CN210212243U - Vehicular unmanned aerial vehicle of fast loading and unloading counter-braking equipment - Google Patents
Vehicular unmanned aerial vehicle of fast loading and unloading counter-braking equipment Download PDFInfo
- Publication number
- CN210212243U CN210212243U CN201920925182.1U CN201920925182U CN210212243U CN 210212243 U CN210212243 U CN 210212243U CN 201920925182 U CN201920925182 U CN 201920925182U CN 210212243 U CN210212243 U CN 210212243U
- Authority
- CN
- China
- Prior art keywords
- unmanned aerial
- aerial vehicle
- limiting
- supporting seat
- vehicle reverse
- 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.)
- Active
Links
Images
Landscapes
- Forklifts And Lifting Vehicles (AREA)
Abstract
The utility model relates to an unmanned aerial vehicle system of turning over technical field just discloses a quick loading and unloading's vehicular unmanned aerial vehicle system of turning over equipment, including supporting seat and bottom plate, the perpendicular welding in supporting seat top middle part has adapter sleeve, the cover has the spacing lantern ring on the adapter sleeve outer wall, the welding has spring B between spacing lantern ring bottom and the supporting seat top, the spacing groove has been seted up on the spacing lantern ring inner wall, spacing inslot chamber is provided with the stopper, stopper through connection sleeve, the adapter sleeve inner chamber has inserted the spliced pole perpendicularly, spherical draw-in groove has been seted up at the spliced pole top. The utility model discloses for the mounting means and the structure of traditional unmanned aerial vehicle reverse system rifle, this device makes the installation of unmanned aerial vehicle reverse system rifle more convenient with the dismantlement, greatly reduced the installation dismantlement time of unmanned aerial vehicle reverse system rifle, reduced staff's the installation dismantlement degree of difficulty.
Description
Technical Field
The utility model relates to an unmanned aerial vehicle counter-system technical field especially relates to a quick loading and unloading's vehicular unmanned aerial vehicle counter-system equipment.
Background
Unmanned aerial vehicle reflexes system, including antenna, interfering signal generator, electrical source controller, interfering signal generator comprises a plurality of different wave band interfering signal emission module, interfering signal generation module, directional panel antenna pass through the signal transmission feeder connect in interfering signal generation module.
Chinese patent number is cn201721673449. x's utility model discloses a quick loading and unloading's vehicular unmanned aerial vehicle system of turning over makes equipment, include the mount pad with vehicle body screw connection, and the top of mount pad is fixed with places the piece, the top of placing the piece is equipped with the rectangle standing groove, and has cup jointed the cavity base in the rectangle standing groove, the top of cavity base is fixed with the bracing piece that the symmetry set up, and the top of bracing piece is fixed with the cloud platform main part, and the top of cloud platform main part is equipped with the unmanned aerial vehicle system of turning over rifle main part, the inboard of cavity base is equipped with fixed knot and constructs. The utility model discloses a cooperation of portable pole, reel, acting as go-between, cavity stopper, cavity fixture block, spring and stand pipe isotructure is used, not only makes whole equipment convenient to carry, simultaneously, only needs to rotate the knob ring, can take out the cavity fixture block from the draw-in groove, and then makes whole unmanned aerial vehicle reverse system rifle main part can easily dismantle get off, need not to use multiple instrument, and then makes to change and maintenance efficiency height, uses in a flexible way.
But the device still has the problem of inconvenient installation and disassembly in the process of actual use.
SUMMERY OF THE UTILITY MODEL
The utility model aims at solving the problem that the installation of the unmanned aerial vehicle reverse gun among the prior art is dismantled and is convenient inadequately, and the vehicular unmanned aerial vehicle reverse equipment of a fast loading and unloading who proposes.
In order to achieve the above purpose, the utility model adopts the following technical scheme:
the utility model provides a quick loading and unloading's vehicular unmanned aerial vehicle system of turning over equipment, includes supporting seat and bottom plate, the perpendicular welding in supporting seat top middle part has adapter sleeve, the cover has the spacing lantern ring on the adapter sleeve outer wall, the welding has spring B between spacing lantern ring bottom and the supporting seat top, the spacing groove has been seted up on the spacing lantern ring inner wall, spacing inslot chamber is provided with the stopper, the stopper runs through adapter sleeve, the adapter sleeve inner chamber has inserted the spliced pole perpendicularly, spherical draw-in groove has been seted up at the spliced pole top, the embedding of spherical draw-in groove inner chamber has the connecting bulb, the welding of connecting bulb top has a supporting bench, the supporting bench welds in unmanned aerial vehicle system rifle main part bottom, bottom plate top left and right sides symmetry is provided with.
