CN216468553U - Special unmanned aerial vehicle of education convenient to dismouting - Google Patents
Special unmanned aerial vehicle of education convenient to dismouting Download PDFInfo
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- CN216468553U CN216468553U CN202123020328.4U CN202123020328U CN216468553U CN 216468553 U CN216468553 U CN 216468553U CN 202123020328 U CN202123020328 U CN 202123020328U CN 216468553 U CN216468553 U CN 216468553U
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Abstract
The utility model discloses a special unmanned aerial vehicle of education convenient to dismouting in unmanned air vehicle technical field, including the organism, organism side fixedly connected with cantilever, cantilever lower extreme fixedly connected with motor, the play axle fixedly connected with screw of motor, organism lower extreme fixedly connected with camera, first connecting block and locking device, first connecting block lower extreme rotate and are connected with the bracing piece, bracing piece lower extreme fixedly connected with bottom plate, bottom plate upper end fixedly connected with buffer, the utility model discloses simple structure cost of manufacture is low, only needs simple operation just can be convenient for overhaul.
Description
Technical Field
The utility model relates to an unmanned air vehicle technique field specifically is a special unmanned aerial vehicle of education convenient to dismouting.
Background
Unmanned aerial vehicle is unmanned aerial vehicle for short, and is an unmanned aerial vehicle operated by radio remote control equipment and a self-contained program control device, or is completely or intermittently and autonomously operated by a vehicle-mounted computer, and in some education courses, courses using the unmanned aerial vehicle can be used to help to obtain data and courseware teaching materials.
However, the majority of existing unmanned aerial vehicles are all the integral type, when overhauing, be not convenient for carry out the dismouting, when connecting device takes place the harm like this, then can't maintain and replace, extravagant manpower and materials also increase maintenance duration simultaneously.
Therefore, the utility model provides a special unmanned aerial vehicle of education convenient to dismouting to solve the problem that the dismouting is not convenient for carry on to the traditional unmanned aerial vehicle integral type that proposes in the above-mentioned background art.
Disclosure of Invention
An object of the utility model is to provide a special unmanned aerial vehicle of education convenient to dismouting to solve the traditional unmanned aerial vehicle integral type that proposes in the above-mentioned background art and be not convenient for carry out the problem of dismouting.
In order to achieve the above object, the utility model provides a following technical scheme:
the utility model provides a special unmanned aerial vehicle of education convenient to dismouting, includes the organism, organism side fixedly connected with cantilever, cantilever lower extreme fixedly connected with motor, the play axle fixedly connected with screw of motor, organism lower extreme fixedly connected with camera, first connecting block and locking device, first connecting block lower extreme rotates and is connected with the bracing piece, bracing piece lower extreme fixedly connected with bottom plate, bottom plate upper end fixedly connected with buffer.
As a further aspect of the present invention: the terminal surface is seted up flutedly under the organism, sliding connection has the safety cover in the recess, the safety cover is transparent material, the camera is located inside the safety cover, and the during operation is installed the safety cover in the recess, just can reach the spacing to the safety cover like this under the effect of recess, can reach the protection to the camera simultaneously under the effect of safety cover.
As a further aspect of the present invention: buffer is including second connecting block, first baffle, damping telescopic link, first spring and third connecting block, bottom plate upper end fixedly connected with second connecting block, second connecting block upper end is rotated and is connected with the damping telescopic link, the one end that the second connecting block was kept away from to the damping telescopic link is rotated and is connected with the third connecting block, fixed connection between third connecting block and the organism, the during operation, when unmanned aerial vehicle whereabouts, when the bottom plate contacts ground, at this moment can push the bottom plate and remove, and then can make the damping telescopic link contract under the effect of second connecting block and third connecting block, just so can reach the purpose of buffering under the effect of damping telescopic link.
