CN1908570A - Long backseat pipe withdrawing type semi-automatic howitzer emitter capable of combination with light arms - Google Patents

Long backseat pipe withdrawing type semi-automatic howitzer emitter capable of combination with light arms Download PDF

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Publication number
CN1908570A
CN1908570A CN 200510089247 CN200510089247A CN1908570A CN 1908570 A CN1908570 A CN 1908570A CN 200510089247 CN200510089247 CN 200510089247 CN 200510089247 A CN200510089247 A CN 200510089247A CN 1908570 A CN1908570 A CN 1908570A
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CN
China
Prior art keywords
howitzer
rifle
gunlock
backseat
automatic
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Pending
Application number
CN 200510089247
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Chinese (zh)
Inventor
张建明
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Individual
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Individual
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Publication date
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Priority to CN 200510089247 priority Critical patent/CN1908570A/en
Publication of CN1908570A publication Critical patent/CN1908570A/en
Pending legal-status Critical Current

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Abstract

Disclosed is a long backseat pipe withdrawing type semi-automatic howitzer emitter capable of combination with light arms, characterized in that, a transmitting tube mounted with a gap vertically in the guide post bushing, a gun bolt case and a gun bolt body are formed into the backseat of the emitter. A swing block iron of the rigid interlocking gear can make and break by the push of the relative working face on the guide strike needle. When the shrapnel is emitted, the backseat simultaneously oppresses the big and small recoil check spring backseat to move to the place. When performing counterrecoil, the holdback blocks the guide strike needle to make the guide strike needle and the gun bolt body generate an amount of relative displacement and after the breech lock adducts inwards to form the unlocking shape and the joint gun bolt body also stops the counterrecoil. When the transmitting tube gun bolt casing is pushed counterrecoil by the large spring and socks away the cartridge case, the emitter is in a state with the boring open waiting to attract. The blocked guide strike needle and the joint gun bolt case are released when shooting, in the push of the small counter-recoil spring, the gun bolt case counterrecoil is pushed into the boring. The slave guide strike needle moves forward due to the self inertia and opens the block iron to finish the closedown and then strike the shrapnel primer. The shooting cycle is semi-automatic.