Preferably, the left side and the right side of the supporting seat symmetrically penetrate through the limiting sliding rods vertically, the outer walls of the limiting sliding rods are wound with springs A, and the springs A are located between the supporting seat and the bottom plate.
Preferably, two sets of all through hinge and bottom plate swing joint bottom the protecting crust, the unmanned aerial vehicle reverse system rifle main part is located two sets of protecting crust inner chambers.
Preferably, rubber pads are symmetrically adhered to the opposite sides of the two groups of protective shells.
Preferably, sponge pads are symmetrically adhered to the inner walls of the two groups of opposite sides of the protective shells.
Preferably, it is two sets of pivot and spacing knot have been welded respectively at the protecting crust top, the pivot runs through gag lever post left side middle part, in the gag lever post right side card was gone into spacing knot, spacing knot is the L type with the gag lever post.
Compared with the prior art, the utility model provides a quick loading and unloading's vehicular unmanned aerial vehicle counter-system equipment possesses following beneficial effect:
1. this quick loading and unloading's vehicular unmanned aerial vehicle system equipment of turning over, through the adapter sleeve ring, the setting of spliced pole and adapter sleeve, press down the adapter sleeve ring, then insert the spliced pole in the adapter sleeve inner chamber, then loosen the adapter sleeve ring, spring B promotes the adapter sleeve ring and rises, the in-process spacing groove that the adapter sleeve ring rises drives the stopper and inserts the adapter sleeve inner chamber, make in the draw-in groove on the stopper embedding spliced pole, just can accomplish the installation of unmanned aerial vehicle system rifle main part, the above-mentioned step of reverse operation, just can demolish unmanned aerial vehicle system rifle main part, installation mode and structure for traditional unmanned aerial vehicle system rifle are turned over, this device makes the installation of unmanned aerial vehicle system rifle more convenient with the dismantlement, greatly reduced the installation dismantlement time of unmanned aerial vehicle system rifle, staff's the installation dismantlement degree of.
2. This quick loading and unloading's vehicular unmanned aerial vehicle system of turning over makes equipment, through the setting of ball groove and connection bulb, when using unmanned aerial vehicle system of turning over rifle main part, connect the bulb and can rotate at the ball groove inner chamber, and then make unmanned aerial vehicle system of turning over rifle main part can be more nimble when using.
3. This quick loading and unloading's vehicular unmanned aerial vehicle system equipment of turning over, through the setting of protecting crust, when unmanned aerial vehicle system rifle main part does not use, the protecting crust can effectually protect unmanned aerial vehicle system rifle main part, avoids unmanned aerial vehicle system rifle main part to receive the erosion that blows, drenches, insolate, has reduced the depreciation speed of unmanned aerial vehicle system rifle main part, the effectual life who prolongs unmanned aerial vehicle system rifle main part.
4. This quick loading and unloading's vehicular unmanned aerial vehicle system of turning back equipment, through spring A's setting, the in-process that removes when the automobile body can inevitably produce the vibration, spring A just can effectually carry out the buffering filter to the vibration this moment, avoids the vibration direct transmission to give unmanned aerial vehicle system of turning back rifle main part, causes unmanned aerial vehicle system of turning back rifle main part inner structure's damage, and then the effectual life who prolongs unmanned aerial vehicle system of turning back rifle main part.
5. This quick loading and unloading's vehicular unmanned aerial vehicle system equipment of turning over, through the setting of foam-rubber cushion, when two sets of protecting crust closed, the foam-rubber cushion on two sets of protecting crust inner walls was cliied unmanned aerial vehicle system rifle main part, when the vehicle turned to or took place to rock, the foam-rubber cushion can effectually be protected unmanned aerial vehicle system rifle main part, avoided unmanned aerial vehicle system rifle main part to collide the damage that leads to with the protecting crust.
And the part that does not relate to among the device all is the same with prior art or can adopt prior art to realize, the utility model discloses can the inconvenient problem of vehicular unmanned aerial vehicle reverse system rifle installation of effectual solution.
