CN218343736U - Environmental investigation unmanned aerial vehicle's crashproof structure - Google Patents
Environmental investigation unmanned aerial vehicle's crashproof structure Download PDFInfo
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- CN218343736U CN218343736U CN202222742229.5U CN202222742229U CN218343736U CN 218343736 U CN218343736 U CN 218343736U CN 202222742229 U CN202222742229 U CN 202222742229U CN 218343736 U CN218343736 U CN 218343736U
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Abstract
The utility model relates to an unmanned aerial vehicle's anticollision technical field specifically indicates an environmental investigation unmanned aerial vehicle's anticollision structure. Including environment investigation unmanned aerial vehicle body, there is the support frame environment investigation unmanned aerial vehicle body below, this internal investigation camera that is equipped with of environment investigation unmanned aerial vehicle, environment investigation unmanned aerial vehicle body both sides all are equipped with anticollision subassembly, this internal solar battery panel that has of environment investigation unmanned aerial vehicle, environment investigation unmanned aerial vehicle body surface is located environment investigation unmanned aerial vehicle body top and is equipped with the subassembly that cleans, clean the subassembly and include two fixed frames, be equipped with the motor in one of them fixed frame, the output shaft of motor has the hob, another fixed frame interpolation is equipped with the gag lever post, hob and gag lever post all overlap and are equipped with the movable block, connect through the connecting rod between two movable blocks, the connecting rod surface is equipped with the pappus brush, the utility model provides a can carry out the duration of debris clearance increase device to the solar panel surface an environment investigation unmanned aerial vehicle's anticollision structure.
Description
Technical Field
The utility model relates to an unmanned aerial vehicle's anticollision technical field specifically indicates an environmental investigation unmanned aerial vehicle's anticollision structure.
Background
The environment investigation is the action of carrying out the condition investigation to natural environment, equips more and more common modern at the unmanned, is comparatively laborsaving environment investigation mode with unmanned aerial vehicle for the environment investigation, carries out the task that the environment investigation not only can be through setting for the investigation environment purpose in advance with unmanned aerial vehicle to carry out the acquireing of different task images through task management.
Application number CN202020001020.1, public (announcement) number CN211766339U discloses an unmanned aerial vehicle for environmental monitoring, include the unmanned aerial vehicle fuselage and install in a set of relative supporting leg in unmanned aerial vehicle fuselage bottom both sides, the arc is installed at unmanned aerial vehicle fuselage both ends and is prevented the board of colliding, is equipped with buffer gear in the anticollision board, this internal environmental monitoring mechanism of installing of unmanned aerial vehicle. The beneficial effects of the utility model are that, through being located the buffer gear of anti-collision inboard, can play the cushioning effect to the anticollision board, prevent that unmanned aerial vehicle from bumping damage phenomenon when abominable topography or weather monitoring, the temperature humidity and the haze signal of environment monitoring mechanism monitorable air are induced air through the air exhauster, improve monitoring effect, and the mounting panel is detachable construction, is convenient for clear up and maintain. The above patents suffer from the following drawbacks: the solar cell panel can shield the efficiency of the solar cell panel for absorbing light energy by falling more sundries on the solar cell panel in the work of struggling an execution environment of the device for investigation, thereby influencing the endurance of the whole device.
SUMMERY OF THE UTILITY MODEL
The to-be-solved technical problem of the utility model is to provide an environmental investigation unmanned aerial vehicle's anticollision structure that can carry out debris clearance increase device's duration to the solar panel surface.
