CN220483552U - Unmanned aerial vehicle gun mechanical bracket - Google Patents
Unmanned aerial vehicle gun mechanical bracket Download PDFInfo
- Publication number
- CN220483552U CN220483552U CN202321570309.5U CN202321570309U CN220483552U CN 220483552 U CN220483552 U CN 220483552U CN 202321570309 U CN202321570309 U CN 202321570309U CN 220483552 U CN220483552 U CN 220483552U
- Authority
- CN
- China
- Prior art keywords
- unmanned aerial
- aerial vehicle
- seat
- mounting bracket
- lateral wall
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Links
- 238000009434 installation Methods 0.000 claims description 13
- 230000000903 blocking effect Effects 0.000 claims description 10
- 230000000670 limiting effect Effects 0.000 claims description 6
- 238000010276 construction Methods 0.000 claims description 2
- 230000009286 beneficial effect Effects 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 230000002349 favourable effect Effects 0.000 description 2
- 238000010304 firing Methods 0.000 description 2
- 125000003003 spiro group Chemical group 0.000 description 2
- 239000007769 metal material Substances 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
Landscapes
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
Abstract
The utility model discloses an unmanned aerial vehicle gun bracket, which comprises a mounting unit, wherein the mounting unit comprises a mounting frame, the lower end of the mounting frame is fixedly connected with a connecting seat, the connecting seat is provided with two sections which are connected with gun stocks together, one side of the lower end of the mounting frame is fixedly provided with a first driving device, and the output end of the first driving device penetrates through a second side wall to extend to the inner side of the mounting frame to be clamped with a gun trigger.
Description
Technical Field
The utility model relates to the technical field of unmanned aerial vehicles, in particular to an unmanned aerial vehicle mechanical bracket.
Background
The unmanned aerial vehicle has the advantages of low cost, high performance, strong maneuverability, simple and convenient use and the like, and is widely applied to the military and civil fields. In the anti-terrorism and anti-riot, the unmanned aerial vehicle can effectively reduce casualties in future urban combat.
The 79-type submachine gun has the characteristics of simple structure, small volume, light weight, good precision, strong short-distance firepower and convenient carrying and use, is commonly applied to special police teams, and in the prior art, aiming at the 79-type submachine gun, no targeted unmanned aerial vehicle bracket is provided, and most of the submachine guns are unmanned aerial vehicle brackets of handguns, which are not beneficial to mountain areas, jungles, short arms, urban street combat and fight for rescuing people.
Disclosure of Invention
The technical problems to be solved by the utility model are as follows: an unmanned aerial vehicle bracket special for a 79-type submachine gun is provided.
In order to solve the technical problems, the utility model provides the following technical scheme: the utility model provides an unmanned aerial vehicle firearm bracket, includes the installation unit, the installation unit includes the mounting bracket, the lower extreme fixedly connected with connecting seat of mounting bracket, the connecting seat is equipped with two sections and is connected jointly with the stock, the lower extreme one side fixed mounting of mounting bracket has a drive arrangement, the output of drive arrangement passes the second lateral wall and extends to the inboard of mounting bracket and firearm trigger looks joint.
This application is through installing 79 submachine rifle in the lower extreme of connecting seat, through the position about the adjusting unit regulation muzzle, the trigger firing is controlled to the first drive arrangement in the reuse second lateral wall outside, has realized to 79 dedicated unmanned aerial vehicle bracket of submachine rifle.
Preferably: the installation unit upper end fixedly connected with adjusting unit, adjusting unit includes the regulation seat, regulation seat fixed connection is in the upper end of mounting bracket, the outside fixedly connected with second drive arrangement of regulation seat, the front end of regulation seat is close to second drive arrangement's position rotation and is connected with the driving gear, second drive arrangement's output is connected with the driving gear.
Preferably: the adjusting unit further comprises a fixing seat, the fixing seat is fixedly arranged at the tail end of the upper end of the mounting frame, one side, away from the second driving device, of the driving gear is meshed with a driven gear, the circle center of the driven gear is fixedly connected with a screw rod, and the tail end of the screw rod is rotationally connected with the fixing seat.
Preferably: the middle section outside activity of lead screw has cup jointed the link, the both sides of link all articulate there is the alignment jig, the one end that the link was kept away from to the alignment jig is connected with the inner chamber of mounting bracket.
Preferably: the outside of the screw rod is positioned between the connecting frame and the fixed seat and is movably sleeved with a limiting block.