Drawings
Fig. 1 is a front sectional view of a vehicular unmanned aerial vehicle reverse braking device for rapid loading and unloading according to the present invention;
fig. 2 is a front view of a vehicular unmanned aerial vehicle reverse braking device for fast loading and unloading according to the present invention;
fig. 3 is a left side view of a vehicular unmanned aerial vehicle reverse braking device for fast loading and unloading provided by the present invention;
fig. 4 is a front sectional view of a support seat, a connecting sleeve and a connecting column of a vehicle-mounted type unmanned aerial vehicle reverse braking device which is quickly assembled and disassembled;
fig. 5 is a top view of a stop lever of a vehicle-mounted type unmanned aerial vehicle reverse braking device for quick loading and unloading according to the present invention;
fig. 6 is the utility model provides a quick loading and unloading's vehicle-mounted unmanned aerial vehicle counter-system equipment's spacing knot right side view.
In the figure: hinge 1, bottom plate 2, spring A3, spacing slide bar 4, stopper 5, adapter sleeve 6, brace table 7, unmanned aerial vehicle reverse system rifle main part 8, rubber pad 9, protecting crust 10, foam-rubber cushion 11, connect bulb 12, spliced pole 13, spacing lantern ring 14, spring B15, supporting seat 16, bolt hole 17, spacing groove 18, spherical draw-in groove 19, gag lever post 20, pivot 21, spacing knot 22.
Detailed Description
The technical solutions in the embodiments of the present invention will be described clearly and completely with reference to the accompanying drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only some embodiments of the present invention, not all embodiments.
In the description of the present invention, it is to be understood that the terms "upper", "lower", "front", "rear", "left", "right", "top", "bottom", "inner", "outer", and the like indicate orientations or positional relationships based on the orientations or positional relationships shown in the drawings, and are only for convenience of description and simplicity of description, and do not indicate or imply that the device or element being referred to must have a particular orientation, be constructed and operated in a particular orientation, and therefore, should not be construed as limiting the present invention.
Referring to fig. 1-6, a vehicular unmanned aerial vehicle of fast loading and unloading system equipment that turns over, including supporting seat 16 and bottom plate 2, the perpendicular welding in the middle part of supporting seat 16 top has adapter sleeve 6, the cover has spacing lantern ring 14 on the adapter sleeve 6 outer wall, the welding has spring B15 between spacing lantern ring 14 bottom and the supporting seat 16 top, spacing groove 18 has been seted up on spacing lantern ring 14 inner wall, spacing groove 18 inner chamber is provided with stopper 5, stopper 5 runs through adapter sleeve 6, spliced pole 13 has been inserted perpendicularly to adapter sleeve 6 inner chamber, spherical draw-in groove 19 has been seted up at spliced pole 13 top, spherical draw-in groove 19 inner chamber embedding has connecting bulb 12, connecting bulb 12 top welding has brace table 7, brace table 7 welds in the 8 bottoms of unmanned aerial vehicle system rifle main part, 2 top left and right sides symmetry of bottom plate are.
The left side and the right side of the supporting seat 16 are symmetrically and vertically penetrated with a limiting slide bar 4, the outer wall of the limiting slide bar 4 is wound with a spring A3, and a spring A3 is positioned between the supporting seat 16 and the bottom plate 2.
Two sets of protecting crust 10 bottoms are all through hinge 1 and 2 swing joint of bottom plate, and unmanned aerial vehicle reverse system rifle main part 8 is located two sets of protecting crust 10 inner chambers.
The top of two sets of protective housing 10 has welded pivot 21 and stop buckle 22 respectively, and pivot 21 runs through gag lever post 20 left side middle part, and in the stop buckle 22 was gone into to gag lever post 20 right side card, stop buckle 22 and gag lever post 20 were the L type.
