CN215753056U - Unmanned aerial vehicle radar hoist device - Google Patents
Unmanned aerial vehicle radar hoist device Download PDFInfo
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- CN215753056U CN215753056U CN202122319317.XU CN202122319317U CN215753056U CN 215753056 U CN215753056 U CN 215753056U CN 202122319317 U CN202122319317 U CN 202122319317U CN 215753056 U CN215753056 U CN 215753056U
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Abstract
The utility model discloses an unmanned aerial vehicle radar hoisting device which comprises a bottom plate, a top plate, a left connecting plate and a right connecting plate, wherein the bottom plate is fixedly connected with the top of a radar, the top plate is positioned above the bottom plate and is connected with the bottom plate through a plurality of flexible components which are uniformly arranged at intervals, the plate surfaces of the left connecting plate and the right connecting plate are vertical, screw holes for fixedly connecting with a mounting plate on a body of an unmanned aerial vehicle are formed in the plate surfaces of the left connecting plate and the right connecting plate, horizontal connecting lugs are correspondingly arranged on the side surfaces, parallel to each other, opposite to each other, of the left connecting plate and the right connecting plate, and the left side and the right side of the top plate are respectively detachably connected with the horizontal connecting lugs of the left connecting plate and the right connecting plate through a plurality of quick-dismounting connecting assemblies. The device has the advantages that the top plate and the left and right connecting plates of the device are connected through the quick-release connecting assembly, so that the radar and the unmanned aerial vehicle can be quickly assembled and disassembled, and the operations such as maintenance, replacement and the like are convenient and fast; gaps are formed among the top of the radar, the bottom plate and the top plate, airflow flowing is facilitated, and the heat dissipation effect is good.
Description
Technical Field
The utility model belongs to the field of unmanned aerial vehicle radar installation accessories, and particularly relates to an unmanned aerial vehicle radar hoisting device.
Background
Set up the radar on unmanned aerial vehicle's fuselage, can effectively promote unmanned aerial vehicle and keep away the barrier function. In addition, carry on the radar that possesses corresponding function after, use unmanned aerial vehicle can also acquire high accuracy point cloud space three-dimensional information, carry out functions such as survey and drawing, geological disaster discernment, geological disaster area deformation monitoring fast.
During unmanned aerial vehicle fuselage hoist and mount radar among the prior art, use the mount of taking the bolt to connect usually, though can realize more firm fixed, nevertheless also have following not enough: the quick assembly and disassembly cannot be realized, and the efficiency of installation, replacement and maintenance is low; the radar is in rigid connection with the fixing frame, the anti-seismic performance and the impact resistance are poor, and the radar is tightly attached to the machine body to influence the heat dissipation performance.
SUMMERY OF THE UTILITY MODEL
The utility model aims to provide an unmanned aerial vehicle radar hoisting device, aiming at overcoming the defects in the prior art.
The technical scheme for solving the technical problems is as follows: the utility model provides an unmanned aerial vehicle radar hoist device, its includes bottom plate, roof, the even board in a left side and the board in the right side, bottom plate and radar top fixed connection, the roof is located the bottom plate top is connected with the bottom plate through the flexible assembly that a plurality of even intervals set up, the screw that is used for with mounting panel fixed connection on the unmanned aerial vehicle fuselage is all offered on the even board in a left side and the board in the right side vertical and face of even board, the even board in a left side and the right side are parallel to each other and correspond on the relative side and are equipped with the horizontally connect ear, the roof left and right sides respectively through a plurality of quick detach coupling assembling correspond with the even board in a left side and the right side horizontally connect ear can dismantle the connection.
On the basis of the technical scheme, the utility model can be further improved as follows.
Further, the flexible assembly includes a top fixed block and a bottom fixed block, fixed connection is carried out through four equal length and evenly spaced lifting ropes circumferentially between the top fixed block and the bottom fixed block, the center of top fixed block and bottom fixed block all is equipped with the fixed orifices, top fixed block and bottom fixed block are respectively through running through the bolt of fixed orifices with roof and bottom plate correspond fixed connection.
The radar shell has the beneficial effects of simple structure, easiness in processing, low cost and better flexibility, and reduces the transmission of rigid vibration to the radar shell by vibration parts such as a machine body engine and the like which are easy to generate.
Further, the top fixing block and the bottom fixing block are both square blocks, and the lifting rope is a steel wire.
The beneficial effects of adopting above-mentioned further scheme are that, the installation of being convenient for, the material is easy and intensity is good and not fragile.