The utility model discloses the technical scheme who adopts does: the utility model provides an environmental investigation unmanned aerial vehicle's crashproof structure which characterized in that: the environment detection unmanned aerial vehicle comprises an environment detection unmanned aerial vehicle body, a support frame is fixed below the environment detection unmanned aerial vehicle body, a detection camera is arranged in the environment detection unmanned aerial vehicle body, two transverse plates are arranged on two sides of the environment detection unmanned aerial vehicle body, a driving blade is arranged above the transverse plates, anti-collision assemblies are arranged on two sides of the environment detection unmanned aerial vehicle body and comprise anti-collision fixing pieces arranged on two sides of the environment detection unmanned aerial vehicle body, the environment detection unmanned aerial vehicle body and the anti-collision fixing pieces are fixedly connected through a plurality of fixing bolts, telescopic rods are fixed in the anti-collision fixing pieces, the anti-collision fixing pieces are connected with anti-collision plates through the telescopic rods, the telescopic rod sleeves are provided with springs, anti-collision cushions are arranged on the surfaces of the anti-collision plates, a solar accumulator plate is arranged in the environment detection unmanned aerial vehicle body, a cleaning assembly is arranged above the environment detection unmanned aerial vehicle body and comprises fixing frames arranged on two sides of the solar accumulator plate respectively, a motor is arranged in the fixing frames, an output shaft of the motor is connected with a spiral rod, a limit rod is inserted in the fixing frame, and a limit rod and a movable block sleeve is arranged on the limit rod.
Preferably, the lower surface of the support frame is fixed with a non-slip mat, and the non-slip mat has the function of increasing the non-slip property when the device is parked.
Preferably, fixed connection between the crashproof mounting and the stiff end of telescopic link, fixed connection between crashproof board and the flexible end of telescopic link.
Preferably, the spring is in a natural extension state, one end of the spring is fixedly connected with the anti-collision fixing piece, and the other end of the spring is fixedly connected with the anti-collision plate.
Preferably, a groove matched with the spring to enter is formed in the anti-collision fixing piece and around the telescopic rod and the spring.
Preferably, the pappus brush is kept away from connecting rod one end and is hugged closely in solar energy electric storage battery surface, and the effect of this setting can be so that the pappus brush increases the dynamics of cleaning when cleaning, be equipped with the spacing recess that cooperation movable block and connecting rod removed in the fixed frame.
Preferably, the both ends of hob and gag lever post all are equipped with the bearing, all be connected fixedly through the bearing between the both ends of fixed frame and hob and the both ends of gag lever post, the rotational position of hob, gag lever post is injectd in the effect of bearing.
The utility model has the advantages that:
the utility model discloses multiple functional, thereby can shorten and spring compression consume some impact energy through the telescopic link when the device receives the striking aloft and reduce the impact damage to the impact on environment investigation unmanned aerial vehicle body surface, the sheltering from thing on solar energy storage battery surface can clean through cleaning the subassembly, wholly sees, the utility model discloses can carry out the duration of debris clearance increase device to the solar panel surface.
Drawings
Fig. 1 is the utility model relates to an environmental investigation unmanned aerial vehicle's crashproof structure's whole direction cross-sectional view that overlooks.
Fig. 2 is the utility model relates to an environmental investigation unmanned aerial vehicle's crashproof structure's elevation.
Fig. 3 is the utility model relates to an environmental investigation unmanned aerial vehicle's crashproof structure's a portion schematic structure.
( 1. An environmental reconnaissance unmanned aerial vehicle body; 2. a support frame; 3. detecting a camera; 4. an anti-collision assembly; 4.1, anti-collision fixing pieces; 4.2, fixing the bolt; 4.3, a telescopic rod; 4.4, a spring; 4.5, an anti-collision plate; 4.6, anti-collision soft cushion; 5. a transverse plate; 6. a driving blade; 7. a solar storage panel; 8. a sweeping assembly; 8.1, a motor; 8.2, a screw rod; 8.3, a bearing; 8.4, a movable block; 8.5, connecting rods; 8.6, a limiting groove; 8.7, a limiting rod; 8.8 fixed frame )
Detailed Description
The present invention will be further explained with reference to the accompanying drawings.
Can carry out the duration of debris clearance increase device to the solar panel surface for environmental investigation unmanned aerial vehicle's crashproof structure, the utility model provides an environmental investigation unmanned aerial vehicle's crashproof structure as shown in the figure, its function lies in: including environment investigation unmanned aerial vehicle body 1, environment investigation unmanned aerial vehicle body 1 below is fixed with support frame 2, this internal investigation camera 3 that is equipped with of environment investigation unmanned aerial vehicle, environment investigation unmanned aerial vehicle body 1 both sides all are equipped with two diaphragms 5, diaphragm 5 top is equipped with drive blade 6, environment investigation unmanned aerial vehicle body 1 both sides all are equipped with anticollision subassembly 4, anticollision subassembly 4 is including setting up in the crashproof mounting 4.1 of environment investigation unmanned aerial vehicle body 1 both sides, through a plurality of fixing bolt 4.2 fixed connection between environment investigation unmanned aerial vehicle body 1 and the crashproof mounting 4.1, anticollision mounting 4.1 internal fixation has telescopic link 4.3, anticollision mounting 4.1 is connected with anticollision board 4.5 through telescopic link 4.3, telescopic link 4.3 overlaps and is equipped with spring 4.4, anticollision board 4.5 surface is equipped with anticollision cushion 4.6, this internal solar energy accumulator plate 7 that is equipped with of environment investigation unmanned aerial vehicle, environment investigation unmanned aerial vehicle body 1 surface is located environment investigation unmanned aerial vehicle body 1 top and is equipped with cleaning assembly 8.8, the connecting rod 8.8 sets up respectively in two movable pole 8.8.8 movable pole internal connections of motor 8.8.8 the motor 8.8 the movable pole 8.8 is equipped with the movable pole 8.8.8.8.8.
The utility model discloses in 2 lower surface fixing of support frame have the slipmat.
The utility model discloses in fixed connection between the stiff end of anticollision mounting 4.1 and telescopic link 4.3, fixed connection between the flexible end of anticollision board 4.5 and telescopic link 4.3.
The utility model discloses in spring 4.4 is in the natural extension state, fixed connection between spring 4.4's one end and the crashproof mounting 4.1, fixed connection between spring 4.4's the other end and the crashproof board 4.5.
The utility model discloses in be located in the anticollision mounting 4.1 and be equipped with the recess that cooperation spring 4.4 got into around telescopic link 4.3 and spring 4.4.
The utility model discloses in the pappus brush is kept away from connecting rod 8.5 one end and is hugged closely in 7 surfaces of solar energy accumulator plate, be equipped with the spacing recess 8.6 that cooperation movable block 8.4 and connecting rod 8.5 removed in the fixed frame 8.8.
The utility model discloses in the both ends of hob 8.2 and gag lever post 8.7 are all overlapped and are equipped with bearing 8.3, all be connected fixedly through bearing 8.3 between the both ends of fixed frame 8.8 and hob 8.2 and gag lever post 8.7's both ends.
The working principle of the device is as follows: the environmental condition of the environmental investigation way is shot by the investigation camera 3 in the flying process of the device, when the device is impacted in the air, the surface of the anti-collision plate 4.5 can be shortened through the telescopic rod 4.3 and the spring 4.4 are arranged in a matched mode, so that when the device is impacted in the air, part of impact energy can be consumed by the telescopic rod 4.3 and the spring 4.4 is compressed, the impact damage of impact force to the surface of the environmental investigation unmanned aerial vehicle body 1 is reduced, when the anti-collision assembly 4 is damaged, the anti-collision assembly 4 is disassembled and replaced by disassembling the fixing bolt 4.2, the solar accumulator plate 7 can absorb light energy and convert the light energy into electric energy, the device body is provided for endurance of environmental investigation work, when the surface of the solar accumulator plate 7 is provided with a shielding object, the motor 8.1 is driven to rotate through the output shaft, the spiral rod 8.2 is driven by the motor 8.1 to work, the spiral rod 8.2 is driven to move under the limit of the limit rod 8.7 while the spiral rod 8.2 rotates, the spiral rod 8.5 drives the accumulator plate 7 to move, and the connection rod 8.5 to move, and the soft brush 7 is driven to prevent the solar accumulator plate from influencing the surface of the solar energy deposition device.
The present invention and the embodiments thereof have been described above, but the description is not limited thereto, and the embodiment shown in the drawings is only one of the embodiments of the present invention, and the actual structure is not limited thereto. In summary, those skilled in the art should understand that they should not be limited to the embodiments described above, and that they can design the similar structure and embodiments without departing from the spirit of the invention.
