CN208134633U - Unmanned plane carry breaks first gun apparatus - Google Patents
Unmanned plane carry breaks first gun apparatus Download PDFInfo
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- CN208134633U CN208134633U CN201820667828.6U CN201820667828U CN208134633U CN 208134633 U CN208134633 U CN 208134633U CN 201820667828 U CN201820667828 U CN 201820667828U CN 208134633 U CN208134633 U CN 208134633U
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Abstract
The utility model discloses a kind of unmanned plane carries to break first gun apparatus, including holder hanger, rotatable installation holder is installed on holder hanger, first rifle component is equipped with brokenly by rotatable connection card in installation holder, the broken first rifle component includes bore, gun barrel is connected in bore exit end, it is connected to by connector with the exhaust outlet of gas cylinder in bore entrance one end, it is connected with Electromagnetical ejector in striker one end of gas cylinder, the striker for hitting gas cylinder discharges high pressure gas；Port is equipped in bore side and is removably connected with magazine, piston is equipped in bore, is equipped with the driving mechanism connecting with piston close to bore one end on gun barrel, clamps bullet for pushing piston to move back the filling of realization bullet and automatically reset after shooting.Beneficial effect is：It can be realized by the cooperation of driving mechanism and Electromagnetical ejector and continuously emitted in best firing point, can guarantee accuracy rate and personal safety.
Description
Technical field
The utility model relates to a kind of weapon device of unmanned plane carry, in particular to a kind of unmanned plane carry breaks first rifle dress
It sets.
Background technique
Under some special screnes of police department, need that specific target subdue or will refer to using broken first rifle
Fixed glass, which break up, to be checked, is monitored or safety rescue, and sometimes these specific targets may be because of depositing
It is not easy to closely arrest in risk, is limited to decisive range, operator is needed to reach specified firing point, and
These positions may cause the personal safety of operator to be unable to get guarantee, it is also possible to which best firing point is located on tens
High-altitude outside hundred meters of building, operator can not reach at all, just have no way of shooting.
Summary of the invention
Best firing point can be reached the technical problem to be solved by the utility model is to provide one kind continuously to be sent out
It penetrates, can guarantee that the unmanned plane carry of accuracy rate and personal safety breaks first gun apparatus.
The technical solution of the utility model is as follows：
A kind of broken first gun apparatus of unmanned plane carry, including holder hanger, are equipped with rotatable installation on holder hanger
Holder is equipped with brokenly first rifle component by rotatable connection card in installation holder, which includes bore,
Bore exit end connects gun barrel, is connected to by connector with the exhaust outlet of gas cylinder in bore entrance one end, in high pressure gas
Striker one end of cylinder is connected with Electromagnetical ejector, and the striker for hitting gas cylinder discharges high pressure gas；It is set in bore side
There is port and be removably connected with magazine, piston is equipped in bore, is equipped on gun barrel close to bore one end and connects with piston
The driving mechanism connect clamps bullet for pushing piston to move back the filling of realization bullet and automatically reset after shooting.
As further preferred, the bore shape is cuboid, is located at its entrance one end in bore top surface and is equipped with bar shaped
Hole is equipped with boss on piston and is pierced by by strip-shaped hole, for connecting the driving mechanism.
As further preferred, the driving mechanism includes the retarder being mounted on gun barrel, and the output end of retarder is
One horizontally disposed and reciprocating rack gear, rack gear outer end are connect with the boss on piston, are moved back for band piston
It is dynamic；Compression spring is equipped between rack gear outer end and connector, automatically reseting for shooting pusher piston clamps bullet.
As further preferred, the gear being engaged with rack in the retarder is sector gear, is pushed away for band carry-over bar
Piston is detached from rack gear realization of engaging after moving back is dallied, so as to the reset of piston.
As further preferred, spring base, the compression spring clamping are respectively fixed on rack gear outer end and connector
Between two spring bases.
As further preferred, fixed inserted with guiding connector sleeve and in bore entrance one end by spiral cover, be oriented to
Connector sleeve outer end is pierced by by the centre bore of spiral cover and is threadedly coupled with the connector, and the axle center of the piston is equipped with through-hole
And the inner end of guiding connector sleeve is sleeved on by clearance fit.
As further preferred, the gas cylinder is located at below gun barrel and is arranged in parallel with gun barrel.
As further preferred, the Electromagnetical ejector includes an installation set, the striker one of installation set and gas cylinder
Outer rim is held to be threadedly coupled, bottom is equipped with electromagnet and buffer spring in installation set, installs in installation set by clearance fit
The striker that strong magnetic pushes emitter to hit gas cylinder is generated after having emitter, the electromagnet to be powered.
As further preferred, it is additionally provided with accumulator on installation holder, for being electrically connected the electromagnet of Electromagnetical ejector
With the battery of unmanned plane, to drive the work of Electromagnetical ejector.
As further preferred, electronic valve is equipped on accumulator, for receiving remote controller signal and the control of unmanned plane
The work of accumulator processed.
As further preferred, two motors are equipped in installation holder, wherein first motor and holder hanger pass through the
One belt gear connection, for driving installation holder to rotate around holder hanger；Second motor and connection card insertion are pacified
The one end filled in holder is connected by the second belt gear, for being drivingly connected fastener and broken first rifle component in installation holder
Interior overturning.
The utility model has the beneficial effects that：The unmanned plane carry breaks first gun apparatus and is hit by remote control trigger Electromagnetical ejector
The striker release high pressure gas for hitting gas cylinder, can quickly fire the rubber bullet entered in bore by magazine；Due to
It is equipped with piston in bore, is equipped with the driving mechanism connecting with piston close to bore one end on gun barrel, is pushed away by driving mechanism
Piston, which moves back the filling of achievable bullet and automatically resets after shooting, clamps bullet；Therefore pass through driving mechanism and electromagnetism bullet
The cooperation of emitter can be realized continuously to be emitted in best firing point, can guarantee accuracy rate and personal safety.
Detailed description of the invention
Fig. 1 is the structural schematic diagram of the utility model.
Fig. 2 is the structural schematic diagram that first rifle component is broken in Fig. 1.
Fig. 3 is the left view of Fig. 2.
Fig. 4 is the top view of Fig. 3.
Fig. 5 is the A-A cross-sectional view of Fig. 2.
In figure：Holder 1, first motor 2, the first belt gear 3, holder hanger 4, accumulator 5, the second motor are installed
6, the second belt gear 7, connection card 8, electronic valve 9, connector 10, spring base 11, compression spring 12, piston 13,
Boss 1301, bore 14, strip-shaped hole 1401, rack gear 15, retarder 16, magazine 17, gun barrel 18, valve inside 19, gas cylinder 20,
Electromagnetical ejector 21, driving motor 22, gear reduction 24, sector gear 25 are oriented to connector sleeve 26, installation set 27, electromagnetism
Iron 28, buffer spring 29, emitter 30, striker 31, spiral cover 32, air gauge 33, union 34.
Specific embodiment
The following will be combined with the drawings in the embodiments of the present invention, carries out the technical scheme in the embodiment of the utility model
Clearly and completely describe, it is clear that the described embodiments are only a part of the embodiments of the utility model, rather than whole
Embodiment.Based on the embodiments of the present invention, those of ordinary skill in the art are without creative efforts
All other embodiment obtained, fall within the protection scope of the utility model.
As shown in Figure 1-Figure 3, the utility model relates to a kind of unmanned plane carry break first gun apparatus, including holder is hung
Frame 4 is equipped with rotatable installation holder 1 on holder hanger 4, passes through rotatable connection in the notch of installation holder 1
Fastener 8 is equipped with brokenly first rifle component.The installation holder 1 be by symmetrical two parts make-up and be connected by screw to and
At equipped with two motors in installation holder 1, wherein first motor 2 and holder hanger 4 pass through the first belt gear 3 and connect
It connects, for driving installation holder 1 to rotate around holder hanger 4；Second motor 6 and one in the insertion installation holder 1 of connection card 8
End is connected by the second belt gear 7, is overturn in installation holder 1 for being drivingly connected fastener 8 and broken first rifle component.
The broken first rifle component includes bore 14, gun barrel 18 has been connected through a screw thread in 14 exit end of bore, in bore
14 entrance one end are connected to by connector 10 with the exhaust outlet of gas cylinder 20, and the gas cylinder 20 is located at 18 lower section of gun barrel simultaneously
It is arranged in parallel with gun barrel 18, the entrance and exit of the connector 10 is in 90 degree of angles.Port is equipped with simultaneously in 14 side of bore
It is removably connected with magazine 17 using screw thread by union 34, the main body of magazine 17 is tubulose and is arranged in parallel with gun barrel 18,
Bottom is equipped with top spring in magazine 17, and the rubber bullet for will be mounted in magazine 17 heads into bore 14.Pass through in bore 14
Glade plane space cooperation is equipped with piston 13, is equipped with the driving mechanism connecting with piston 13 close to 14 one end of bore on gun barrel 18, uses
Bullet is clamped in pushing piston 13 to move back the filling of realization bullet and automatically reset after shooting.In the striker 31 of gas cylinder 20
One end is connected with Electromagnetical ejector 21, and the striker 31 for hitting gas cylinder 20 discharges high pressure gas.In gas cylinder 20
The other end is equipped with air gauge 33, for showing air pressure inside.It is equipped with valve inside 19 in 20 side of gas cylinder, for into it
Portion's inflation.
14 shape of bore is cuboid, is located at its entrance one end equipped with strip-shaped hole 1401, in work in 14 top surface of bore
A rectangular boss 1301 is equipped with close to 14 entrance one end of bore on plug 13 and is pierced by by strip-shaped hole 1401, for connecting the drive
Motivation structure.
The driving mechanism includes the retarder 16 being mounted on gun barrel 18, which includes one by two parts pair
Shell made of connecing, is equipped with driving motor 22 and gear reduction 24 in shell, and the output end of gear reduction 24 is
Boss 1301 on one horizontally disposed and reciprocating rack gear 15,15 outer end of rack gear and piston 13 is connected by screw
It connects, is moved backward for band piston 13.Compression spring 12 is equipped between 15 outer end of rack gear and connector 10, outside rack gear 15
End with spring base 11 is fixed with by screw respectively on connector 10, the compression spring 12 be clamped in two spring bases 11 it
Between.It automatically resets for shooting pusher piston 13 and clamps bullet.The tooth engaged in the gear reduction 24 with rack gear 15
Wheel is sector gear 25, which, which is evenly distributed with straight-tooth and is in always with the pinion gear of upper level, engages shape
State, 25 other side outer rim of sector gear are machined with the sector of half of circumference, push piston 13 to move back for band carry-over bar 15
It is detached from the realization of engaging with rack gear 15 later to dally, so as to the reset of piston 13.
In 14 entrance one end of bore inserted with being oriented to connector sleeve 26 and being fixed by spiral cover 32, it is oriented to outside connector sleeve 26
End is pierced by by the centre bore of spiral cover 32 and is connect with the connector 10 by thread seal, and the axle center of the piston 13 is set
There is through-hole and is sleeved on the inner end of guiding connector sleeve 26 by clearance fit.
The Electromagnetical ejector 21 includes an installation set 27,31 one end outer rim of striker of installation set 27 and gas cylinder 20
It is threadedly coupled, bottom is equipped with electromagnet 28 and buffer spring 29 in installation set 27, and buffer spring 29 is set in electromagnet 28
Periphery, emitter 30 is equipped with by clearance fit in installation set 27, the electromagnet 28 generates strong magnetic and pushes after being powered
Emitter 30 hits the striker 31 of gas cylinder 20 to discharge high pressure gas.
It is additionally provided with the accumulator 5 as made of boost module and capacitance connection in the notch inner top of installation holder 1, for electricity
The electromagnet 28 of Electromagnetical ejector 21 and the battery of unmanned plane are connected, to drive the work of Electromagnetical ejector 21.5 table of accumulator
Face be equipped with three eight segment numeral pipe Dynamically Announce alternating voltages, Electromagnetical ejector 21 ejection electric discharge after, by 5 energy storage of accumulator into
Row emits next time, forms semi-automatic repeating.
Electronic valve 9 is connected with by triode on the boost module of accumulator 5, for receiving the remote controler of unmanned plane
Signal and the work for controlling accumulator 5.
When work, the rubber bullet used is filled in magazine 17, which is mounted on unmanned plane by holder hanger 4
Bottom of the frame is connected the battery of the power input of accumulator 5 and unmanned plane by conducting wire, by first motor 2, the second motor
6 and driving motor 22 be electrically connected respectively with the winged control of unmanned plane.After taking off, pass through the remote control control unmanned plane during flying of unmanned plane
To best firing point, while by the remote control control first motor 2 of unmanned plane and the rotation of the second motor 6, to control peace
It fills the broken first rifle component on holder 1 and is in best shooting angle.
The remote controler starting driving motor 22 for passing through unmanned plane when shooting first, by gear reduction 24 with carry-over bar
15 and piston 13 move backward, enter in bore 14 for rubber bullet and reserve enough spaces, when piston 13 is moved to rear end, bullet
The rubber bullet of outermost end enters in bore under the spring effect of top in casket 17, this hour rack 15 is disengaged from sector gear 25, tooth
Item 15 and piston move ahead under the action of compression spring 12 to be resetted, and rubber bullet is clamped between piston and gun barrel 18, with preparation
It penetrates.
Then it is acted by the remote control control electronic valve 9 of unmanned plane, makes 5 quick release high voltage and current of accumulator extremely
Electromagnetical ejector 21, the electromagnet 28 of Electromagnetical ejector generate strong magnetic after being powered and push 30 fast ram gas cylinder 20 of emitter
Striker to discharge high pressure gas.High pressure gas is sequentially entered in connector 10 and bore by the exhaust outlet of gas cylinder, will
The rubber bullet being clamped between piston and gun barrel is quickly got by gun barrel, realizes percussion.After firing, rack gear 15 and rotation one
The sector gear in week repeats to engage, and driving motor 22 iterates through gear reduction 24 and moves back with carry-over bar 15 and piston
Dynamic, piston repeats above-mentioned movement and rubber bullet is clamped between piston and gun barrel again, the remote controler of Repetitive controller unmanned plane, just
Continuous shooting can be achieved.
It is not only in the description and the implementation although the embodiments of the present invention have been disclosed as above
Listed utilization, it can be applied to various fields suitable for the present invention completely, for those skilled in the art,
Other modifications may be easily implemented, therefore without departing from the general concept defined in the claims and the equivalent scope, this reality
It is not limited to specific details and legend shown and described herein with novel.
Claims (10)
1. a kind of unmanned plane carry breaks first gun apparatus, including holder hanger, rotatable installation cloud is installed on holder hanger
Platform, it is characterized in that：First rifle component is equipped with brokenly by rotatable connection card in installation holder, which includes
Bore connects gun barrel in bore exit end, is connected to by connector with the exhaust outlet of gas cylinder in bore entrance one end,
Striker one end of gas cylinder is connected with Electromagnetical ejector, and the striker for hitting gas cylinder discharges high pressure gas；In bore
Side is equipped with and port and is removably connected with magazine, and piston is equipped in bore, on gun barrel close to bore one end be equipped with
The driving mechanism of piston connection clamps bullet for pushing piston to move back the filling of realization bullet and automatically reset after shooting.
2. unmanned plane carry according to claim 1 breaks first gun apparatus, it is characterized in that：The bore shape is cuboid,
It is located at its entrance one end equipped with strip-shaped hole in bore top surface, boss is equipped on piston and is pierced by by strip-shaped hole, for connecting
State driving mechanism.
3. unmanned plane carry according to claim 1 or 2 breaks first gun apparatus, it is characterized in that：The driving mechanism includes peace
Retarder on gun barrel, the output end of retarder are a horizontally disposed and reciprocating rack gear, rack gear outer end with
Boss connection on piston, moves backward for band piston；It is equipped with compression spring between rack gear outer end and connector, is used for
It shoots pusher piston and automatically resets and clamp bullet.