Description

Long backseat pipe withdrawing type semi-automatic howitzer emitter capable of combination with light arms
Technical field
Present technique invention belongs to light arm firearms technical field, is specifically related to a kind of light-duty long backseat pipe withdrawing type semi-automatic grenade launcher of howitzer of emission bore more than 20 millimeters that can be combined into one with rifle class light arm.
Background technology
At present, both at home and abroad the artillery system that can launch bore howitzer more than 20 millimeters of trial-production-step pomegranate is unified the grenade launcher of two-tube rifle, when the emission howitzer, owing to the peak value kick is crossed the ambassador soldier and is difficult to bear explosive payload and the howitzer range that has limited the howitzer propellant powder, and complex structure, volume weight is bigger, is not easy to the user and portably uses.
The technological invention content
Present technique invention is a kind of light-duty long backseat pipe withdrawing type semi-automatic grenade launcher that can be combined into one with rifle class light arm or use separately of peak value kick can alleviate the howitzer emission time.
The purpose of present technique invention realizes like this: 1. the transmitting tube gap of long backseat pipe withdrawing type semi-automatic grenade launcher is installed in the rifle body formula carrying handle frame casket of transmitter.Carrying handle frame casket is the body junction member, be shaped on two vertical hole slots that are arranged above and below in the carrying handle frame casket body, go up the fairlead that long stroke back seat is implemented for the howitzer transmitting tube in vertical hole and move forward and backward when advancing again, following pod can be used as automatic rifle body of rifle guide groove and the automatic rifle body of a gun is fastened and connected.2. howitzer transmitting tube and transmitting tube body of rifle and can with the transmitting tube body of rifle carry out the rigidity locking installation the gunlock of gib swing type locking sheet become transmitter jointly back seat partly, this back seat part can be done moving forward and backward of long stroke in the guiding trepanning of frame casket body.3. the rear end face of carrying handle frame casket connect to be installed straight formula gun stock, and the interior space of gun stock is contained and fixed by the outer ring big spring of doing for howitzer transmitting tube and the multiple precession of transmitting tube casing back seat with for transmitter gunlock back seat and advancing groups of springs, groups of springs spring abutment that the inner ring little spring that starts to do formed and the grenade launcher sear that is installed in groups of springs spring abutment rear side again.4. the carrying handle rear side of carrying handle frame casket is that the howitzer that is connected as a single entity with carrying handle shoots bucket or magazine interface.5. the plate machine of grenade launcher firing lock can be installed in the plate machine unification of the rifle firing lock that is combined into one with it in the trigger guard before little handle of rifle body.6. with transmitter carrying handle frame casket under the gun barrel front end appropriate location of the automatic rifle that is fastened and connected of pod the dual-purpose bipod of bifilar spear gun thorn type can be installed.
The advantage and the good effect of present technique invention are simple in structure firm, volume is little, in light weight, external form is smooth succinct, compare with the semi-automatic grenade launcher of other rigid locking mechanisms, kick peak value when the structure of employing technological invention and the long backseat pipe withdrawing type semi-automatic grenade launcher of actuation cycle process have alleviated the howitzer emission greatly, the shooting back seat is soft, can increase the explosive payload and the howitzer range of howitzer propellant powder.Additional bifilar forked type bayonet can be shot bipod and be used, and has improved shooting stability, helps long-range shooting.Bullet bucket type appearance magazine is convenient to the user and is used filling.
Description of drawings
Accompanying drawing 1 is that the primary structural component guide pin bushing is the schematic diagram of the structure and the actuation cycle process of present technique inventive embodiments.(a) shows among the figure: locking and percussion situation; (b) again advance to unblank and cut open the chest shooting situation to be set out.1, primary structural component guide pin bushing; 2, howitzer transmitting tube; 3, transmitter body of rifle; 4, gib locking supporting surface; 5, gunlock body; 6, locking sheet gib; 7, guide rod firing pin; 8, the spacing lateral pin of guide rod firing pin; 9, locking working face; 10, locking supporting surface; 11, the working face of unblanking; 12, sear supporting surface; 13, the outer ring is multiple greatly has meal; 14, the little kicker of inner ring; 15, spring base; 16, sear.
Accompanying drawing 2 is schematic diagrames that present technique invention and automatic rifle are integrated.Among the figure: 1, carrying handle frame box primary structural component; 2, howitzer transmitting tube; 17, the rifle body of a gun; 18, straight formula gun stock; 19, rifle pipe; 20, Forend cover; 21, mechanical scanning tool; 22, howitzer shoots bucket; 23, grenade launcher bolt handle; 24, howitzer percussion plate machine; 25, rifle plates machine; 26, little handle; 27, bifilar forked type bayonet.
Specific embodiments
Below in conjunction with accompanying drawing embodiment is further specified
