CN2906530Y - Electrical firing device for antiaircraft machine gun - Google Patents
Electrical firing device for antiaircraft machine gun Download PDFInfo
- Publication number
- CN2906530Y CN2906530Y CN 200620110712 CN200620110712U CN2906530Y CN 2906530 Y CN2906530 Y CN 2906530Y CN 200620110712 CN200620110712 CN 200620110712 CN 200620110712 U CN200620110712 U CN 200620110712U CN 2906530 Y CN2906530 Y CN 2906530Y
- Authority
- CN
- China
- Prior art keywords
- trigger
- electromagnet
- trigger shaft
- machine gun
- antiaircraft machine
- 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.)
- Expired - Fee Related
Links
- 238000010304 firing Methods 0.000 title description 6
- 230000004083 survival effect Effects 0.000 abstract description 2
- 230000001960 triggered effect Effects 0.000 abstract 2
- 230000003213 activating effect Effects 0.000 abstract 1
- 230000003247 decreasing effect Effects 0.000 abstract 1
- 239000011090 solid board Substances 0.000 abstract 1
- 238000009527 percussion Methods 0.000 description 10
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical group [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 3
- 238000005516 engineering process Methods 0.000 description 3
- 238000000034 method Methods 0.000 description 3
- 230000008569 process Effects 0.000 description 3
- 239000000853 adhesive Substances 0.000 description 2
- 230000001070 adhesive effect Effects 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 230000008901 benefit Effects 0.000 description 1
- 230000015556 catabolic process Effects 0.000 description 1
- 230000007812 deficiency Effects 0.000 description 1
- 238000006731 degradation reaction Methods 0.000 description 1
- 230000005611 electricity Effects 0.000 description 1
- 230000036541 health Effects 0.000 description 1
- 230000008676 import Effects 0.000 description 1
- 230000006872 improvement Effects 0.000 description 1
- 238000002789 length control Methods 0.000 description 1
- 230000001737 promoting effect Effects 0.000 description 1
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- Toys (AREA)
Abstract
The utility model discloses a power triggered device for antiaircraft gun, comprising a breech, a trigger, and a shank. A magnetic switch is positioned on the shank behind the trigger through a magnetic solid board. A trigger lever is arranged between the magnetic switch and the trigger. The magnetic core is connected with an end of the trigger lever, and the other end is positioned in front of the trigger for activating the trigger. A trigger lever reset spring is arranged between the magnetic switch and trigger. When the magnet is on, the core enables the trigger lever to move towards the magnet. The trigger is activated by the trigger lever which acts as a human hand. Therefore, the power triggered device can realize remote shooting from the armed car. Soldiers do not need to get out of the car, which solves the safety problems, improves the survival opportunities of the passengers in a battle, what's more, the shooting is accurate, and the delay of shooting time and manual shooting is decreased.
Description
Technical field
The utility model relates to the improvement technology of antiaircraft machine gun, in particular for the percussion lock on the antiaircraft machine gun on the panzer.
Background technology
On the panzer of the usefulness of operation such as tank, armoured carrier, the infantry fighting vehicles, dispose secondary weapons such as antiaircraft machine gun mostly.The percussion lock of existing antiaircraft machine gun is a trigger configuration, and antiaircraft machine gun is realized percussion by the staff cocking fully.Put forth effort for the ease of pulling, be positioned at both sides, trigger rear portion at gun breech and be provided with handle.This antiaircraft machine gun in use, needing the soldier to walk out panzer could shoot, soldier's health is directly exposed under enemy's the firepower, loses protection, is easy under attackly, its life security can not get effective guarantee, causes the combat casualty easily.
The content of utility model
Need direct manual manipulation at existing antiaircraft machine gun percussion lock existence, can not ensure the deficiency of soldier's safety, the purpose of this utility model provides a kind of antiaircraft machine gun electric shoot device of electric control operation, can be implemented in the purpose of percussion antiaircraft machine gun in the panzer.
The purpose of this utility model is achieved in that a kind of antiaircraft machine gun electric shoot device, comprise gun breech, trigger and handle, by the electromagnet fixed head electro-magnet switch is installed at gun breech, electro-magnet switch is positioned at the trigger rear portion, between electro-magnet switch and trigger, be provided with trigger shaft, electromagnet core is connected with trigger shaft one end, and the trigger shaft other end is the T type and is used for cocking across trigger the place ahead, is provided with the trigger shaft back-moving spring between electro-magnet switch and trigger shaft.
Further improve and be: the trigger shaft limited block spacing to trigger shaft is installed on the electromagnet fixed head.