As a further aspect of the present invention: the damping telescopic link periphery fixedly connected with first baffle, the first spring of fixedly connected with between the first baffle, first spring is located the damping telescopic link outside, and the during operation when the damping telescopic link contracts, can reach the extrusion to first spring at this moment under the effect of first baffle, then the damping telescopic link of being convenient for resets under the effect of first spring.
As a further aspect of the present invention: the locking device comprises a fixed block, a handle, a clamping hole, a clamping rod, a second baffle, a circular groove and a second spring, the lower end of the machine body is fixedly connected with a fixed block, a circular groove is arranged in the fixed block, a second baffle plate is connected in the circular groove in a sliding manner, the second baffle is fixedly connected with a second spring which is fixedly connected with the inner wall of the circular groove, a clamping rod is rotationally connected in the second baffle, a handle is fixedly connected at the side end of the clamping rod, the clamping rod is connected with the fixed block in a sliding manner, when the protective cover is pushed to be inserted into the groove in work, the clamping rod is extruded at the moment, thereby achieving the compression of the second spring under the action of the second baffle plate, when the clamping rod is opposite to the clamping hole, at this time, the clamping rod can be clamped into the clamping hole under the action of the second spring, so that the protection cover can be fixed.
As a further aspect of the present invention: the safety cover side end face is seted up the card hole, block between card hole and the kelly, the one end that the kelly is close to the card hole has seted up the inclined plane, and the during operation is because the inclined plane has been seted up to the one end of kelly, is convenient for extrude the kelly like this and removes.
Advantageous effects
Compared with the prior art, the beneficial effects of the utility model are that:
under the matching of the fixed block, the handle, the clamping hole, the clamping rod, the second baffle plate, the circular groove and the second spring, when the protective cover needs to be disassembled, the handle is rotated to enable the inclined surface formed by the clamping rod to face the upper end, so that the protective cover is convenient to disassemble; when the safety cover is installed to needs, turning handle for the inclined plane that the kelly was seted up is towards the lower extreme, just is convenient for install the safety cover in the recess when installing the safety cover like this, has solved traditional unmanned aerial vehicle integral type and has not been convenient for carry out the problem of dismouting, great improvement maintenance efficiency.
Drawings
Fig. 1 is a schematic structural view of the present invention;
fig. 2 is an enlarged schematic structural view of a portion a in fig. 1 according to the present invention;
fig. 3 is a schematic structural view of a middle front view partial section of the present invention;
fig. 4 is an enlarged schematic structural diagram of a portion B in fig. 3 according to the present invention.
In the figure: 1-machine body, 2-cantilever, 3-propeller, 4-motor, 5-bottom plate, 6-support rod, 7-protective cover, 8-first connecting block, 9-buffer device, 901-second connecting block, 902-first baffle, 903-damping telescopic rod, 904-first spring, 905-third connecting block, 10-locking device, 1001-fixing block, 1002-handle, 1003-clamping hole, 1004-clamping rod, 1005-second baffle, 1006-circular groove, 1007-second spring, 11-camera and 12-groove.
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. Based on the embodiments in the present invention, all other embodiments obtained by a person skilled in the art without creative work belong to the protection scope of the present invention.
Please refer to fig. 1 ~ 4, in the embodiment of the utility model provides an in, a special unmanned aerial vehicle of education convenient to dismouting, including organism 1, 1 side fixedly connected with cantilever 2 of organism, 2 lower extreme fixedly connected with motors 4 of cantilever, motor 4's play axle fixedly connected with screw 3, 1 lower extreme fixedly connected with camera 11 of organism, first connecting block 8 and locking device 10, 8 lower extreme rotations of first connecting block are connected with bracing piece 6, 6 lower extreme fixedly connected with bottom plates 5 of bracing piece, 5 upper end fixedly connected with buffer 9 of bottom plate.
As a further embodiment of the present invention: the terminal surface is seted up flutedly 12 under organism 1, and sliding connection has safety cover 7 in the recess 12, and safety cover 7 is transparent material, and camera 11 is located inside safety cover 7, and the during operation installs the safety cover 7 in recess 12, just can reach the spacing to safety cover 7 like this under the effect of recess 12, can reach the protection to camera 11 simultaneously under the effect of safety cover 7.
As a still further embodiment of the present invention: buffer 9 is including second connecting block 901, first baffle 902, damping telescopic link 903, first spring 904 and third connecting block 905, 5 upper end fixedly connected with second connecting block 901 of bottom plate, second connecting block 901 upper end is rotated and is connected with damping telescopic link 903, the one end that second connecting block 901 was kept away from to damping telescopic link 903 is rotated and is connected with third connecting block 905, fixed connection between third connecting block 905 and the organism 1, in operation, when unmanned aerial vehicle whereabouts, when bottom plate 5 contacts ground, at this moment can push bottom plate 5 and remove, and then can make damping telescopic link 903 contract under the effect of second connecting block 901 and third connecting block 905, just so can reach the purpose of buffering under the effect of damping telescopic link 903.
As a still further embodiment of the present invention: damping telescopic link 903 periphery fixedly connected with first baffle 902, the first spring 904 of fixedly connected with between the first baffle 902, first spring 904 is located damping telescopic link 903 outside, and the during operation, when damping telescopic link 903 contracts, can reach the extrusion to first spring 904 under the effect of first baffle 902 at this moment, then be convenient for damping telescopic link 903 to reset under the effect of first spring 904.
As a still further embodiment of the present invention: the locking device 10 comprises a fixing block 1001, a handle 1002, a clamping hole 1003, a clamping rod 1004, a second baffle 1005, a circular groove 1006 and a second spring 1007, the fixing block 1001 is fixedly connected to the lower end of the machine body 1, the circular groove 1006 is formed in the fixing block 1001, the second baffle 1005 is slidably connected with the circular groove 1006, the second spring 1007 is fixedly connected to the second baffle 1005, the second spring 1007 is fixedly connected to the inner wall of the circular groove 1006, the clamping rod 1004 is rotatably connected to the second baffle 1005, the handle 1002 is fixedly connected to the side end of the clamping rod 1004, the clamping rod 1004 is slidably connected to the fixing block 1001, when the locking device works, when the protective cover 7 is pushed to be inserted into the groove 12, the clamping rod 1004 is extruded, the second spring 1007 can be compressed under the action of the second baffle 1005, when the clamping rod 1004 faces the clamping hole 1003, the clamping rod 1004 can be clamped into the clamping hole 1003 under the action of the second spring 1007, this achieves a fixing of the protective cap 7.
As a still further embodiment of the present invention: the side end face of the protective cover 7 is provided with a clamping hole 1003, the clamping hole 1003 is clamped with a clamping rod 1004, one end of the clamping rod 1004 close to the clamping hole 1003 is provided with an inclined surface, and during operation, one end of the clamping rod 1004 is provided with the inclined surface, so that the clamping rod 1004 is conveniently extruded to move.
The utility model discloses a theory of operation is:
when the utility model is used, when the unmanned aerial vehicle falls, when the bottom plate 5 contacts the ground, the bottom plate 5 is extruded to move, and then the damping telescopic rod 903 can be contracted under the action of the second connecting block 901 and the third connecting block 905, and then the compression of the first spring 904 can be achieved under the action of the first baffle 902, so that the purpose of buffering can be achieved under the action of the first spring 904 and the damping telescopic rod 903; when the protective cover 7 needs to be detached, the handle 1002 is rotated firstly to enable the inclined surface of the clamping rod 1004 to face the upper end, then the protective cover 7 is pulled downwards, the clamping rod 1004 is extruded to slide in the circular groove 1006, further, the second spring 1007 can be extruded under the action of the second baffle 1005, when the protective cover 7 is detached, the clamping rod 1004 can be conveniently reset under the action of the second spring 1007, when the protective cover 7 needs to be installed, the handle 1002 is rotated to enable the inclined surface of the clamping rod 1004 to face the lower end, therefore, when the protective cover 7 is pushed to move towards the groove 12, at this time, the protective cover 7 can be conveniently installed, and then the purpose of fixing the protective cover 7 can be achieved under the action of the clamping rod 1004.