Shown in accompanying drawing 1, the structure of long backseat pipe withdrawing type semi-automatic grenade launcher and back seat back seat partly, multiple advance and the actuation cycle of semi-automatic percussion is to implement like this: 1. vertical guide pin bushing internal clearance of row is installed with howitzer transmitting tube 2 that can vertically move forward and backward and the transmitter body of rifle 3 of fixedlying connected with the transmitting tube afterbody on the primary structural component carrying handle frame casket body 1, the appropriate location of body of rifle 3 endoporus is shaped on gib locking supporting surface 4, and casing 3 internal clearances are installed with the gunlock body 5 that can move forward and backward.The locking sheet gib 6 of gib swing type blocking mechanism is installed on the appropriate location of gunlock body 5.The through hole internal clearance at gunlock body center be installed with can be in through hole the guide rod firing pin 7 of an amount of axially movable double as gunlock recoil rod, guide rod firing pin 7 is limited by the spacing lateral pin 8 of the guide rod firing pin on the gunlock body 5 with the gunlock body 5 relative stroke distances that move forward and backward, the guide rod firing pin is shaped on locking working face 9 on 7 appropriate locations, gib supporting surface 10, unblank working face 11 and sear supporting surface 12.The ramp effect of locking sheet gib 6 each related work face when being subjected to guide rod firing pin 7 and moving forward and backward can do one one close swing finish close, unlocking action.The rear end face of transmitter body of rifle 3 and gunlock body 5 is contacting the recoil check spring group of being advanced little spring 14 combinations of sending out by big spring 13 that supplies transmitting tube and body of rifle to advance again and gunlock again.The guide rod position of guide rod firing pin 7 is run through gunlock and is advanced again and send out in the little spring 14 and the cluster spring seat 15 of groups of springs, and the rear side of combination spring abutment 15 is equipped with the sear 16 of firing lock.2. the kick of howitzer when emission shooting makes the howitzer transmitting tube 2, transmitter body of rifle 3 of transmitter back seat part and moves with big little spring 13 and the long stroke back seat of 14 enforcements that the gunlock body 5 of 3 one-tenths rigidity lockings of body of rifle situation is oppressed the kicker group simultaneously backward.Put in place back and begin multiple when advancing to move of back seat stroke, sear 16 snaps in the sear supporting surface 12 of guide rod firing pin 7, by the guide rod firing pin 7 of jam when the gunlock body is answered into forward with gunlock body 5 relative to moving a suitable stroke distances backward, after locking sheet gib 6 rear portions moved past gib supporting surface 12 and locking working face 11 on the guide rod firing pin 7 on the gunlock body in this trip distance, inwardly swing folded and enters the working face 12 of unblanking and finish unlocking action.Gunlock body 5 after unblanking stops to continue to advance again because of the related jam effect of sear 16 and guide rod firing pin 7 and the spacing lateral pin 8 of guide rod firing pin.Free the transmitter body of rifle 3 of locking situation and transmitting tube 2 after unblanking and under the promotion of advancing big spring 13 again, advance mobilely separately again, and in the multiple stroke that advances, very cylinder is transferred to by being installed in casing 3 in group bullet on the appropriate location.Transmitting tube 2 and body of rifle 3 enter a back transmitter become the to cut open the chest percussion situation for the treatment of of shooting mode again.When 3. howitzer is pulled the trigger, pull the sear supporting surface 12 back release guide rod firing pins 7 and the gunlock body 5 that is subjected to the related jam effect of guide rod firing pin 7 and the spacing lateral pin 8 of guide rod firing pin that transmitter firing lock pulling sear 16 breaks away from guide rod firing pins 7.Gunlock body 5 after the release is sent out little spring and is inconjunction with 7 beginnings of guide rod firing pin under promoting and answers into mobilely forward advancing again, and the one piece of howitzer that in advancing mobile stroke again ammunition feed mechanism is provided pushes the breech of transmitting tube 2.Gunlock body 5 stops to advance again after springing into thorax and entering the position again when mobile finishing to push away, be subjected to the gunlock body 5 related inertia force that advance the mobile weight of guide rod firing pin 7 dependence own again to continue to move forward, in the stroke that this moves forward, after locking working face 9 promoted locking lug 6 outside flare up locking situations, the firing pin position bump howitzer fire in a stove before fuel is added of guide rod firing pin 7 was implemented the howitzer emission.In howitzer when emission,, the transmitter back seat begins partly that back seat next time advances again and the circulation of firing action, and endless form is automanual.4. if increase the member of other electronic control types in the firing lock of the semi-automatic grenade launcher that present technique is invented, the semi automatic fire endless form of present technique invention can be improved to the continuous semi automatic fire circulation of being adjusted and controlled the transmitter firing rate by the electronic control type member easily.
Shown in accompanying drawing 2: it is can be achieved like this that long backseat pipe withdrawing type semi-automatic grenade launcher and automatic rifle are combined into one: 1. the following pod of carrying handle frame casket body 1 can be used as automatic rifle body of rifle and the automatic rifle body of a gun 17 composition one that is fastened and connected.2. the rear end face of carrying handle frame casket body 1 connects the straight formula gun stock 18 of installation.3. the front end of carrying handle frame casket body 1 fixedly connected the Forend cover 20 of envelope howitzer transmitting tube 2 and rifle gun barrel 19.4. the Forend appropriate location, last plane of overlapping the carrying handle of 20 front end appropriate locations and carrying handle frame casket 1 is equipped with machinery aiming county 21.5. the carrying handle rear side is that the howitzer that is connected as a single entity with carrying handle frame casket shoots bucket 22.6. plate machine 25 unifications of the plate machine 24 of grenade launcher firing lock and rifle firing lock are installed in the trigger guard of little handle 26 front ends of rifle body.7. be equipped with on the automatic rifle gun barrel 19 front end appropriate locations can before and after the bifilar forked type bayonet 27 of folding.8. bifilar forked type bayonet 27 with 19 one-tenth 90 ° of positions of gun barrel the time can about open as the shooting bipod and use.

