as a shoe or multi-disc brake.
  • a trigger is also attached to the leveling lever 43 and acts on the trigger of the weapon via a Bowden cable 47.
  • the weapon can be loaded through, for example, a further Bowden cable 48.
  • the Bowden cable 48 engages with an actuating hook 49 on a loading lever 50 of the weapon 23. (The Bowden cable 47 is not shown in FIG. 2).
  • Fig. 7 the leveling lever 43 is shown with the handle 44 but without the operating lever 45.
  • an axis 71 which is approximately parallel to the handle 44, is fastened, about which a lever 72 can be pivoted, the lower end of which projects beyond the handle 44 and is designed as a trigger 73.
  • a core 74 of the Bowden cable 47 articulated by means of a fork 75 attached to its end.
  • a securing roller 76 can be pivoted about an axis 77 in three stages.
  • the axis 77 runs approximately parallel to the longitudinal extension of the leveling lever 43 and approximately perpendicular to the axis 71 and radially to the length of the handle 44.
  • a securing wing 78 is fastened to the securing roller 76 and serves to pivot the securing roller 76.
  • the securing roller 76 At the opposite, upper end of the securing roller 76, where it is located in the region of the upper arm of the lever 72, on which the core 74 of the Bowden cable 47 is articulated, the securing roller is provided with a cutout 79 as well as millings for producing stop surfaces 80 and 81 .
  • the stop surfaces 80, 81 or the cutout 79 can optionally be pivoted into the movement path of the upper arm of the two-armed lever 72. If the locking wing 78 and thus the locking roller 76 are in the position shown, then the two-armed lever 72 cannot be pivoted in the pull-off direction because the upper arm rests on the stop surface 81.
  • the stop surface 80 is in the path of movement of the upper arm of the lever 72 and permits limited movement. If the trigger 73 is now actuated, the core 74 is moved forward and in turn actuates the trigger of the weapon 23, whereby a shot is triggered. The relevant position of the safety wing 78 is marked on the handle 44 with an E. If a burst of fire is to be triggered, the trigger of the weapon 23 must be pulled through further.
  • the securing wing 78 must first be pivoted into the third position labeled F, as a result of which the cutout 79 of the securing roller 76 comes into the movement path of the upper arm of the lever 72.
  • the lever 72 can be pivoted further and thus the trigger of the weapon 23 can be pulled through to the position of the burst of fire or continuous fire.
  • the associated position of the securing wing 78 is designated F in FIG. 7.
  • the Bowden cable 47 ' leads to an intermediate lever 51 which is attached to the handlebar 39' and which engages a trigger 52 of the weapon 23 ', to the trigger housing of which it is fastened by means of a quick-release fastener.
  • FIG. 1 Another actuator in the form of a side straightening lever is not shown in the drawing.
  • This side straightening lever is used to rotate the rotary ring 5 with all the parts attached to it relative to the vehicle.
  • An actuating member for releasing a spring-loaded brake is also provided on the side straightening lever, which is attached to the rotating ring 5 and provided with parts on the counter ring 6 or spring-loaded surfaces.
  • the inner cylinder surface of the counter ring fixed to the vehicle can serve as a braking surface, on which brake elements attached to the upper, horizontal leg of the ring 5 act.
  • a trigger for the Bowden cable 47 or 47 ' On the leveling lever 43 or the handle 44 there is also a trigger for the Bowden cable 47 or 47 ', likewise not shown in the drawing, which is preferably provided with adjustable stops for limiting the trigger movement in order to pull the trigger 52 to different extents can, which makes it possible, when using suitable weapons, to trigger the trigger only to the extent that it executes the set weapon function, e.g. Secure, single fire, continuous fire or burst of fire.
  • the inner actuating end facing the shooter can be provided with a releasable lock which makes it possible to fix the loading lever in the position in which the breech is pulled backwards is. This enables the weapon to be completely secured against unintentional firing of a shot, because even when the trigger is actuated, no shot can be released.
  • the roller screen 12 consists of a body 53 'made of armored steel which is cast in one piece and which is pivotably mounted in the receptacle 11 while maintaining narrow gaps.
  • the roller screen 12 consists of a base body 53 and a size L. body on the lateral surface and on the sides surrounding jacket 54 made of rolled and optionally heat-treated steel sheet.
  • the basic body 53 is in this case made of a material that is not as resistant, for example of light metal, and has a gap 69 between the jacket 54 and the base body 53.
  • chambers 70 opening into the lateral surface of the base body 53 are formed in the base body 53.
  • This design has the advantage that the shell 54 can deform somewhat towards the base 53 when bombarded, so that throws on the edge of the shot crater do not prevent the mobility of the roller blind 12 in the cutout of the receptacle 11. This largely prevents jamming or limiting the height range due to bombardment effects.