In the utility model, when in use, the limiting rod 20 is rotated to rotate the limiting rod 20 out of the limiting buckle 22, then the protective shell 10 can be opened towards two sides, then the unmanned aerial vehicle reverse gun main body 8 can be used, when the unmanned aerial vehicle reverse gun main body 8 is installed, the connecting sleeve ring 14 is pressed downwards, then the connecting column 13 is inserted into the inner cavity of the connecting sleeve 6, then the connecting sleeve ring 14 is loosened, the spring B15 pushes the connecting sleeve ring 14 to rise, the limiting groove 18 drives the limiting block 5 to be inserted into the inner cavity of the connecting sleeve 6 in the rising process of the connecting sleeve ring 14, so that the limiting block 5 is embedded into the clamping groove on the connecting column 13, the installation of the unmanned aerial vehicle reverse gun main body 8 can be completed, the steps are operated reversely, the unmanned aerial vehicle reverse gun main body 8 can be dismantled, compared with the installation mode and the structure of the traditional unmanned aerial vehicle reverse gun, the device makes the installation and the dismantling of the, greatly reducing the installation and disassembly time of the unmanned aerial vehicle reverse lance, reducing the installation and disassembly difficulty of workers, through the arrangement of the spherical clamping groove 19 and the connecting ball head 12, when the unmanned aerial vehicle reverse lance main body 8 is used, the connecting ball head 12 can rotate in the inner cavity of the spherical clamping groove 19, further leading the unmanned aerial vehicle reverse lance main body 8 to be more flexible when in use, when the unmanned aerial vehicle reverse lance main body 8 is not used, the protective shell 10 can effectively protect the unmanned aerial vehicle reverse lance main body 8, avoiding the unmanned aerial vehicle reverse lance main body 8 from being eroded by wind, rain and sunshine, reducing the depreciation speed of the unmanned aerial vehicle reverse lance main body 8, effectively prolonging the service life of the unmanned aerial vehicle reverse lance main body 8, and when a vehicle body moves, the vibration can be generated inevitably, at the moment, the spring A3 can effectively buffer and filter the vibration, avoiding the direct transmission to the unmanned aerial vehicle reverse lance main body 8, cause the damage of 8 inner structures of unmanned aerial vehicle reverse system rifle main part, and then the effectual life who prolongs the unmanned aerial vehicle reverse system rifle main part 8, and when two sets of protecting crust 10 were closed, the foam-rubber cushion 11 on two sets of protecting crust 10 inner walls was cliied unmanned aerial vehicle reverse system rifle main part 8, when the vehicle turned to or took place to rock, foam-rubber cushion 11 can effectually protect unmanned aerial vehicle reverse system rifle main part 8, avoid the damage that unmanned aerial vehicle reverse system rifle main part 8 and protecting crust 10 bump lead to.
The above, only be the concrete implementation of the preferred embodiment of the present invention, but the protection scope of the present invention is not limited thereto, and any person skilled in the art is in the technical scope of the present invention, according to the technical solution of the present invention and the utility model, the concept of which is equivalent to replace or change, should be covered within the protection scope of the present invention.
Claims (6)
1. The vehicle-mounted unmanned aerial vehicle reverse-braking device capable of being rapidly assembled and disassembled comprises a supporting seat (16) and a bottom plate (2), and is characterized in that a connecting sleeve (6) is perpendicularly welded in the middle of the top end of the supporting seat (16), a limiting sleeve ring (14) is sleeved on the outer wall of the connecting sleeve (6), a spring B (15) is welded between the bottom of the limiting sleeve ring (14) and the top of the supporting seat (16), a limiting groove (18) is formed in the inner wall of the limiting sleeve ring (14), a limiting block (5) is arranged in the inner cavity of the limiting groove (18), the limiting block (5) penetrates through the connecting sleeve (6), a connecting column (13) is vertically inserted into the inner cavity of the connecting sleeve (6), a spherical clamping groove (19) is formed in the top of the connecting column (13), a connecting ball head (12) is embedded into the inner, brace table (7) weld in unmanned aerial vehicle reverse system rifle main part (8) bottom, bottom plate (2) top left and right sides symmetry is provided with protecting crust (10).
2. The vehicular unmanned aerial vehicle of claim 1, wherein the support base (16) is provided with a limiting slide rod (4) symmetrically and vertically penetrating the left side and the right side of the support base, a spring A (3) is wound on the outer wall of the limiting slide rod (4), and the spring A (3) is positioned between the support base (16) and the bottom plate (2).
3. The vehicle-mounted rapid loading and unloading unmanned aerial vehicle reverse-braking device according to claim 1, wherein the bottoms of the two sets of protective shells (10) are movably connected with the bottom plate (2) through hinges (1), and the unmanned aerial vehicle reverse-braking gun main body (8) is positioned in the inner cavities of the two sets of protective shells (10).