4. unmanned plane carry according to claim 3 breaks first gun apparatus, it is characterized in that：It is engaged with rack in the retarder
Gear be sector gear, for carry-over bar push piston move back after be detached from rack gear engage realization dally, to live
The reset of plug.
5. unmanned plane carry according to claim 3 breaks first gun apparatus, it is characterized in that：Divide on rack gear outer end and connector
It is not fixed with spring base, the compression spring is clamped between two spring bases.
6. unmanned plane carry according to claim 1 or 2 breaks first gun apparatus, it is characterized in that：It is inserted into bore entrance one end
There is guiding connector sleeve and to fix by spiral cover, guiding connector sleeve outer end be pierced by by the centre bore of spiral cover and with the company
Fitting is threadedly coupled, and the axle center of the piston is equipped with through-hole and is sleeved on the inner end of guiding connector sleeve by clearance fit.
7. unmanned plane carry according to claim 1 breaks first gun apparatus, it is characterized in that：The gas cylinder is located under gun barrel
Fang Bingyu gun barrel parallel arrangement.
8. unmanned plane carry according to claim 1 breaks first gun apparatus, it is characterized in that：The Electromagnetical ejector includes one
Installation set, installation set are threadedly coupled with striker one end outer rim of gas cylinder, and bottom is equipped with electromagnet and buffering in installation set
Spring, is equipped with emitter by clearance fit in installation set, and the electromagnet generates strong magnetic and emitter is pushed to hit after being powered
Hit the striker of gas cylinder.
9. unmanned plane carry according to claim 1 or 8 breaks first gun apparatus, it is characterized in that：It is additionally provided on installation holder
Accumulator, for being electrically connected the electromagnet of Electromagnetical ejector and the battery of unmanned plane, to drive the work of Electromagnetical ejector.
10. unmanned plane carry according to claim 9 breaks first gun apparatus, it is characterized in that：Electronic valve is equipped on accumulator
Door, for receiving the remote controller signal of unmanned plane and controlling the work of accumulator.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820667828.6U CN208134633U (en) | 2018-05-07 | 2018-05-07 | Unmanned plane carry breaks first gun apparatus |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820667828.6U CN208134633U (en) | 2018-05-07 | 2018-05-07 | Unmanned plane carry breaks first gun apparatus |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN208134633U true CN208134633U (en) | 2018-11-23 |
Family
ID=64312897
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201820667828.6U Active CN208134633U (en) | 2018-05-07 | 2018-05-07 | Unmanned plane carry breaks first gun apparatus |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN208134633U (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108482680A (en) * | 2018-05-07 | 2018-09-04 | 辽宁力德航空科技有限公司 | Unmanned plane carry breaks first gun apparatus |
| CN109436343A (en) * | 2018-12-20 | 2019-03-08 | 天津聚飞创新科技有限公司 | Unmanned plane |
| CN110253505A (en) * | 2019-06-11 | 2019-09-20 | 南京腾亚精工科技有限公司 | Fastener driving tool |
| CN112455692A (en) * | 2021-01-27 | 2021-03-09 | 北京天创凯睿科技有限公司 | Machine gun sliding seat for fighter plane |
-
2018
- 2018-05-07 CN CN201820667828.6U patent/CN208134633U/en active Active
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108482680A (en) * | 2018-05-07 | 2018-09-04 | 辽宁力德航空科技有限公司 | Unmanned plane carry breaks first gun apparatus |
| CN109436343A (en) * | 2018-12-20 | 2019-03-08 | 天津聚飞创新科技有限公司 | Unmanned plane |
| CN109436343B (en) * | 2018-12-20 | 2024-02-20 | 北京科新信息技术有限公司 | Unmanned plane |
| CN110253505A (en) * | 2019-06-11 | 2019-09-20 | 南京腾亚精工科技有限公司 | Fastener driving tool |
| CN110253505B (en) * | 2019-06-11 | 2022-03-15 | 南京腾亚精工科技股份有限公司 | Fastener driving tool |
| CN112455692A (en) * | 2021-01-27 | 2021-03-09 | 北京天创凯睿科技有限公司 | Machine gun sliding seat for fighter plane |
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