Preferably: the lower extreme one side of mounting bracket is connected with the second lateral wall, first drive arrangement fixed mounting is in the outside of second lateral wall, and the lower extreme of mounting bracket is connected with first lateral wall with the opposite one side of second lateral wall, be hollow out construction on first lateral wall, the second lateral wall.
Preferably: the first side wall and the second side wall are provided with a plurality of fixing holes.
Preferably: the output end of the first driving device penetrates through the second side wall and extends to the inner cavity of the mounting frame to be fixedly connected with a rotating handle, and one side, facing the first side wall, of the free end of the rotating handle is fixedly connected with a connecting rod.
Preferably: the front end of the second side wall is connected with an integrally formed bullet blocking plate, and the bullet blocking plate is of a folding edge structure.
Preferably: the upper end fixedly connected with connecting plate of adjusting unit, installation unit, adjusting unit are all through connecting plate and unmanned aerial vehicle lower extreme fixed connection.
Compared with the prior art, the utility model has the beneficial effects that: this application passes through the lower extreme at the connecting seat with the stock position of 79 submachine rifle through bolt spiro union to set up the fixed orifices on through first lateral wall, the second lateral wall and further fix it, make the trigger position and the connecting rod looks butt of firearm, utilize second drive arrangement to drive driving gear simultaneously and rotate in step along with driven gear, and then when on the sky, adjust muzzle position, this application simple structure, convenient operation proposes a dedicated unmanned aerial vehicle bracket to 79 submachine rifle, be favorable to mountain region, jungle, short weapon meet, city war and rescue man's battle.
Drawings
FIG. 1 is a schematic view of the overall structure of an unmanned aerial vehicle mechanical bracket according to an embodiment of the present utility model;
FIG. 2 is a schematic side view of a mechanical bracket of an unmanned aerial vehicle according to an embodiment of the present utility model;
fig. 3 is a schematic bottom view of a mechanical bracket of an unmanned aerial vehicle according to an embodiment of the utility model.
In the figure: 1-a mounting unit; 11-mounting rack; 12-connecting seats; 13-a first sidewall; 14-a second sidewall; 15-a first drive; 16-rotating handle; 17-connecting rod; 18-spring blocking plates; 19-fixing holes; 2-an adjusting unit; 21-an adjusting seat; 22-a second drive means; 23-a drive gear; 24-driven gear; 25-adjusting frames; 26-connecting frames; 27-a screw rod; 28-fixing seat; 29-a limiting block; 3-connecting plates.
Detailed Description
In order to facilitate the understanding of the technical scheme of the present utility model by those skilled in the art, the technical scheme of the present utility model will be further described with reference to the accompanying drawings.
The terms "first," "second," and the like, are used for descriptive purposes only and are not to be construed as indicating or implying relative importance or implicitly indicating the number of technical features indicated. Thus, a feature defining "a first" or "a second" may explicitly or implicitly include one or more such feature. In the description of the present application, the meaning of "a plurality" is two or more, unless explicitly defined otherwise.
Referring to fig. 1, the embodiment discloses an unmanned aerial vehicle mechanical bracket, which comprises a mounting unit 1, an adjusting unit 2 and a connecting plate 3.
Referring to fig. 1-3, the whole installation unit 1 is made of metal materials and comprises an installation frame 11, a connecting seat 12, a first side wall 13, a second side wall 14, a first driving device 15, a rotating handle 16, a connecting rod 17, a bullet baffle 18 and a fixing hole 19, wherein the installation frame 11 is a plane plate with a rectangular structure, the connecting seat 12 is fixedly installed at the lower end of the installation frame 11, two sections are arranged on the lower surface of the connecting seat 12 and are in threaded connection with a butt of a submachine gun through bolts and 79, so that the stability of the firearm is ensured.
As shown in fig. 1, the first side wall 13 is fixedly connected to the bottom of the right side surface of the mounting frame 11 through a bolt, the second side wall 14 is fixedly connected to the bottom of the left side surface of the mounting frame 11 through a bolt, the first side wall 13 is opposite to the second side wall 14, a plurality of fixing holes 19 matched with firearms are formed in the side walls of the first side wall 13 and the second side wall 14, in this embodiment, the fixing holes 19 are round holes, stability of the firearms is further guaranteed, hollow structures are arranged on the side walls of the first side wall 13 and the second side wall 14, and are triangular in shape, and accordingly the whole weight of the mounting unit 1 is effectively reduced through the hollow structures, so that the unmanned aerial vehicle can fly flexibly in the air.