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 utility model provides a special unmanned aerial vehicle of education convenient to dismouting, includes organism (1), its characterized in that: organism (1) side fixedly connected with cantilever (2), cantilever (2) lower extreme fixedly connected with motor (4), the play axle fixedly connected with screw (3) of motor (4), organism (1) lower extreme fixedly connected with camera (11), first connecting block (8) and closing device (10), first connecting block (8) lower extreme rotates and is connected with bracing piece (6), bracing piece (6) lower extreme fixedly connected with bottom plate (5), bottom plate (5) upper end fixedly connected with buffer (9).
2. The unmanned aerial vehicle special for education convenient to dismouting of claim 1, characterized in that: the camera is characterized in that a groove (12) is formed in the lower end face of the machine body (1), a protective cover (7) is connected in the groove (12) in a sliding mode, the protective cover (7) is made of transparent materials, and the camera (11) is located inside the protective cover (7).
3. The unmanned aerial vehicle special for education convenient to dismouting of claim 1, characterized in that: buffer (9) including second connecting block (901), first baffle (902), damping telescopic link (903), first spring (904) and third connecting block (905), bottom plate (5) upper end fixedly connected with second connecting block (901), second connecting block (901) upper end is rotated and is connected with damping telescopic link (903), the one end that second connecting block (901) were kept away from in damping telescopic link (903) is rotated and is connected with third connecting block (905), fixed connection between third connecting block (905) and organism (1).
4. The unmanned aerial vehicle special for education convenient to dismouting of claim 3, characterized in that: damping telescopic link (903) periphery fixedly connected with first baffle (902), first spring (904) of fixedly connected with between first baffle (902), first spring (904) are located damping telescopic link (903) outside.
5. The unmanned aerial vehicle special for education convenient to dismouting of claim 2, characterized in that: the locking device (10) comprises a fixing block (1001), a handle (1002), a clamping hole (1003), a clamping rod (1004), a second baffle (1005), a circular groove (1006) and a second spring (1007), wherein the fixing block (1001) is fixedly connected to the lower end of the machine body (1), the circular groove (1006) is formed in the fixing block (1001), the second baffle (1005) is connected in the circular groove (1006) in a sliding mode, the second spring (1007) is fixedly connected to the second baffle (1005), the inner wall of the circular groove (1006) is fixedly connected to the second spring (1007), the clamping rod (1004) is rotatably connected to the second baffle (1005), the handle (1002) is fixedly connected to the side end of the clamping rod (1004), and the clamping rod (1004) is connected to the fixing block (1001) in a sliding mode.
6. The unmanned aerial vehicle special for education convenient to dismouting of claim 5, characterized by that: the side end face of the protective cover (7) is provided with a clamping hole (1003), the clamping hole (1003) is clamped with a clamping rod (1004), and one end, close to the clamping hole (1003), of the clamping rod (1004) is provided with an inclined face.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202123020328.4U CN216468553U (en) | 2021-12-03 | 2021-12-03 | Special unmanned aerial vehicle of education convenient to dismouting |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202123020328.4U CN216468553U (en) | 2021-12-03 | 2021-12-03 | Special unmanned aerial vehicle of education convenient to dismouting |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN216468553U true CN216468553U (en) | 2022-05-10 |
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ID=81419098
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202123020328.4U Active CN216468553U (en) | 2021-12-03 | 2021-12-03 | Special unmanned aerial vehicle of education convenient to dismouting |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN216468553U (en) |
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2021
- 2021-12-03 CN CN202123020328.4U patent/CN216468553U/en active Active
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