Furthermore, the quick-release connecting assembly comprises a clamping claw part and a bolt part, wherein hook-shaped clamping claws with opposite openings are arranged on the clamping claw part in pairs, movable pins which move in the horizontal direction under the driving of the pressing handle are arranged on the bolt part, and the movable pins are respectively corresponding to a locking connection state and an unlocking removal state when inserted into the openings of the hook-shaped clamping claws or moved out of the openings of the hook-shaped clamping claws.
The beneficial effect who adopts above-mentioned further scheme is, simple structure, and the dismouting is very convenient.
Furthermore, the clamping claw part is fixed on the horizontal connecting lug, the plug pin part is fixed on the bottom surface of the top plate, the top surface of the clamping claw part is provided with a convex column which extends upwards, a counter bore which is correspondingly matched with the convex column is arranged on the bottom surface of the plug pin part, the hook-shaped clamping claws are arranged on the clamping claw part in a front-back opposite mode, and the pressing handle and the movable pin are arranged on the plug pin part in a front-back opposite mode.
The convex column is matched with the counter bore, so that the acting force of the relative movement of the clamping claw part and the plug pin part in the horizontal direction on the movable pin and the hook-shaped clamping claw can be well resisted.
Furthermore, through holes for the radar antenna to extend upwards are oppositely arranged on the bottom plate and the top plate.
The beneficial effect of adopting above-mentioned further scheme is, easy to assemble radar antenna, the suitability is good.
Furthermore, the bottom plate, the top plate, the left connecting plate and the right connecting plate are all provided with hollow holes for reducing weight.
Adopt above-mentioned further scheme's beneficial effect be, light in weight alleviates the load to unmanned aerial vehicle.
Furthermore, the number of the flexible assemblies and the number of the quick-release connecting assemblies are four.
The beneficial effect who adopts above-mentioned further scheme is that, the four corners distributes, connects firmly, and stability is good.
Compared with the prior art, the utility model has the technical effects and advantages that:
the top plate and the left and right connecting plates of the device are connected through a quick-release connecting assembly, the left and right connecting plates are connected with the unmanned aerial vehicle body, and the top plate is connected with the radar through a bottom plate below the top plate, so that the radar and the unmanned aerial vehicle can be quickly disassembled and assembled, and the operations of maintenance, replacement and the like are convenient and fast; the bottom plate and the top plate are connected through the flexible assembly, the machine body can be weakened to a certain degree to transmit vibration of the radar, meanwhile, gaps are formed between the top of the radar and the bottom plate and between the top plate and the bottom plate, airflow flowing is facilitated, and the heat dissipation effect is good.
Drawings
Fig. 1 is an axonometric view of an unmanned aerial vehicle radar hoisting device provided by the utility model;
fig. 2 is a front view of the unmanned aerial vehicle radar lifting device shown in fig. 1;
fig. 3 is a side view of the drone radar hoist shown in fig. 1;
fig. 4 is a schematic view of the quick release connection assembly of the left and right link plates of the radar lifting device of the unmanned aerial vehicle shown in fig. 1 in an unlocked state;
figure 5 is an isometric view of the flexible components of the unmanned aerial vehicle radar lifting device shown in figure 1;
fig. 6 is an axonometric view of the unmanned aerial vehicle radar lifting device shown in fig. 1 after the left side plate, the horizontal connecting lug and the quick-release connecting assembly are assembled.
In the drawings, the components represented by the respective reference numerals are listed below:
1. a base plate; 2. a top plate; 3. a left connecting plate; 4. a right connecting plate; 5. a radar; 6. a horizontal connecting lug; 7. Pushing the fixed block; 8. a bottom fixed block; 9. a lifting rope; 10. a hook-shaped claw; 11. a movable pin; 12. pressing the handle; 13. a convex column.
Detailed Description
The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only a part of the embodiments of the present invention, and not all of the embodiments. All other embodiments, which can be derived by a person skilled in the art from the embodiments given herein without making any creative effort, shall fall within the protection scope of the present invention.
In the description of the present invention, if terms indicating orientation such as "upper", "lower", "left", "right", "top", "bottom", "inner", "outer", etc., are used, they indicate orientation or positional relationship based on that shown in the drawings, and are only for convenience of description and simplicity of description, but do not indicate or imply that the device or element being referred to must have a particular orientation, be constructed in a particular orientation, and be operated, and thus, should not be construed as limiting the present invention.