4. A fast loading and unloading vehicular unmanned aerial vehicle counteraction apparatus according to claim 1, wherein rubber pads (9) are symmetrically adhered to the opposite sides of the two sets of protective shells (10).
5. The vehicular unmanned aerial vehicle counteraction apparatus of claim 1, wherein sponge pads (11) are symmetrically adhered to the inner walls of the two sets of protection shells (10) at the opposite sides.
6. The vehicle-mounted unmanned aerial vehicle reverse braking device capable of being rapidly mounted and dismounted as claimed in claim 1, wherein a rotating shaft (21) and a limiting buckle (22) are respectively welded to the tops of two groups of protective shells (10), the rotating shaft (21) penetrates through the middle of the left side of a limiting rod (20), the right side of the limiting rod (20) is clamped into the limiting buckle (22), and the limiting buckle (22) and the limiting rod (20) are L-shaped.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201920925182.1U CN210212243U (en) | 2019-06-19 | 2019-06-19 | Vehicular unmanned aerial vehicle of fast loading and unloading counter-braking equipment |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201920925182.1U CN210212243U (en) | 2019-06-19 | 2019-06-19 | Vehicular unmanned aerial vehicle of fast loading and unloading counter-braking equipment |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN210212243U true CN210212243U (en) | 2020-03-31 |
Family
ID=69932892
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201920925182.1U Active CN210212243U (en) | 2019-06-19 | 2019-06-19 | Vehicular unmanned aerial vehicle of fast loading and unloading counter-braking equipment |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN210212243U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN116902246A (en) * | 2023-09-12 | 2023-10-20 | 成都庆龙航空科技有限公司 | Unmanned aerial vehicle investigation recognition device |
-
2019
- 2019-06-19 CN CN201920925182.1U patent/CN210212243U/en active Active
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN116902246A (en) * | 2023-09-12 | 2023-10-20 | 成都庆龙航空科技有限公司 | Unmanned aerial vehicle investigation recognition device |
| CN116902246B (en) * | 2023-09-12 | 2023-12-12 | 成都庆龙航空科技有限公司 | Unmanned aerial vehicle investigation recognition device |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN210212243U (en) | Vehicular unmanned aerial vehicle of fast loading and unloading counter-braking equipment | |
| CN111022880B (en) | Fixing device for electrical signal equipment | |
| CN112427806A (en) | Novel combined dust removal device for laser welding of power battery module | |
| CN111313352B (en) | Cable fixed connection device | |
| CN211010472U (en) | Special support for media shooting equipment | |
| CN207683718U (en) | A kind of marine air installation system | |
| CN115754572A (en) | Multifunctional charging pile detection equipment and method thereof | |
| CN206010193U (en) | A kind of robot soldering pliers apparatus for placing | |
| CN216306065U (en) | Air exhausting device for centrifugal ventilation valve of aircraft engine | |
| CN214057904U (en) | Foldable perpendicular unmanned aerial vehicle that throws bullet | |
| KR20110111728A (en) | Movable gunshot test device | |
| CN201462439U (en) | Portable lighting device for urethane foam gap filler ejection gun | |
| CN212989640U (en) | Multi-channel ground penetrating radar system | |
| CN206944826U (en) | The launching tube angle adjustment mechanism of saving casting device | |
| CN207687674U (en) | A kind of ship air bottle mounting structure | |
| CN209350270U (en) | Manipulator pulldown takes the fixed device of tire | |
| CN207683717U (en) | A kind of ship air bottle fixed structure | |
| CN215922583U (en) | Unmanned aerial vehicle airborne mobile phone support for field investigation and evidence demonstration and charging fixing mechanism thereof | |
| CN201670353U (en) | Far-distant life-saving throwing device | |
| CN213589591U (en) | Compressed air foam nozzle for high-risk complex environment | |
| CN219915677U (en) | But electric power detects with angle regulation's cable tester | |
| CN215117911U (en) | Electromechanical device installation and maintenance comprehensive practical training platform | |
| CN219382838U (en) | Positioning charging male and female seat for unmanned aerial vehicle | |
| CN218329586U (en) | Laser destroying device | |
| CN213712708U (en) | LED lamp with adjustable color temperature and low loss |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant |