CN214165282U - Unmanned aerial vehicle for environmental monitoring based on remote sensing image - Google Patents
Unmanned aerial vehicle for environmental monitoring based on remote sensing image Download PDFInfo
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- CN214165282U CN214165282U CN202120091118.5U CN202120091118U CN214165282U CN 214165282 U CN214165282 U CN 214165282U CN 202120091118 U CN202120091118 U CN 202120091118U CN 214165282 U CN214165282 U CN 214165282U
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- unmanned aerial
- aerial vehicle
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- remote sensing
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- 230000007613 environmental effect Effects 0.000 title claims abstract description 23
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- 238000013016 damping Methods 0.000 claims description 15
- 238000010521 absorption reaction Methods 0.000 claims description 11
- 239000002184 metal Substances 0.000 claims description 8
- 239000011247 coating layer Substances 0.000 claims description 7
- 239000011248 coating agent Substances 0.000 claims 1
- 238000000576 coating method Methods 0.000 claims 1
- 238000012876 topography Methods 0.000 abstract description 6
- 230000007246 mechanism Effects 0.000 description 9
- 239000012528 membrane Substances 0.000 description 6
- 238000004078 waterproofing Methods 0.000 description 3
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- 230000009286 beneficial effect Effects 0.000 description 1
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- 230000001771 impaired effect Effects 0.000 description 1
- 238000011065 in-situ storage Methods 0.000 description 1
- 208000015181 infectious disease Diseases 0.000 description 1
- 230000008595 infiltration Effects 0.000 description 1
- 238000001764 infiltration Methods 0.000 description 1
- 238000007689 inspection Methods 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
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- 238000012986 modification Methods 0.000 description 1
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Abstract
The utility model discloses an unmanned aerial vehicle for environmental monitoring based on remote sensing image, including fuselage shell, connecting rod and damper, fuselage shell both sides surface is equal fixedly connected with connecting piece, the connecting piece is provided with four, four the inside internal thread that all is provided with of connecting piece, and four the connecting piece is kept away from the one end of fuselage shell all is connected with through the internal thread screw thread the connecting rod, the connecting rod lower surface is kept away from the one end of connecting piece is provided with damper, the damper lower extreme is provided with the lifting base, the damper upper end is provided with the screw, the utility model discloses an one end of keeping away from fuselage shell at four connecting rod lower surfaces all is provided with damper, when unmanned aerial vehicle meets comparatively abominable topography, can carry out shock attenuation processing to the collision that unmanned aerial vehicle when descending and bottom surface produced through damper, prevent that unmanned aerial vehicle from damaging, cause the loss.
Description
Technical Field
The utility model belongs to the technical field of environmental monitoring, concretely relates to unmanned aerial vehicle for environmental monitoring based on remote sensing image.
Background
An unmanned aircraft, abbreviated as "drone", and abbreviated in english as "UAV", is an unmanned aircraft that is operated by a radio remote control device and a self-contained program control device, or is operated autonomously, either completely or intermittently, by an onboard computer. Drones tend to be more suitable for tasks that are too "fool, dirty, or dangerous" than are manned aircraft. Unmanned aerial vehicles can be classified into military and civil applications according to the application field. For military use, unmanned aerial vehicles divide into reconnaissance aircraft and target drone. In the civil aspect, the unmanned aerial vehicle + the industry application is really just needed by the unmanned aerial vehicle; at present, the unmanned aerial vehicle is applied to the fields of aerial photography, agriculture, plant protection, miniature self-timer, express transportation, disaster relief, wild animal observation, infectious disease monitoring, surveying and mapping, news reporting, power inspection, disaster relief, film and television shooting, romantic manufacturing and the like, the application of the unmanned aerial vehicle is greatly expanded, and developed countries actively expand industrial application and develop unmanned aerial vehicle technology.
Unmanned aerial vehicle that current environmental monitoring used, the protectiveness is relatively poor, when meetting abominable topography, unmanned aerial vehicle very easily damages the unmanned aerial vehicle bottom plate when descending, leads to unmanned aerial vehicle to be unable, and is comparatively troublesome.