As shown in fig. 1 to 6, the utility model provides an unmanned aerial vehicle radar hoisting device, which comprises a bottom plate 1, a top plate 2, a left connecting plate 3 and a right connecting plate 4, wherein the top of the bottom plate 1 is fixedly connected with the top of a radar 5, the top plate 2 is positioned above the bottom plate 1 and is connected with the bottom plate 1 through a plurality of flexible components which are uniformly arranged at intervals, the plate surfaces of the left connecting plate 3 and the right connecting plate 4 are vertical, screw holes for fixedly connecting with a mounting plate on an unmanned aerial vehicle body are formed in the plate surfaces of the left connecting plate 3 and the right connecting plate 4, horizontal connecting lugs 6 are correspondingly arranged on the side surfaces of the left connecting plate 3 and the right connecting plate 4 which are parallel to each other and opposite to each other, and the left side and the right side of the top plate 2 are correspondingly detachably connected with the horizontal connecting lugs 6 of the left connecting plate 3 and the right connecting plate 4 through a plurality of quick-release connecting components.
It should be noted that this radar hoist device can be connected with the cooperation of unmanned aerial vehicle fuselage bottom, and unmanned aerial vehicle fuselage bottom is preset with about even board pass through the mounting panel of bolt fastening.
In an embodiment of the present invention, the flexible assembly includes a top fixing block 7 and a bottom fixing block 8, the top fixing block 7 and the bottom fixing block 8 are fixedly connected through four lifting ropes 9 which are equal in length and are uniformly spaced in the circumferential direction, fixing holes are respectively formed in the centers of the top fixing block 7 and the bottom fixing block 8, and the top fixing block 7 and the bottom fixing block 8 are respectively and correspondingly and fixedly connected with the top plate 2 and the bottom plate 1 through bolts penetrating through the fixing holes.
It can be understood that a cake-shaped supporting foot (cushion block) can be correspondingly arranged on the lower surface of the corresponding area of the bottom plate and the bottom fixing plate, the through holes can be correspondingly arranged on the bottom plate and the cushion block, the bolt can penetrate through the bottom fixing block, the bottom plate and the supporting foot and then is fixedly connected with the top surface of the radar shell, so that the bottom plate is spaced apart from the top surface of the radar shell, the airflow can flow through the top plate of the radar shell, and the heat dissipation effect is good.
In one embodiment of the present invention, the top fixing block 7 and the bottom fixing block 8 are both square blocks, and the lifting rope 9 is a steel wire.
It is understood that the fixing block is not limited to be a square block, but may also be a round cake (cylinder), a round table or other structures capable of achieving similar functions.
In one embodiment of the utility model, the quick release connection assembly comprises a claw part and a bolt part, wherein hook-shaped claws 10 with opposite openings are arranged on the claw part in pairs, movable pins 11 which move in the horizontal direction under the driving of a pressing handle 12 are arranged on the bolt part, and the movable pins 11 correspond to a locking connection state and an unlocking removal state respectively when being inserted into the openings of the hook-shaped claws 10 or being moved out of the openings of the hook-shaped claws 10.
In one embodiment of the present invention, the claw part is fixed on the horizontal connecting lug 6, the plug pin part is fixed on the bottom surface of the top plate 2, the top surface of the claw part is provided with a convex column 13 extending upwards, the bottom surface of the plug pin part is provided with a counter bore correspondingly matched with the convex column 13, the hook-shaped claws 10 are arranged on the claw part in a front-back opposite manner, and the pressing handle 12 and the movable pin 11 are arranged on the plug pin part in a front-back opposite manner.
The quick-release connecting piece with the structure can also be used as a blade seat, the structure is simple, the clamping claw part and the bolt part are correspondingly connected with the top plate and the horizontal connecting lug through bolts, and a spring is arranged in the bolt part so that the pressing handle can reset after being compressed.
In one embodiment of the present invention, the bottom plate 1 and the top plate 2 are provided with through holes for the radar 5 antenna to protrude upwards.
In one embodiment of the utility model, the bottom plate 1, the top plate 2, the left connecting plate 3 and the right connecting plate 4 are all provided with hollowed holes for reducing weight.
In one embodiment of the present invention, the number of the flexible assemblies and the number of the quick-release connecting assemblies are four.
The utility model has the basic principle that a left connecting plate and a right connecting plate are firstly fixed on a mounting plate of an unmanned aerial vehicle body, a bottom plate is fixed with the top surface of a radar shell, a top plate is connected to the bottom plate through a flexible assembly, a claw part and a bolt part of each quick-release connecting assembly are correspondingly connected to the top surface of a horizontal connecting part and the bottom surface of the top plate respectively, a pressing handle is pressed to enable a movable pin to be positioned at a position which is easy to enter an opening of a hook-shaped claw, then the pressing handle is released, and the movable pin is reset to enter the hook-shaped claw, so that locking connection is realized. When the radar needs to be quickly detached from the machine body, the pressing handle is pressed to enable the movable pin to extend out of the opening of the hook-shaped clamping jaw, unlocking is achieved, and therefore the radar can be quickly detached.
Finally, it should be noted that: although the present invention has been described in detail with reference to the foregoing embodiments, it will be apparent to those skilled in the art that modifications may be made to the embodiments or portions thereof without departing from the spirit and scope of the utility model.
Claims (8)
1. The utility model provides an unmanned aerial vehicle radar hoist device, its characterized in that links board (3) and right side even board (4) including bottom plate (1), roof (2), a left side, bottom plate (1) and radar (5) top fixed connection, roof (2) are located bottom plate (1) top and through the flexible assembly of a plurality of even interval settings with be connected bottom plate (1), the left side links board (3) and the right side and all offers on the face vertical and the face of board (4) be used for with the mounting panel fixed connection's on the unmanned aerial vehicle fuselage screw, the left side links board (3) and the right side and links board (4) and to correspond on the side parallel to each other and relative and be equipped with horizontal connection ear (6), roof (2) the left and right sides respectively through a plurality of quick detach coupling assembling correspond with the left side links board (3) and the horizontal connection ear (6) of board (4) can dismantle the connection.
2. The unmanned aerial vehicle radar hoist device of claim 1, characterized in that, flexible assembly includes top fixed block (7) and end fixed block (8), carry out fixed connection through four isometric and circumference evenly spaced lifting ropes (9) between top fixed block (7) and the end fixed block (8), the center of top fixed block (7) and end fixed block (8) all is equipped with the fixed orifices, top fixed block (7) and end fixed block (8) respectively through running through the bolt of fixed orifices with roof (2) and bottom plate (1) correspond fixed connection.
3. The unmanned aerial vehicle radar lifting device of claim 2, wherein the top fixing block (7) and the bottom fixing block (8) are both square blocks, and the lifting rope (9) is a steel wire.
4. The unmanned aerial vehicle radar lifting device of claim 1, wherein the quick release connection assembly comprises a claw portion and a plug portion, hook-shaped claws (10) with opposite openings are arranged on the claw portion in pairs, movable pins (11) which move in the horizontal direction under the driving of a pressing handle (12) are arranged on the plug portion, and the movable pins (11) correspond to a locking connection state and an unlocking removal state respectively when being inserted into the openings of the hook-shaped claws (10) or being removed from the openings of the hook-shaped claws (10).
5. The unmanned aerial vehicle radar lifting device of claim 4, wherein the claw part is fixed on the horizontal connecting lug (6), the plug pin part is fixed on the bottom surface of the top plate (2), a convex column (13) extending upwards is arranged on the top surface of the claw part, a counter bore correspondingly matched with the convex column (13) is arranged on the bottom surface of the plug pin part, the hook-shaped claw (10) is arranged on the claw part in a front-back opposite mode, and the pressing handle (12) and the movable pin (11) are arranged on the plug pin part in a front-back opposite mode.
6. The unmanned aerial vehicle radar lifting device of claim 1, wherein the bottom plate (1) and the top plate (2) are relatively provided with through holes for the radar (5) antenna to extend upwards.
7. The unmanned aerial vehicle radar lifting device of any one of claims 1 to 6, wherein hollow holes for weight reduction are formed in the bottom plate (1), the top plate (2), the left connecting plate (3) and the right connecting plate (4).
8. The radar lifting device for unmanned aerial vehicles according to any one of claims 1 to 6, wherein the number of the flexible assemblies and the number of the quick-release connecting assemblies are four.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202122319317.XU CN215753056U (en) | 2021-09-24 | 2021-09-24 | Unmanned aerial vehicle radar hoist device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202122319317.XU CN215753056U (en) | 2021-09-24 | 2021-09-24 | Unmanned aerial vehicle radar hoist device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN215753056U true CN215753056U (en) | 2022-02-08 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202122319317.XU Active CN215753056U (en) | 2021-09-24 | 2021-09-24 | Unmanned aerial vehicle radar hoist device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN215753056U (en) |
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2021
- 2021-09-24 CN CN202122319317.XU patent/CN215753056U/en active Active
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