  • a lip 55 is attached to the underside of the base plate 8 and extends up to close to the casing 54, which consists of a steel sheet and the penetrating lead, which is tangential to the casing The lead flows in because it behaves almost like a liquid under the high stress when it hits it.
  • the weapon 23 or 23 'can as shown in FIGS Cover 56 which can be pivoted about the weapon pivot axis 29 and which protects the weapon against the effects of weather, dirt and also against the action of throwing anchors and stones and the like during police use.
  • the cover 56 also covers the magazine of the weapon.
  • the magazine is to be replaced Provide hatch cover 10 on its front side adjacent to cover 56 with a flap 57 through which a magazine change from the outside is hardly possible can be carried out visibly.
  • Additional devices such as loudspeaker 58 or an all-round indicator (blue light) 59, are built on the cover 56 for police use.
  • the power supply These units as well as a radio antenna, if provided, are carried out by means of cables routed inwards through the cover hood 56.
  • a latchable stop 61 is attached, which comprises a bolt 64 which can be pivoted about a pin 63 in a holder 62.
  • the bolt 64 has two arc-shaped stop surfaces 65 on its two opposite end faces and a cam 66 located between them and projecting radially outward to the axis of rotation of the rotary ring 5, in whose movement the stop bolts 60 protrude when the rotary ring 5 is rotated when the bolt 64 is in its middle rest position shown in dashed lines in Fig. 4.
  • the latching is effected by rounded recesses 67 machined into the latch 64 on the opposite side of the latch 64, into which a spring-loaded pin 69 engages, which is mounted and guided radially to the pin 63 in a bore in the holder 62.
  • the bolt 64 assumes the middle position shown in dashed lines in FIG. 4. If the rotary ring 5 is pivoted so far in the direction of an arrow 68 that the stop 61 passes the first stop bolt 60, the cam 66 runs against the stop bolt 60 and swivels the bolt 64 into the position shown in solid lines in FIG one of the two arcuate stop surfaces 65 faces the stop bolt 60 which is arranged downstream in the direction of the arrow 68. With the abutting surface 65 against the second stop pin 60 the rotational movement is finally limited. When moving back, the front stop pin 60 runs against the surface adjacent to the cam 66 and swivels the latch 64 back into the position shown in broken lines.
  • the mount shown can be used as a universal mount for both police and military use and can be used both as a top mount and as an open mount. It is particularly advantageous that the shooter can work with the sight he is used to from using the weapon, because a mechanical rear sight and a mechanical sight can be used, which are designed in the same way as the sighting device on the weapon.
  • the length of the line of sight between the rear sight and the front sight can also be measured on the weapon as well as on the mount.
  • the axis parallelogram 13, 29, 38, 40 has as a fixed base the two axes 13 and 29, about which the other two axes move accordingly, the weapon axis and the line of sight being aligned with one another.
  • the angle mirror with fixed mirrors provides an inexpensive and robust sighting device that allows good battlefield observation.
  • All operations such as aiming, releasing, single fire, continuous fire and through-loading, preferably for fighting earth targets, are with the hatch cover 10 closed under armor protection, in order to be able to effectively combat flight targets, preferably in military use, the hatch cover 10 is opened and the quick-release fasteners on the axle 40 and on the trigger 52 and through-loading lever 50 are released. This allows the shooter to fight flight and earth targets without any restrictions.
  • a weapon-specific flying sight is preferred.
  • the brake of the rotating ring 5 is released and locked in the release position.
  • the upper carriage must then be fixed in the tubular sleeve 24 and only be pivotable in height. However, it is better if the rotating ring is braked and does not remain released.
  • the upper mount on the tubular sleeve 24 can then be pivoted freely about the vertical axis and it can be conveniently shot out of the hatch in a position of the rotating ring in the lateral directional range of approximately 150 °. If a larger side straightening area is required, the carriage in the vehicle is rotated accordingly and then fixed again. In this mode of operation, the probability of being hit is increased compared to the previously described mode of operation.
  • the invention is not limited to the exemplary embodiments shown, but deviations are possible without leaving the scope of the invention.
  • individual features of the invention can be used individually or in combination.
  • the upper mount 2 can comprise differently designed storage racks 32, support tubes 33 and brackets 34 with fastening means 35 and handlebars 39, which are each adapted to different weapons 23.