Compared to existing technology, the utlity model has following advantage:
1, this electric shoot device adopts magnet control, drive trigger shaft toward the motion of electromagnet direction by iron core, the trigger shaft cocking, trigger shaft is equivalent to staff, realize panzer remote control shooting in the car of antiaircraft machine gun, the soldier need not stretch out outside the car, has fundamentally solved soldier's protection question, improves occupant's battlefield survival;
2, when the trigger move distance was pulled the trigger stroke greater than it, antiaircraft machine gun was promptly pulled the trigger, and had realized the electronics percussion of antiaircraft machine gun;
3, the setting of trigger shaft limited block guarantees that the shooting of this electric shoot device is reliable, and the shooting time delay is compared also with manual shooting and had substantial degradation;
4, also can manual manipulation under the out of use situation of electric shoot device, do not influence the final use of weapon, have and be suitable for widely and promotional value;
5, the utlity model has simple in structurely, compact, in light weight, easy and simple to handle, assembling and dissembling speed is fast, for ease of maintenaince, characteristics such as man-machine work efficiency is good.
Description of drawings
Fig. 1 is a structural representation of the present utility model.
Fig. 2 is the vertical view after Fig. 1 removes the electromagnet fixed head.
Among the figure, 1-gun breech, 2-trigger, 3-trigger shaft, 4-handle, 5-electromagnet fixed head, 6-electromagnet, 7-return spring, 8-screw, 9-electromagnet core, 10-antiaircraft machine gun separator tube, 11-limited block.
The specific embodiment
The utility model is described in further detail below in conjunction with accompanying drawing.
Referring to Fig. 1, Fig. 2, as can be seen, antiaircraft machine gun electric shoot device of the present utility model still keeps trigger 2, handle 4 from the figure, and handle 4 is fixed on the end of gun breech 1 by screw, is positioned at both sides, trigger 2 rear portion.The electro-magnet switch that its newly-increased core is mainly trigger shaft 3, is made up of electromagnet 6 and electromagnet core 9.Electro-magnet switch is positioned at trigger 2 rear portions and is fixed on the electromagnet fixed head 5, is fixed on the gun breech 1 by electromagnet fixed head 5 again.Trigger shaft 3 is between electro-magnet switch and trigger 2; Trigger shaft 3 is the T font, and trigger 2 be arranged in parallel for two triggering pullings, and trigger shaft 3 vertical sections are positioned in the middle of two triggering pullings and pass through screw 8 and are connected with electromagnet core 9 hinges, and trigger shaft 3 horizontal segments are positioned at trigger 2 the place aheads and are used for cocking 2.Be provided with trigger shaft back-moving spring 7 between electromagnet 6 and trigger shaft 3, back-moving spring 7 is enclosed within on the iron core 9, and its two ends are connected with trigger shaft 3 with electromagnet 6 respectively.Antiaircraft machine gun separator tube 10 is installed on gun breech 1.After lifting fire, trigger shaft 3 resets under the effect of back-moving spring 7.
For making trigger shaft 3 can reliably spur antiaircraft machine gun trigger 2, the utility model electromagnet fixed head 5 is provided with the trigger shaft limited block 11 spacing to trigger shaft, has guaranteed the reliable percussion of this electric shoot device.Trigger shaft limited block 11 is positioned at after two triggering pullings 2, on the trigger shaft limited block, be provided with for the vertical section of trigger shaft and pass the groove that Open Side Down, trigger shaft vertically section passes the trigger shaft limited block by the groove on the trigger shaft limited block, and the trigger shaft horizontal segment is over against the trigger shaft limited block.When the trigger shaft cocking moves backward, the motion of its vertical direction will be subjected to the restriction of limited block, and can not break away from trigger, make trigger shaft can reliably spur the antiaircraft machine gun trigger, guarantee that percussion is reliable.
Operation principle of the present utility model and process: after the electro-magnet switch energising, promptly produce magnetic field and make iron core inspiration electromagnet (among the figure for moving right), motion drive trigger shaft unshakable in one's determination overcomes the active force of back-moving spring and trigger and moves, and then makes trigger also along with (to the right) motion by the trigger shaft cocking.This process back-moving spring is compressed, the savings energy.When the trigger range ability was pulled the trigger stroke greater than it, antiaircraft machine gun was promptly pulled the trigger by the electronics of percussion realization antiaircraft machine gun.In case and electromagnet outage magnetic field disappears, back-moving spring is released trigger shaft again, and trigger shaft resets, for shooting is next time got ready.
The power on/off of the utility model electromagnet can adopt following proposal to realize: a firing button is set, and firing button is sent out driver module by motor and electric shock and is connected with relay, and relay is as the switch of magnet switching electricity.If discharge cock is closed, shooter presses firing button, the percussion signal imports the motor and an electric shock driver module of letter control system into, and " motor and electric shock are sent out driver module " processing of process letter control system also output signal makes the relay adhesive, makes the electromagnet energising after the relay adhesive.Electromagnet outage after shooter unclamps firing button, trigger automatically resets under the effect of back-moving spring, and antiaircraft machine gun is lifted fire.Shooting bullet number is by the time length control of pressing firing button.
Claims (4)
1, a kind of antiaircraft machine gun electric shoot device, comprise gun breech (1), trigger (2) and handle (4), it is characterized in that: the electro-magnet switch of being made up of electromagnet (6) and electromagnet core (9) is installed at gun breech (1), electro-magnet switch is positioned at trigger (2) rear portion, is provided with trigger shaft (3) between electromagnet (6) and trigger (2); Electromagnet core (9) is connected with trigger shaft (3) one ends, and trigger shaft (3) other end is the T type and is used for cocking across trigger (2) the place ahead, is provided with trigger shaft back-moving spring (7) between electromagnet (6) and trigger shaft (3).
2, antiaircraft machine gun electric shoot device according to claim 1 is characterized in that: described electromagnet (6) is installed in gun breech by T type electromagnet fixed head (5).
3, antiaircraft machine gun electric shoot device according to claim 2 is characterized in that: described electromagnet fixed head (5) is provided with the trigger shaft limited block (11) spacing to trigger shaft.
4, antiaircraft machine gun electric shoot device according to claim 1 is characterized in that: described trigger shaft (3) is hinged by screw (8) and electromagnet core (9).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 200620110712 CN2906530Y (en) | 2006-05-31 | 2006-05-31 | Electrical firing device for antiaircraft machine gun |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 200620110712 CN2906530Y (en) | 2006-05-31 | 2006-05-31 | Electrical firing device for antiaircraft machine gun |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN2906530Y true CN2906530Y (en) | 2007-05-30 |
Family
ID=38115170
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN 200620110712 Expired - Fee Related CN2906530Y (en) | 2006-05-31 | 2006-05-31 | Electrical firing device for antiaircraft machine gun |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN2906530Y (en) |
Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| TWI414744B (en) * | 2011-03-04 | 2013-11-11 | Military Academy | 7.62 mm general machine gun with the shooting module |
| TWI612273B (en) * | 2016-09-26 | 2018-01-21 | 李崇銘 | Automatic electric gun structure |
| CN108088306A (en) * | 2018-01-18 | 2018-05-29 | 南京理工大学 | A kind of wireless remote control electric shoot device |
| CN110560305A (en) * | 2019-08-02 | 2019-12-13 | 北京北机机电工业有限责任公司 | Mechanical unlocking automatic trigger device |
| CN111854516A (en) * | 2020-08-03 | 2020-10-30 | 泰州学院 | Automatic Rifle Timed Firing System |
| CN115979057A (en) * | 2022-11-25 | 2023-04-18 | 湖南宇正智能科技有限公司 | Manual-automatic integrated percussion device |
| CN116007432A (en) * | 2022-11-25 | 2023-04-25 | 湖南宇正智能科技有限公司 | Novel seat frame device for improving shooting precision of heavy machine gun |
-
2006
- 2006-05-31 CN CN 200620110712 patent/CN2906530Y/en not_active Expired - Fee Related
Cited By (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| TWI414744B (en) * | 2011-03-04 | 2013-11-11 | Military Academy | 7.62 mm general machine gun with the shooting module |
| TWI612273B (en) * | 2016-09-26 | 2018-01-21 | 李崇銘 | Automatic electric gun structure |
| CN108088306A (en) * | 2018-01-18 | 2018-05-29 | 南京理工大学 | A kind of wireless remote control electric shoot device |
| CN108088306B (en) * | 2018-01-18 | 2023-08-04 | 南京理工大学 | Wireless remote control electric firing device |
| CN110560305A (en) * | 2019-08-02 | 2019-12-13 | 北京北机机电工业有限责任公司 | Mechanical unlocking automatic trigger device |
| CN110560305B (en) * | 2019-08-02 | 2020-10-13 | 北京北机机电工业有限责任公司 | Mechanical unlocking automatic trigger device |
| CN111854516A (en) * | 2020-08-03 | 2020-10-30 | 泰州学院 | Automatic Rifle Timed Firing System |
| CN115979057A (en) * | 2022-11-25 | 2023-04-18 | 湖南宇正智能科技有限公司 | Manual-automatic integrated percussion device |
| CN116007432A (en) * | 2022-11-25 | 2023-04-25 | 湖南宇正智能科技有限公司 | Novel seat frame device for improving shooting precision of heavy machine gun |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| C17 | Cessation of patent right | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20070530 Termination date: 20100531 |