Claims (5)

1, a kind of can the combination with rifle class light arm or the independent light-duty long backseat pipe withdrawing type semi-automatic grenade launcher that uses as a kind of small arms, it is characterized in that: can in the vertical dowel hole of main structure body spare, make the howitzer transmitting tube that long stroke moves forward and backward, transmitter body of rifle and the back seat part that can become transmitter jointly with the gunlock body of body of rifle rigidity locking.Kick during the howitzer shooting puts the recoil movement simultaneously of back seat part in place.Rigid locking mechanism was unblanked when back seat was partly answered into, and unblank back transmitting tube and body of rifle advance and the dial-out cylinder percussion situation for the treatment of that transmitter becomes to cut open the chest to shoot separately again.During percussion, need the pulling sear to discharge to be implemented answering of gunlock body into to move and push away and spring into thorax by the guide rod firing pin of jam and gunlock body, and behind the locking gunlock percussion howitzer fire in a stove before fuel is added.Making the locking sheet gib of rigid locking mechanism can carry out one one actuating member that closes the make and break lock action that swings is to be shaped on the locking working face in the gunlock body by being installed in, the gib supporting surface is carried out when the guide rod firing pin of unblank working face and sear supporting surface moves forward and backward in the gunlock body relatively.The shooting circulation is automanual.
2, according to claim 1, transmitting tube, transmitter body of rifle and gunlock body jointly partly can long stroke back seats as back seat and are advanced mobile again.
3, according to claim 1: the unlocking action of rigid locking mechanism is to finish in the process that begins to advance again after back seat part back seat puts in place.
4, according to claim 1: carry out that blocking mechanism is unblanked and the actuating member of firing action be by be shaped on locking working face, gib supporting surface, the guide rod firing pin of the double as gunlock recoil rod of unblank working face and sear supporting surface comes complete.
5, according to claim 1: the shooting circulation is automanual, as if increase other Electronic Control members in firing lock, can reach the continuous semi automatic fire circulation of adjustment and control shooting firing rate by adjusting the blanking time that discharges sear.
CN 200510089247 2005-08-01 2005-08-01 Long backseat pipe withdrawing type semi-automatic howitzer emitter capable of combination with light arms Pending CN1908570A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN 200510089247 CN1908570A (en) 2005-08-01 2005-08-01 Long backseat pipe withdrawing type semi-automatic howitzer emitter capable of combination with light arms

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN 200510089247 CN1908570A (en) 2005-08-01 2005-08-01 Long backseat pipe withdrawing type semi-automatic howitzer emitter capable of combination with light arms

Publications (1)

Publication Number Publication Date
CN1908570A true CN1908570A (en) 2007-02-07

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CN 200510089247 Pending CN1908570A (en) 2005-08-01 2005-08-01 Long backseat pipe withdrawing type semi-automatic howitzer emitter capable of combination with light arms

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Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN108955377A (en) * 2018-07-16 2018-12-07 哈尔滨工业大学 A kind of small-diameter circular cylindricality target Consecutive launcher
CN113295046A (en) * 2020-10-16 2021-08-24 湖北江华机械有限公司 Grenade launcher launching mechanism

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN108955377A (en) * 2018-07-16 2018-12-07 哈尔滨工业大学 A kind of small-diameter circular cylindricality target Consecutive launcher
CN113295046A (en) * 2020-10-16 2021-08-24 湖北江华机械有限公司 Grenade launcher launching mechanism

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