The first drive device 15 is installed in the outside of second lateral wall 14, and the output of first drive device 15 passes second lateral wall 14 and extends to the space below mounting bracket 11, and the one end and the output fixed connection of first drive device 15 of commentaries on classics handle 16, and the one end that the commentaries on classics handle 16 kept away from first drive device 15 is towards the position fixedly connected with connecting rod 17 of first lateral wall 13, and connecting rod 17 joint is at 97 submachine gun trigger positions.
In this embodiment, when the firearm is integrally transported by the unmanned aerial vehicle together with the installation unit 1, the first driving device 15 is controlled to drive the rotating handle 16 to rotate, and then the connecting rod 17 is driven to rotate back and forth, and the connecting rod 17 rotates to trigger the trigger, so that the firing effect is achieved.
As shown in fig. 1, the bullet blocking plate 18 is located at the front end of the second side wall 14, which may be formed by extending the second side wall 14, where the dang bullet blocking plate 18 and the second side wall 14 are integrally formed and form a substantially 7-shaped structure, the bottom of the bullet blocking plate 18 is in a folded edge structure, and the folded surface of the bullet blocking plate 18 faces to the outside for blocking the popped bullet shell during shooting, so that the practicality and safety of the application are improved when the bullet shell is popped up to the blade of the unmanned aerial vehicle.
Referring to fig. 1-2, the adjusting unit 2 is located at the upper end of the mounting frame 11, and the adjusting unit 2 includes an adjusting seat 21, a second driving device 22, a driving gear 23, a driven gear 24, an adjusting frame 25, a connecting frame 26, a screw rod 27, a fixing seat 28, and a limiting block 29; the adjusting seat 21 is movably connected to the top of the mounting frame 11, a second driving device 22 is installed on one side of the adjusting seat 21, a driving gear 23 is rotatably connected to the outer side of the adjusting seat 21 and is close to the position of the second driving device 22, the output end of the second driving device 22 is meshed with a rotating rod inside the driving gear 23, a driven gear 24 is rotatably connected to one side, far away from the second driving device 22, of the adjusting seat 21, and the driven gear 24 is meshed with the driving gear 23.
The fixing base 28 is fixedly arranged at the tail end position of the upper end of the mounting frame 11, one end of the screw rod 27 is fixedly connected with the driven gear 24, and the other end of the screw rod is rotatably connected with the inner side of the fixing base 28.
The outside rotation of lead screw 27 has cup jointed link 26, and the both sides of link 26 are articulated have alignment jig 25, and the bottom of alignment jig 25 is articulated with mounting bracket 11, and when unmanned aerial vehicle is inoperative, the one end that alignment jig 25 kept away from link 26 can install in the upper end of mounting bracket 11 with the horizontally folding mode.
In this embodiment, through starting second drive arrangement 22, make it drive driving gear 23 and rotate together with driven gear 24, and then drive lead screw 27 and rotate in fixing base 28's inboard to drive link 26 and slide along the axial direction of lead screw 27 on lead screw 27, and then lifting adjustment frame 25, when unmanned aerial vehicle carries out the official business in the sky, can effectively adjust muzzle position through controlling second drive arrangement 22, the effectual flexibility of having improved this application, practicality.
The limiting block 29 is rotatably connected to the outer side of the screw rod 27 and located between the connecting frame 26 and the fixing seat 28, so that the limiting effect is effectively achieved.
Referring to fig. 1-2, the connecting plate 3 is fixedly installed at the upper end of the adjusting seat 21, the whole connecting plate 3 is of a rectangular planar plate structure, and the upper end face of the connecting plate 3 is fixedly connected with the lower end of the unmanned aerial vehicle.
The working principle of the embodiment is as follows: the staff passes through the bolt spiro union with the stock position of 79 submachine rifle at the lower extreme of connecting seat 12 to set up fixed orifices 19 on through first lateral wall 13, second lateral wall 14 and further fix it, make the trigger position and the connecting rod 17 butt of firearms, the staff can drive driving gear 23 and rotate in step along with driven gear 24 through second drive arrangement 22 subaerial, thereby adjust muzzle position, also can adjust the muzzle position through control second drive arrangement 22 in the sky, rethread connecting plate 3 is whole to the unmanned aerial vehicle lower extreme with installing unit 1, adjusting unit 2 and firearms, carry out the task, this application simple structure, convenient operation, a dedicated unmanned aerial vehicle bracket to 79 submachine rifle is favorable to mountain region, jungle, short weapon meet, city battle and rescue personnel's fight.
It will be evident to those skilled in the art that the utility model is not limited to the details of the foregoing illustrative embodiments, and that the present utility model may be embodied in other specific forms without departing from the spirit or essential characteristics thereof. The present embodiments are therefore to be considered in all respects as illustrative and not restrictive, the scope of the utility model being indicated by the appended claims rather than by the foregoing description, and all changes which come within the meaning and range of equivalency of the claims are therefore intended to be embraced therein.