SUMMERY OF THE UTILITY MODEL
The to-be-solved technical problem of the utility model is to overcome current defect, provide an unmanned aerial vehicle for environmental monitoring based on remote sensing image to solve the problem that the unmanned aerial vehicle descends and damages the bottom plate when meetting the bad topography that provides in the above-mentioned background art.
In order to achieve the above object, the utility model provides a following technical scheme: the utility model provides an unmanned aerial vehicle for environmental monitoring based on remote sensing image, includes fuselage shell, connecting rod and damper, the equal fixedly connected with connecting piece in fuselage shell both sides surface, the connecting piece is provided with four, four the inside internal thread that all is provided with of connecting piece, and four the connecting piece is kept away from the one end of fuselage shell all has through internal thread threaded connection the connecting rod, the connecting rod lower surface is kept away from the one end of connecting piece is provided with damper, the damper lower extreme is provided with the base that rises and falls, the damper upper end is provided with the screw.
Preferably, damper includes spliced pole, support column, shock attenuation groove, shock attenuation telescopic link and damping spring, just the support column is inside to be seted up the shock attenuation groove, the shock attenuation inslot portion is provided with the spliced pole.
Preferably, the damping telescopic rod is arranged between the connecting column and the bottom end inside the damping groove, and a damping spring is arranged on the surface of the damping telescopic rod.
Preferably, the middle part of the lower end of the body shell is provided with a camera, a camera sensor chip is arranged in the camera, and an infrared sensor is arranged on the surface of one side of the camera.
Preferably, the outermost side of the surface of the fuselage shell is provided with a waterproof film.
Preferably, the inner side of the waterproof film is provided with a coating layer, and the inner side of the coating layer is provided with a breathable layer.
Preferably, a metal layer is arranged on the inner side of the breathable layer.
Compared with the prior art, the utility model provides an unmanned aerial vehicle for environmental monitoring based on remote sensing image possesses following beneficial effect:
1. the utility model discloses a keep away from the one end of fuselage shell all to be provided with damper under four connecting rods, when meeting comparatively abominable topography when unmanned aerial vehicle descends, can carry out the shock attenuation through damper with the collision that the bottom surface produced when unmanned aerial vehicle descends, prevent that unmanned aerial vehicle from damaging, cause the loss, through being provided with the base that rises and falls at the damper lower extreme, make unmanned aerial vehicle more stable when descending, can not take place to turn on one's side;
2. the utility model discloses a be provided with waterproof membrane in fuselage shell's the outside, can effectually prevent through waterproof membrane that unmanned aerial vehicle from entering into inside unmanned aerial vehicle fuselage shell when surging, cause the damage of unmanned aerial vehicle's inside water circuit of intaking, lead to unmanned aerial vehicle to damage, through be provided with the dope layer in waterproof membrane inboard, increased unmanned aerial vehicle's aesthetic property;
3. the utility model discloses a be provided with ventilative layer in the dope layer inboard, when unmanned aerial vehicle is when the operation, the inside a large amount of heats that can produce of fuselage shell, distribute away the heat through ventilative layer is convenient, unmanned aerial vehicle's life has been increased, through be provided with the metal level at ventilative in situ side, unmanned aerial vehicle fuselage shell's tightness has been increased, when unmanned aerial vehicle bumps, the effectual unmanned aerial vehicle internals of having guaranteed are not damaged, through being provided with camera sensor chip inside the camera, the convenience is through the camera to the region that needs carry out environmental monitoring taking an aerial photograph, through being provided with infrared inductor on one side of the camera, make unmanned aerial vehicle can carry out the task at night.
Drawings
The accompanying drawings are included to provide a further understanding of the invention, and are incorporated in and constitute a part of this specification, illustrate embodiments of the invention, and together with the description, do not constitute a limitation of the invention, in which:
fig. 1 is a schematic structural view of the unmanned aerial vehicle for environmental monitoring based on remote sensing images provided by the present invention;
fig. 2 is a front view of a body shell of the unmanned aerial vehicle for environmental monitoring based on remote sensing images, provided by the utility model;
fig. 3 is a schematic view of a material structure of a body shell of the unmanned aerial vehicle for environmental monitoring based on remote sensing images according to the present invention;
fig. 4 is a schematic structural view of a damping mechanism in the unmanned aerial vehicle for environmental monitoring based on remote sensing images provided by the utility model;
in the figure: 1. a fuselage shell; 2. a waterproof film; 3. a coating layer; 4. a breathable layer; 5. a metal layer; 6. a connecting member; 7. a connecting rod; 8. a propeller; 9. a damping mechanism; 91. connecting columns; 92. a support pillar; 93. a damping groove; 94. a shock-absorbing telescopic rod; 95. a damping spring; 10. a lifting base; 11. a camera; 12. an infrared sensor.
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.
Referring to fig. 1-4, the present invention provides a technical solution: an unmanned aerial vehicle for environmental monitoring based on remote sensing images comprises a body shell 1, connecting rods 7 and shock absorption mechanisms 9, wherein the surfaces of the two sides of the body shell 1 are fixedly connected with connecting pieces 6, the number of the connecting pieces 6 is four, internal threads are arranged inside the four connecting pieces 6, one ends of the four connecting pieces 6, which are far away from the body shell 1, are connected with the connecting rods 7 through the internal threads, the shock absorption mechanisms 9 are arranged at the ends, which are far away from the connecting pieces 6, of the lower surfaces of the connecting rods 7, the lower ends of the shock absorption mechanisms 9 are provided with lifting bases 10, and the upper ends of the shock absorption mechanisms 9 are provided with propellers 8, the utility model discloses a shock absorption mechanism 9 is arranged at one end, which is far away from the body shell 1, of the lower surfaces of the four connecting rods 7, when the unmanned aerial vehicle lands in severe terrains, the shock absorption treatment can be carried out on the collision generated by the landing and the bottom surface of the unmanned aerial vehicle through the shock absorption mechanism 9, prevent that unmanned aerial vehicle from damaging, cause the loss, through be provided with the base 10 that rises and falls at the 9 lower extremes of damper, it is more stable when making unmanned aerial vehicle descend, can not take place to turn on one's side.
The utility model discloses in, preferred, damper 9 includes spliced pole 91, support column 92, damping groove 93, shock attenuation telescopic link 94 and damping spring 95, and support column 92 is inside to have seted up damping groove 93, and damping groove 93 is inside to be provided with spliced pole 91.
The utility model discloses in, it is preferred, be provided with shock attenuation telescopic link 94 between spliced pole 91 and the inside bottom of shock attenuation groove 93, shock attenuation telescopic link 94 surface is provided with damping spring 95.
The utility model discloses in, preferred, 1 lower extreme mid portion of fuselage shell is provided with camera 11, the inside camera sensor chip that is provided with of camera 11, and 11 a side surfaces of camera are provided with infrared inductor 12, through being provided with camera sensor chip in 11 insides of camera, conveniently carry out the region of environmental monitoring through camera 11 to needs and take photo by plane, through being provided with infrared inductor 12 in 11 one sides of camera, make unmanned aerial vehicle can carry out the task at night.
The utility model discloses in, preferred, 1 surface of fuselage shell is provided with waterproofing membrane 2 in the outside, and when unmanned aerial vehicle was when carrying out the task, the moisture of doping in the air can permeate inside 1 fuselage shell of unmanned aerial vehicle, sets up inside waterproofing membrane 2 can effectually prevent moisture infiltration fuselage shell 1, has increased unmanned aerial vehicle's security.
The utility model discloses in, preferred, 2 inboards of waterproofing membrane are provided with dope layer 3, have increased unmanned aerial vehicle's aesthetic property, 3 inboards of dope layer are provided with ventilative layer 4, when unmanned aerial vehicle long-time operation inside can produce a large amount of heats, through setting up ventilative layer 4 can effectual increase unmanned aerial vehicle fuselage shell 1's gas permeability, place the too high life that leads to influencing unmanned aerial vehicle of 1 surface temperature of unmanned aerial vehicle fuselage shell.