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  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Optics & Photonics (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Telescopes (AREA)
EP80100078A 1979-01-26 1980-01-08 Affût pour mitrailleuse légère Expired EP0013897B1 (fr)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE2902992 1979-01-26
DE2902992A DE2902992C3 (de) 1979-01-26 1979-01-26 Lafette zur Aufnahme leichter Maschinenwaffen mit einer Umlenkvisierung

Publications (2)

Publication Number Publication Date
EP0013897A1 true EP0013897A1 (fr) 1980-08-06
EP0013897B1 EP0013897B1 (fr) 1982-04-21

Family

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Family Applications (1)

Application Number Title Priority Date Filing Date
EP80100078A Expired EP0013897B1 (fr) 1979-01-26 1980-01-08 Affût pour mitrailleuse légère

Country Status (3)

Country Link
US (1) US4336743A (fr)
EP (1) EP0013897B1 (fr)
DE (1) DE2902992C3 (fr)

Cited By (2)

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Publication number Priority date Publication date Assignee Title
FR2593612A1 (fr) * 1986-01-27 1987-07-31 Sopelem Dispositif de visee periscopique
EP2216616A3 (fr) * 2009-02-06 2012-05-23 Rheinmetall Landsysteme GmbH Dispositif de sécurité d'une arme lafettée

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GB8829192D0 (en) * 1988-12-14 1998-03-18 Vickers Shipbuilding & Eng Improvements in or relating to field howitzers
FR2650385B1 (fr) * 1989-07-31 1994-09-09 Hispano Suiza Sa Affut antiaerien leger deployable
FR2656683B1 (fr) * 1989-12-28 1992-03-27 Hispano Suiza Sa Tourelle pour blinde leger equipee d'une arme laterale.
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DE4136602A1 (de) * 1991-11-07 1993-05-13 Wegmann & Co Gmbh Drehringlafette fuer eine leichte waffe an einem kampffahrzeug, insbesondere an einer luke eines kampfpanzers
US6237462B1 (en) * 1998-05-21 2001-05-29 Tactical Telepresent Technolgies, Inc. Portable telepresent aiming system
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DE102004043711B4 (de) * 2004-09-09 2007-05-31 Heckler & Koch Gmbh Freirichtlafette sowie Waffenanordnung mit einer Freirichtlafette
US7743543B2 (en) 2005-10-06 2010-06-29 Theodore Karagias Trigger mechanism and a firearm containing the same
US7752798B2 (en) * 2005-10-14 2010-07-13 Mayerle Ronald T See-through periscope for sighting-in optical or open sights on a firearm
US20070251375A1 (en) * 2006-04-28 2007-11-01 Lockheed Martin Corporation Segmented gun turret for quick assembly
US20110072956A1 (en) * 2007-03-29 2011-03-31 Wall Marcus L Tactical Utility Pole and Door Mount Systems and Methods of Use Thereof
US7802509B2 (en) * 2007-03-29 2010-09-28 Marcus L Wall Tactical utility pole system and method of use thereof
US8109192B2 (en) * 2009-01-28 2012-02-07 Nobles Manufacturing, Inc. Locking mount system for weapons
US20120011963A1 (en) * 2010-07-19 2012-01-19 Burtek, Inc. Traverse mechanism
FR2979425B1 (fr) * 2011-08-29 2013-09-20 Stdm Dispositif de commande de tir deportee permettant la manipulation, en site et gisement, d'une arme.
US9328996B1 (en) 2013-01-16 2016-05-03 Raymond A. Lia Bow sight having extended accuracy range
DE102013101635A1 (de) 2013-02-19 2014-08-21 Krauss-Maffei Wegmann Gmbh & Co. Kg Waffenstation
US10371479B2 (en) * 2013-09-11 2019-08-06 Merrill Aviation, Inc. Stabilized integrated commander's weapon station for combat armored vehicle
US9377255B2 (en) 2014-02-03 2016-06-28 Theodore Karagias Multi-caliber firearms, bolt mechanisms, bolt lugs, and methods of using the same
ITUB20151137A1 (it) * 2015-05-28 2016-11-28 Oto Melara Spa Sistema di supporto per arma da fuoco, in particolare destinato ad essere montato appeso ad una superficie superiore.
CA2999996C (fr) * 2015-09-29 2019-10-22 Russell FRANK Systeme de tourelle coque de camping-car
US11067347B2 (en) 2018-11-30 2021-07-20 Theodore Karagias Firearm bolt assembly with a pivoting handle

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FR638545A (fr) * 1926-12-09 1928-05-26 Precision Moderne Affût pour matériel de tir principalement contre avions
US2085024A (en) * 1933-01-05 1937-06-29 Greenhow Maury Jr Machine gun mount
US2360850A (en) * 1942-07-01 1944-10-24 Joseph M Colby Gun mount
US2390516A (en) * 1941-07-11 1945-12-11 David J Crawford Gun sight mounting
FR916891A (fr) * 1944-10-10 1946-12-18 Arme à feu automatique
US2441874A (en) * 1942-02-24 1948-05-18 Harold W Evans Gun mount for land and water vehicles
US2458956A (en) * 1942-06-26 1949-01-11 Motley Lewis Gun mounting
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CH494940A (de) * 1966-06-24 1970-08-15 Walter Dipl Ing Ruf Panzerfahrzeug mit einer Vorrichtung zur Halterung einer leichten Waffe auf dem Dach
DE2033501A1 (de) * 1969-08-20 1971-03-04 Dansk Industri Syndikat A/S, Herlev (Danemark) Fahrzeuglafette fur gabelgetragenes Maschinengewehr
US3854377A (en) * 1972-05-20 1974-12-17 Keller & Knappich Augsburg Tank turret for automatic weapons

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FR638545A (fr) * 1926-12-09 1928-05-26 Precision Moderne Affût pour matériel de tir principalement contre avions
US2085024A (en) * 1933-01-05 1937-06-29 Greenhow Maury Jr Machine gun mount
US2390516A (en) * 1941-07-11 1945-12-11 David J Crawford Gun sight mounting
US2441874A (en) * 1942-02-24 1948-05-18 Harold W Evans Gun mount for land and water vehicles
US2458956A (en) * 1942-06-26 1949-01-11 Motley Lewis Gun mounting
US2360850A (en) * 1942-07-01 1944-10-24 Joseph M Colby Gun mount
FR916891A (fr) * 1944-10-10 1946-12-18 Arme à feu automatique
US2466725A (en) * 1945-05-22 1949-04-12 Marvin J Minter Vehicle mounted gun and periscope mounting therefor
GB1055480A (en) * 1963-12-05 1967-01-18 Ruf Walter Weapon mountings
CH494940A (de) * 1966-06-24 1970-08-15 Walter Dipl Ing Ruf Panzerfahrzeug mit einer Vorrichtung zur Halterung einer leichten Waffe auf dem Dach
DE2033501A1 (de) * 1969-08-20 1971-03-04 Dansk Industri Syndikat A/S, Herlev (Danemark) Fahrzeuglafette fur gabelgetragenes Maschinengewehr
US3854377A (en) * 1972-05-20 1974-12-17 Keller & Knappich Augsburg Tank turret for automatic weapons

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FR2593612A1 (fr) * 1986-01-27 1987-07-31 Sopelem Dispositif de visee periscopique
EP2216616A3 (fr) * 2009-02-06 2012-05-23 Rheinmetall Landsysteme GmbH Dispositif de sécurité d'une arme lafettée

Also Published As

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US4336743A (en) 1982-06-29
DE2902992C3 (de) 1981-09-24
DE2902992A1 (de) 1980-07-31
DE2902992B2 (de) 1980-11-13
EP0013897B1 (fr) 1982-04-21

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