CN221738115U - Many rotor unmanned aerial vehicle protection device - Google Patents
Many rotor unmanned aerial vehicle protection device Download PDFInfo
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- CN221738115U CN221738115U CN202420315396.8U CN202420315396U CN221738115U CN 221738115 U CN221738115 U CN 221738115U CN 202420315396 U CN202420315396 U CN 202420315396U CN 221738115 U CN221738115 U CN 221738115U
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- 230000004224 protection Effects 0.000 title claims abstract description 79
- 238000004140 cleaning Methods 0.000 claims abstract description 75
- 230000007246 mechanism Effects 0.000 claims abstract description 25
- 238000013016 damping Methods 0.000 claims abstract description 20
- 239000000872 buffer Substances 0.000 claims abstract description 18
- 230000000712 assembly Effects 0.000 claims 2
- 238000000429 assembly Methods 0.000 claims 2
- 230000000694 effects Effects 0.000 abstract description 9
- 239000000428 dust Substances 0.000 description 6
- 230000003139 buffering effect Effects 0.000 description 4
- 230000001681 protective effect Effects 0.000 description 3
- 238000000034 method Methods 0.000 description 2
- 230000003014 reinforcing effect Effects 0.000 description 2
- 239000011435 rock Substances 0.000 description 2
- 208000035473 Communicable disease Diseases 0.000 description 1
- 230000004075 alteration Effects 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 208000015181 infectious disease Diseases 0.000 description 1
- 238000007689 inspection Methods 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 238000013507 mapping Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012544 monitoring process Methods 0.000 description 1
- 230000002035 prolonged effect Effects 0.000 description 1
- 230000009979 protective mechanism Effects 0.000 description 1
- 239000007858 starting material Substances 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
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Abstract
The utility model discloses a multi-rotor unmanned aerial vehicle protection device, which belongs to the technical field of unmanned aerial vehicles and comprises an unmanned aerial vehicle body, wherein rotor wing protection plates are arranged on two sides of the unmanned aerial vehicle body, a buffer assembly is arranged on the surface of each rotor wing protection plate, a protection mechanism is arranged below the unmanned aerial vehicle body, supporting mechanisms are arranged on two sides of the protection mechanism, a camera device is arranged in the protection mechanism, and a cleaning assembly is arranged on the surface of the protection mechanism; according to the utility model, the buffer assembly is arranged, the anti-collision shell and the anti-collision plate are arranged on the surface of the rotor wing protection plate through the fixing plate, so that the anti-collision effect of the rotor wing protection plate is improved, when collision occurs, the damping rod and the buffer sponge can absorb and eliminate impact force generated during collision, and therefore, the unmanned aerial vehicle body is prevented from falling down due to shaking after being impacted, and the impact force generated by the collision is prevented from damaging the components inside the unmanned aerial vehicle body.
Description
Technical Field
The utility model belongs to the technical field of unmanned aerial vehicles, and particularly relates to a multi-rotor unmanned aerial vehicle protection device.
Background
The unmanned aerial vehicle is an unmanned aerial vehicle which is controlled by using radio remote control equipment and a self-provided program control device, is currently applied to the fields of aerial photography, agriculture, plant protection, miniature self-timer shooting, express delivery transportation, disaster rescue, wild animal observation, infectious disease monitoring, mapping, news reporting, electric power inspection, disaster relief, film and television shooting, romantic manufacturing and the like, and greatly expands the application of the unmanned aerial vehicle.
The utility model provides a many rotor unmanned aerial vehicle protection device that chinese patent bulletin number CN214451897U discloses, includes the device main part, the device main part includes unmanned aerial vehicle main part and camera, one side fixedly connected with guard plate of unmanned aerial vehicle main part, one side fixedly connected with screw of guard plate, one side fixedly connected with support frame of unmanned aerial vehicle main part, one side of camera is provided with protection machanism, protection machanism includes protection casing and connecting block, one side swing joint of camera has the protection casing, one side fixedly connected with connecting block of protection casing, one side fixedly connected with connecting rod of connecting block, one side fixedly connected with fixed block of camera. According to the utility model, the protection mechanism is arranged, and the connecting rod extends to the inside of the fixed block, so that the surface of the device is protected, the device is prevented from being polluted in the using process, and the service life of the device is prolonged when the device is used as a whole.