Claims (7)
1. The utility model provides an environmental investigation unmanned aerial vehicle's crashproof structure which characterized in that: the environment detection unmanned aerial vehicle comprises an environment detection unmanned aerial vehicle body (1), wherein a support frame (2) is fixed below the environment detection unmanned aerial vehicle body (1), a detection camera (3) is arranged in the environment detection unmanned aerial vehicle body (1), two transverse plates (5) are arranged on two sides of the environment detection unmanned aerial vehicle body (1), a driving blade (6) is arranged above each transverse plate (5), anti-collision assemblies (4) are arranged on two sides of the environment detection unmanned aerial vehicle body (1), each anti-collision assembly (4) comprises an anti-collision fixing piece (4.1) arranged on two sides of the environment detection unmanned aerial vehicle body (1), the environment detection unmanned aerial vehicle body (1) and the anti-collision fixing piece (4.1) are fixedly connected through a plurality of fixing bolts (4.2), each anti-collision fixing piece (4.3) is internally fixed with the anti-collision fixing piece (4.1), each anti-collision fixing piece (4.1) is connected with an anti-collision plate (4.5) through a telescopic rod (4.3), each telescopic rod (4.3) is sleeved with a spring (4.4), each anti-collision plate (4.4) is provided with a cushion (4.6) on the surface, each anti-collision plate (7) is arranged in each anti-collision plate (1), each solar energy storage plate (8) is arranged above the environment detection unmanned aerial vehicle body (7) and arranged on the environment detection unmanned aerial vehicle body (1), each solar energy storage plate (8) and is arranged above the unmanned aerial vehicle body (8), one of them be equipped with motor (8.1) in fixed frame (8.8), the output shaft of motor (8.1) has hob (8.2), another fixed frame (8.8) interpolation is equipped with gag lever post (8.7), hob (8.2) and gag lever post (8.7) all overlap and are equipped with movable block (8.4), two connect through connecting rod (8.5) between movable block (8.4), connecting rod (8.5) surface is equipped with the pappus brush.
2. The anti-collision structure of the environmental reconnaissance unmanned aerial vehicle as claimed in claim 1, wherein: and the lower surface of the support frame (2) is fixed with an anti-skid pad.
3. The anti-collision structure of the environmental reconnaissance unmanned aerial vehicle as claimed in claim 1, wherein: fixed connection between the stiff end of anticollision mounting (4.1) and telescopic link (4.3), fixed connection between the flexible end of crashproof board (4.5) and telescopic link (4.3).
4. The anti-collision structure of the environmental reconnaissance unmanned aerial vehicle as claimed in claim 1, wherein: the spring (4.4) is in a natural extension state, one end of the spring (4.4) is fixedly connected with the anti-collision fixing piece (4.1), and the other end of the spring (4.4) is fixedly connected with the anti-collision plate (4.5).
5. The anti-collision structure of the environmental reconnaissance unmanned aerial vehicle according to claim 1, wherein a groove for the spring (4.4) to enter is formed in the anti-collision fixing piece (4.1) around the telescopic rod (4.3) and the spring (4.4).
6. The anti-collision structure of the environmental reconnaissance unmanned aerial vehicle as claimed in claim 1, wherein: the one end of pappus brush is kept away from connecting rod (8.5) and is hugged closely in solar energy accumulator plate (7) surface, be equipped with spacing recess (8.6) that cooperation movable block (8.4) and connecting rod (8.5) removed in fixed frame (8.8).
7. The anti-collision structure of the environmental reconnaissance unmanned aerial vehicle as claimed in claim 1, wherein: both ends of hob (8.2) and gag lever post (8.7) all overlap and are equipped with bearing (8.3), all be connected fixedly through bearing (8.3) between the both ends of fixed frame (8.8) and hob (8.2) and the both ends of gag lever post (8.7).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202222742229.5U CN218343736U (en) | 2022-10-18 | 2022-10-18 | Environmental investigation unmanned aerial vehicle's crashproof structure |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202222742229.5U CN218343736U (en) | 2022-10-18 | 2022-10-18 | Environmental investigation unmanned aerial vehicle's crashproof structure |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN218343736U true CN218343736U (en) | 2023-01-20 |
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ID=84897138
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202222742229.5U Active CN218343736U (en) | 2022-10-18 | 2022-10-18 | Environmental investigation unmanned aerial vehicle's crashproof structure |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN218343736U (en) |
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2022
- 2022-10-18 CN CN202222742229.5U patent/CN218343736U/en active Active
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