The above-described embodiments merely represent embodiments of the utility model, the scope of the utility model is not limited to the above-described embodiments, and it is obvious to those skilled in the art that several variations and modifications can be made without departing from the spirit of the utility model, which are all within the scope of the utility model.
Claims (10)
1. An unmanned aerial vehicle firearm support, characterized in that: including installation unit (1), installation unit (1) includes mounting bracket (11), the lower extreme fixedly connected with connecting seat (12) of mounting bracket (11), connecting seat (12) are equipped with two sections and are connected jointly with the stock, the lower extreme one side fixed mounting of mounting bracket (11) has first drive arrangement (15), the output of first drive arrangement (15) passes second lateral wall (14) and extends to the inboard of mounting bracket (11) and firearm trigger looks joint.
2. An unmanned aerial vehicle firearm carrier according to claim 1, wherein: the installation unit (1) upper end fixedly connected with adjusting unit (2), adjusting unit (2) are including adjusting seat (21), adjust seat (21) fixed connection in the upper end of mounting bracket (11), the outside fixedly connected with second drive arrangement (22) of adjusting seat (21), the front end of adjusting seat (21) is close to the position rotation of second drive arrangement (22) and is connected with driving gear (23), the output of second drive arrangement (22) is connected with driving gear (23).
3. An unmanned aerial vehicle firearm carrier according to claim 2, wherein: the adjusting unit (2) further comprises a fixing seat (28), the fixing seat (28) is fixedly arranged at the tail end of the upper end of the mounting frame (11), one side, far away from the second driving device (22), of the driving gear (23) is meshed with a driven gear (24), the circle center of the driven gear (24) is fixedly connected with a screw rod (27), and the tail end of the screw rod (27) is rotationally connected with the fixing seat (28).
4. A unmanned aerial vehicle firearm carrier according to claim 3, wherein: the middle section outside of lead screw (27) has movably cup jointed link (26), the both sides of link (26) all articulate have alignment jig (25), the one end that link (26) was kept away from to alignment jig (25) is connected with the inner chamber of mounting bracket (11).
5. The unmanned aerial vehicle firearm carrier of claim 4, wherein: the outside of the screw rod (27) is positioned between the connecting frame (26) and the fixed seat (28) and is movably sleeved with a limiting block (29).
6. An unmanned aerial vehicle firearm carrier according to claim 1, wherein: the lower extreme one side of mounting bracket (11) is connected with second lateral wall (14), first drive arrangement (15) fixed mounting is in the outside of second lateral wall (14), and the lower extreme of mounting bracket (11) is connected with first lateral wall (13) with the opposite one side of second lateral wall (14), be hollow out construction on first lateral wall (13), second lateral wall (14).
7. The unmanned aerial vehicle firearm carrier of claim 6, wherein: a plurality of fixing holes (19) are formed in the first side wall (13) and the second side wall (14).
8. An unmanned aerial vehicle firearm carrier according to claim 1, wherein: the output end of the first driving device (15) penetrates through the second side wall (14) and extends to the inner cavity of the mounting frame (11) to be fixedly connected with a rotating handle (16), and one side, facing the first side wall (13), of the free end of the rotating handle (16) is fixedly connected with a connecting rod (17).
9. An unmanned aerial vehicle firearm carrier according to claim 1, wherein: the front end of the second side wall (14) is connected with an integrally formed bullet blocking plate (18), and the bullet blocking plate (18) is of a folding edge structure.
10. An unmanned aerial vehicle firearm carrier according to claim 2, wherein: the upper end fixedly connected with connecting plate (3) of adjusting unit (2), installation unit (1), adjusting unit (2) are all through connecting plate (3) and unmanned aerial vehicle lower extreme fixed connection.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202321570309.5U CN220483552U (en) | 2023-06-16 | 2023-06-16 | Unmanned aerial vehicle gun mechanical bracket |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202321570309.5U CN220483552U (en) | 2023-06-16 | 2023-06-16 | Unmanned aerial vehicle gun mechanical bracket |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN220483552U true CN220483552U (en) | 2024-02-13 |
Family
ID=89826952
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202321570309.5U Active CN220483552U (en) | 2023-06-16 | 2023-06-16 | Unmanned aerial vehicle gun mechanical bracket |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN220483552U (en) |
-
2023
- 2023-06-16 CN CN202321570309.5U patent/CN220483552U/en active Active
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| GR01 | Patent grant |