The above-disclosed patents have the following problems: the protection effect of the protection plate is poor, and the impact force generated during collision cannot be processed, so that the unmanned aerial vehicle body is easy to shake and fall; in the flight process of the unmanned aerial vehicle body, dust is easy to adhere to the surface of the camera device protective cover, so that shooting of the camera device is affected.
Disclosure of utility model
To solve the problems set forth in the background art. The utility model provides a multi-rotor unmanned aerial vehicle protection device which has the characteristics of eliminating impact force generated when an unmanned aerial vehicle body collides and cleaning the surface of a protective cover.
In order to achieve the above purpose, the present utility model provides the following technical solutions: the utility model provides a many rotor unmanned aerial vehicle protection device, includes the unmanned aerial vehicle body, the both sides of unmanned aerial vehicle body are provided with the rotor guard plate, and the surface of rotor guard plate is provided with buffer assembly, and the below of unmanned aerial vehicle body is provided with protection machanism, and protection machanism's both sides are provided with supporting mechanism, and protection machanism's inside is provided with camera device, and protection machanism's surface is provided with clean subassembly.
Preferably, the buffer assembly comprises an anti-collision shell, a damping rod, an anti-collision plate, a fixing plate, a buffer sponge, a spring rod and a sleeve, wherein the fixing plate is arranged on one side of the rotor wing protection plate, the anti-collision shell is arranged on the other side of the fixing plate, the damping rod is arranged between the fixing plate and the anti-collision shell, the spring rod is arranged on two sides of the damping rod, the sleeve is arranged at one end of the spring rod, the buffer sponge is arranged in the anti-collision shell, and the anti-collision plate is arranged on one side of the buffer sponge.
Preferably, the surface of fixed plate is provided with a plurality of groups of fixing bolt, and the fixed plate passes through the fixing bolt setting at the surface of rotor guard plate.
Preferably, the inside of sleeve is cavity form and sleeve inside is provided with the stopper, and the spring rod pierces through the sleeve and is connected with inside stopper.
Preferably, the cleaning component comprises a motor, a cleaning rod, a cleaning brush, a fixing frame, a connecting seat, a sliding block, a sliding groove and a spring, wherein the cleaning rod is arranged on the surface of the protection mechanism, the motor is arranged on one side of the cleaning rod, the fixing frame is arranged on the outer side of the motor, the connecting seat is arranged inside the cleaning rod, the sliding groove is arranged above and below the connecting seat, the sliding block is arranged inside the sliding groove, the spring is arranged on one side of the connecting seat, and the cleaning brush is arranged on the other side of the connecting seat.
Preferably, one side of the connecting seat is provided with three groups of connecting rods, and the connecting rods penetrate through the inside of the cleaning rod to be connected with the cleaning brush.
Compared with the prior art, the utility model has the beneficial effects that:
1. According to the utility model, the buffer assembly is arranged, the anti-collision shell and the anti-collision plate are arranged on the surface of the rotor wing protection plate through the fixing plate, so that the anti-collision effect of the rotor wing protection plate is improved, when collision occurs, the damping rod and the buffer sponge can absorb and eliminate impact force generated during collision, and therefore, the unmanned aerial vehicle body is prevented from falling down due to shaking after being impacted, and the impact force generated by the collision is prevented from damaging the components inside the unmanned aerial vehicle body.
2. According to the utility model, the cleaning assembly is arranged, when the protection mechanism is required to be cleaned, the motor drives the cleaning rod to clean the protection mechanism, dust attached to the surface of the protection cover is prevented from affecting shooting of the internal camera device, and the cleaning brush can be tightly attached to the surface of the protection mechanism through rebound of the spring due to the fact that the spring is arranged in the cleaning rod.
Drawings
FIG. 1 is a schematic diagram of the structure of the present utility model;
FIG. 2 is a schematic view of a cushioning assembly according to the present utility model;
FIG. 3 is a cross-sectional view of a cushioning assembly of the present utility model;
FIG. 4 is a schematic view of a cleaning assembly according to the present utility model;
FIG. 5 is a side view of a cleaning assembly of the present utility model;
Figure 6 is a cross-sectional view of a cleaning assembly of the present utility model.
In the figure: 1. an unmanned aerial vehicle body; 2. rotor wing protection plates; 3. a buffer assembly; 31. an anti-collision shell; 32. a damping rod; 33. an anti-collision plate; 34. a fixing plate; 35. buffering sponge; 36. a spring rod; 37. a sleeve; 4. a support mechanism; 5. a protective mechanism; 6. a cleaning assembly; 61. a motor; 62. a cleaning lever; 63. a cleaning brush; 64. a fixing frame; 65. a connecting seat; 66. a slide block; 67. a chute; 68. a spring; 7. an image pickup device.
Detailed Description
The following description of the embodiments of the present utility model will be made clearly and completely with reference to the accompanying drawings, in which it is apparent that the embodiments described are only some embodiments of the present utility model, but not all embodiments. All other embodiments, which can be made by those skilled in the art based on the embodiments of the utility model without making any inventive effort, are intended to be within the scope of the utility model.
Example 1
Referring to fig. 1-6, the present utility model provides the following technical solutions: the utility model provides a many rotor unmanned aerial vehicle protection device, includes unmanned aerial vehicle body 1, and unmanned aerial vehicle body 1's both sides are provided with rotor guard plate 2, and rotor guard plate 2's surface is provided with buffer assembly 3, and unmanned aerial vehicle body 1's below is provided with protection machanism 5, and protection machanism 5's both sides are provided with supporting mechanism 4, and protection machanism 5's inside is provided with camera device 7, and protection machanism 5's surface is provided with clean subassembly 6.
Specifically, the buffer assembly 3 includes the crashproof shell 31, the damping pole 32, crashproof board 33, fixed plate 34, buffering sponge 35, spring lever 36 and sleeve 37, wherein, one side of rotor guard plate 2 is provided with fixed plate 34, the opposite side of fixed plate 34 is provided with crashproof shell 31, be provided with damping pole 32 between fixed plate 34 and the crashproof shell 31, the both sides of damping pole 32 are provided with spring lever 36, the one end of spring lever 36 is provided with sleeve 37, the inside of crashproof shell 31 is provided with buffering sponge 35, one side of buffering sponge 35 is provided with crashproof plate 33.
Through adopting above-mentioned technical scheme, the surface at rotor guard plate 2 is installed through fixed plate 34 to anticollision shell 31 and crashproof board 33, thereby the crashproof effect of rotor guard plate 2 has been improved, when bumping, the damping pole 32 that sets up between crashproof shell 31 and the fixed plate 34 can absorb and eliminate the impact force that produces when striking and the buffer sponge 35 that sets up in the crashproof shell 31 also can cushion, thereby prevent that unmanned aerial vehicle body 1 from producing after the striking and rocking and leading to unmanned aerial vehicle body 1 to drop also prevented the inside subassembly of impact force harm unmanned aerial vehicle body 1 that produces, still be provided with spring pole 36 and sleeve 37 between crashproof shell 31 and the fixed plate 34, thereby make crashproof board 33 receive crashproof shell 31 after the striking and can stretch out and draw back.
Specifically, the surface of the fixing plate 34 is provided with a plurality of groups of fixing bolts, and the fixing plate 34 is arranged on the surface of the rotor wing protection plate 2 through the fixing bolts.
Through adopting above-mentioned technical scheme, the surface of fixed plate 34 is provided with a plurality of groups of fixing bolt, and fixed plate 34 passes through the fixing bolt setting on the surface of rotor guard plate 2 to the convenience of customers installs and dismantles fixed plate 34.
Specifically, the inside of the sleeve 37 is hollow, a limiting block is arranged inside the sleeve 37, and the spring rod 36 penetrates through the sleeve 37 to be connected with the limiting block inside.
Through adopting above-mentioned technical scheme, the inside of sleeve 37 is hollow to make things convenient for the flexible of spring rod 36, spring rod 36 pierces through sleeve 37 and is connected with the stopper of inside, thereby makes the one end of spring rod 36 can fix in the inside of sleeve 37.
When this embodiment is used, anticollision shell 31 and anticollision board 33 pass through fixed plate 34 and install the surface at rotor guard plate 2, thereby the anticollision effect of rotor guard plate 2 has been improved, when bumping, the damping pole 32 that sets up between anticollision shell 31 and the fixed plate 34 can absorb and eliminate the impact force that produces when bumping and the buffer sponge 35 that sets up in the anticollision shell 31 also can cushion, thereby prevent that unmanned aerial vehicle body 1 from producing after bumping and rocking and leading to unmanned aerial vehicle body 1 to drop also prevent the inside subassembly of unmanned aerial vehicle body 1 of impact force that produces, still be provided with spring bar 36 and sleeve 37 between anticollision shell 31 and the fixed plate 34, thereby make anticollision shell 31 can stretch out and draw back after anticollision board 33 receives the striking, the surface of fixed plate 34 is provided with a plurality of sets of fixing bolt, fixed plate 34 passes through the fixing bolt setting at rotor guard plate 2, thereby the user installs and dismantles fixed plate 34, sleeve 37's inside is hollow, thereby the flexible of spring bar 36 is convenient, spring bar 36 is connected with inside stopper, thereby make the one end of spring bar 36 can fix inside sleeve 37.
Example 2
This embodiment differs from embodiment 1 in that: specifically, the cleaning assembly 6 includes a motor 61, a cleaning lever 62, a cleaning brush 63, a fixing frame 64, a connecting seat 65, a slider 66, a chute 67 and a spring 68, wherein the surface of the protection mechanism 5 is provided with the cleaning lever 62, one side of the cleaning lever 62 is provided with the motor 61, the outside of the motor 61 is provided with the fixing frame 64, the inside of the cleaning lever 62 is provided with the connecting seat 65, the chute 67 is provided above and below the connecting seat 65, the slider 66 is provided in the inside of the chute 67, one side of the connecting seat 65 is provided with the spring 68, and the other side of the connecting seat 65 is provided with the cleaning brush 63.
Through adopting above-mentioned technical scheme, clean pole 62 is connected with cleaning brush 63 through the connecting seat 65 that inside set up, thereby because one side of connecting seat 65 is provided with spring 68 and makes cleaning brush 63 hug closely the surface at protection machanism 5 through spring 68's resilience, thereby reinforcing cleaning brush 63's cleaning effect and connecting seat 65's top and below are provided with spout 67 and slider 66, thereby can assist connecting seat 65 to stretch out and draw back, when needs are clean protection machanism 5, starter motor 61 drives clean pole 62 and rotates, thereby clean pole 62 rotates and drives cleaning brush 63 clean protection machanism 5, prevent that the dust that the protection casing surface is attached from influencing the shooting of inside camera device 7.
Specifically, one side of the connection base 65 is provided with three sets of connection rods, which penetrate the inside of the cleaning rod 62 to be connected with the cleaning brush 63.
Through adopting above-mentioned technical scheme, one side of connecting seat 65 is provided with three sets of connecting rods, and the connecting rod pierces through the inside of cleaning rod 62 and is connected with cleaning brush 63 to the stability when having improved cleaning brush 63 clean has prevented that the cleaning brush from taking place to rock when 63 are clean.
When the cleaning brush is used, the cleaning rod 62 is connected with the cleaning brush 63 through the connecting seat 65 arranged inside, the cleaning brush 63 can be tightly attached to the surface of the protection mechanism 5 through resilience of the spring 68 due to the fact that the spring 68 is arranged on one side of the connecting seat 65, so that cleaning effect of the cleaning brush 63 is enhanced, the sliding groove 67 and the sliding block 66 are arranged above and below the connecting seat 65, the connecting seat 65 can be assisted to stretch and retract, when the protection mechanism 5 needs to be cleaned, the motor 61 is started to drive the cleaning rod 62 to rotate, the cleaning rod 62 rotates to drive the cleaning brush 63 to clean the protection mechanism 5, dust attached to the surface of the protective cover is prevented from affecting shooting of the internal camera device 7, and due to the fact that three groups of connecting rods are arranged on one side of the connecting seat 65, the connecting rods penetrate through the inside of the cleaning rod 62 and are connected with the cleaning brush 63, so that stability of the cleaning brush 63 in cleaning is improved, and shaking of the cleaning brush 63 is prevented when the cleaning brush is cleaned.
The damping rod 32 of the present utility model is of the type known in the art and is selected from the group consisting of HCL-30.
The structure and the use principle of the rotor protection plate 2, the supporting mechanism 4 and the protection mechanism 5 in the utility model are disclosed in a multi-rotor unmanned aerial vehicle protection device disclosed in China patent publication No. CN 214451897U.
The working principle and the using flow of the utility model are as follows: when the unmanned aerial vehicle protection device is used for unmanned aerial vehicle anti-collision of the multi-rotor unmanned aerial vehicle protection device, when the unmanned aerial vehicle body 1 collides, the generated impact force needs to be processed, the anti-collision shell 31 and the anti-collision plate 33 are installed on the surface of the rotor protection plate 2 through the fixing plate 34, so that the anti-collision effect of the rotor protection plate 2 is improved, when the unmanned aerial vehicle protection device collides, the damping rod 32 arranged between the anti-collision shell 31 and the fixing plate 34 absorbs and eliminates the impact force generated during the collision, the buffer sponge 35 arranged in the anti-collision shell 31 also buffers, so that the unmanned aerial vehicle body 1 is prevented from shaking after the collision, the unmanned aerial vehicle body 1 falls down, the impact force generated during the collision is prevented from damaging components in the unmanned aerial vehicle body 1, the spring rod 36 and the sleeve 37 are arranged between the anti-collision shell 31 and the fixing plate 34, the anti-collision shell 31 can be stretched after the collision of the anti-collision plate 33 is impacted, a plurality of groups of fixing bolts are arranged on the surface of the fixing plate 34, the fixing plate 34 is arranged on the surface of the rotor protection plate 2 through the fixing bolts, so that a user can conveniently install and detach the fixing plate 34, the inside of the sleeve 37 is hollow, and the inside of the sleeve 37 can conveniently penetrate through the inside the fixing plate 36, and one end of the spring rod 36 can be conveniently stretched out and fixed inside the sleeve 37; when using, be used for many rotor unmanned aerial vehicle protection device's protection casing cleanness, when unmanned aerial vehicle body 1 during operation, need handle the dust that protection machanism 5 surface was attached, clean pole 62 is connected with cleaning brush 63 through the connecting seat 65 that the inside set up, thereby one side of connecting seat 65 is provided with spring 68 makes cleaning brush 63 hug closely at protection machanism 5's surface through spring 68's resilience, thereby reinforcing cleaning brush 63's cleaning effect and connecting seat 65's top and below are provided with spout 67 and slider 66, thereby can assist connecting seat 65 to stretch out and draw back, when need clean protection machanism 5, start motor 61 drives cleaning rod 62 and rotates, thereby cleaning rod 62 rotates and drives cleaning brush 63 clean protection machanism 5, prevent the dust that protection casing surface is attached to influence inside camera device 7's shooting, owing to one side of connecting seat 65 is provided with three sets of connecting rods, the connecting rod pierces the inside of cleaning rod 62 is connected with cleaning brush 63, thereby stability when having improved cleaning brush 63 and prevented that the cleaning brush from taking place to rock when 63 is clean.
Although embodiments of the present utility model have been shown and described, it will be understood by those skilled in the art that various changes, modifications, substitutions and alterations can be made therein without departing from the principles and spirit of the utility model, the scope of which is defined in the appended claims and their equivalents.
Claims (4)
1. The utility model provides a many rotor unmanned aerial vehicle protection device, includes unmanned aerial vehicle body, its characterized in that: the unmanned aerial vehicle comprises an unmanned aerial vehicle body, wherein rotor wing protection plates are arranged on two sides of the unmanned aerial vehicle body, buffer assemblies are arranged on the surfaces of the rotor wing protection plates, a protection mechanism is arranged below the unmanned aerial vehicle body, supporting mechanisms are arranged on two sides of the protection mechanism, a camera device is arranged inside the protection mechanism, and cleaning assemblies are arranged on the surfaces of the protection mechanism;
The damping assembly comprises an anti-collision shell, damping rods, an anti-collision plate, a fixing plate, a damping sponge, a spring rod and a sleeve, wherein the fixing plate is arranged on one side of the rotor wing protection plate, the anti-collision shell is arranged on the other side of the fixing plate, the damping rods are arranged between the fixing plate and the anti-collision shell, the spring rods are arranged on two sides of the damping rods, the sleeve is arranged at one end of each spring rod, the damping sponge is arranged in the anti-collision shell, and the anti-collision plate is arranged on one side of each damping sponge;
The cleaning assembly comprises a motor, a cleaning rod, a cleaning brush, a fixing frame, a connecting seat, a sliding block, a sliding groove and a spring, wherein the cleaning rod is arranged on the surface of the protection mechanism, the motor is arranged on one side of the cleaning rod, the fixing frame is arranged on the outer side of the motor, the connecting seat is arranged inside the cleaning rod, the sliding groove is arranged above and below the connecting seat, the sliding block is arranged inside the sliding groove, the spring is arranged on one side of the connecting seat, and the cleaning brush is arranged on the other side of the connecting seat.
2. The multi-rotor unmanned aerial vehicle protection device of claim 1, wherein: the surface of fixed plate is provided with a plurality of groups of fixing bolt, and the fixed plate passes through the fixing bolt setting at the surface of rotor guard plate.
3. The multi-rotor unmanned aerial vehicle protection device of claim 1, wherein: the inside of sleeve is cavity form and sleeve inside is provided with the stopper, and the spring beam pierces through the sleeve and is connected with inside stopper.
4. The multi-rotor unmanned aerial vehicle protection device of claim 1, wherein: three groups of connecting rods are arranged on one side of the connecting seat, penetrate through the inside of the cleaning rod and are connected with the cleaning brush.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202420315396.8U CN221738115U (en) | 2024-02-20 | 2024-02-20 | Many rotor unmanned aerial vehicle protection device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202420315396.8U CN221738115U (en) | 2024-02-20 | 2024-02-20 | Many rotor unmanned aerial vehicle protection device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN221738115U true CN221738115U (en) | 2024-09-20 |
Family
ID=92736044
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202420315396.8U Active CN221738115U (en) | 2024-02-20 | 2024-02-20 | Many rotor unmanned aerial vehicle protection device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN221738115U (en) |
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2024
- 2024-02-20 CN CN202420315396.8U patent/CN221738115U/en active Active
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