The utility model discloses in, preferred, 4 inboards on ventilative layer are provided with metal level 5, through setting up metal level 5, the effectual tightness that increases unmanned aerial vehicle fuselage shell 1, when unmanned aerial vehicle unfortunate bumps, metal level 5 can effectually guarantee that the part of unmanned aerial vehicle fuselage shell 1 inside can not be impaired.
The utility model discloses a theory of operation and use flow: when the unmanned aerial vehicle is used, the unmanned aerial vehicle is placed on the flat ground, then the unmanned aerial vehicle is started through remote control, the four propellers 8 start to rotate, the unmanned aerial vehicle starts to take off, when the unmanned aerial vehicle moves to the upper part of a region needing aerial photography, the region is aerial photographed through the camera 11, the waterproof film 2 arranged on the outer side of the body shell 1 can effectively prevent moisture in the air from entering the interior of the unmanned aerial vehicle through the body shell 1 to cause water inlet short circuit in the unmanned aerial vehicle and damage, the coating layer 3 arranged on the inner side of the waterproof film 2 can increase the attractiveness of the unmanned aerial vehicle, after the unmanned aerial vehicle runs for a long time, a large amount of heat can be generated in the interior, the breathable layer 4 arranged on the inner side of the coating layer 3 can effectively dissipate the heat, the service life of the unmanned aerial vehicle is effectively prolonged, when the unmanned aerial vehicle is in case of unfortunate collision, the metal layer 5 arranged on the inner side of the breathable layer 4 can effectively protect parts in the body shell 1 of the unmanned aerial vehicle, make unmanned aerial vehicle safer, after the aerial photography, unmanned aerial vehicle need descend, and when the topography of landing point is comparatively abominable, the shock-absorbing mechanism 9 of setting in the base 10 upper end of rising and falling can effectually carry out the shock attenuation processing to the collision dynamics that produces when unmanned aerial vehicle descends, effectually prevent that unmanned aerial vehicle from descending to the comparatively abominable landing point in topography time, unmanned aerial vehicle's bottom surface damages, cause the unmanned aerial vehicle to damage, and the base 10 of rising and falling can effectually guarantee that unmanned aerial vehicle is more steady when descending.
The model of the camera sensor chip is OV7949, and the manufacturer is Shenzhen large Mongolian science and technology Limited.
Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that changes, modifications, substitutions and alterations can be made in these embodiments without departing from the principles and spirit of the invention, the scope of which is defined in the appended claims and their equivalents.
Claims (7)
1. The utility model provides an unmanned aerial vehicle for environmental monitoring based on remote sensing image, includes fuselage shell (1), connecting rod (7) and damper (9), its characterized in that: fuselage shell (1) both sides equal fixedly connected with connecting piece in surface (6), connecting piece (6) are provided with four, four connecting piece (6) are inside all to be provided with the internal thread, and four connecting piece (6) are kept away from the one end of fuselage shell (1) all has through internal thread threaded connection connecting rod (7), connecting rod (7) lower surface is kept away from the one end of connecting piece (6) is provided with damper (9), damper (9) lower extreme is provided with the base (10) that rises and falls, damper (9) upper end is provided with screw (8).
2. The unmanned aerial vehicle for environmental monitoring based on remote sensing image of claim 1, characterized in that: damper (9) are including spliced pole (91), support column (92), shock attenuation groove (93), shock attenuation telescopic link (94) and damping spring (95), just support column (92) are inside to be seted up shock attenuation groove (93), shock attenuation groove (93) are inside to be provided with spliced pole (91).
3. The unmanned aerial vehicle for environmental monitoring based on remote sensing image of claim 2, characterized in that: the shock absorption telescopic rod (94) is arranged between the connecting column (91) and the bottom end inside the shock absorption groove (93), and a shock absorption spring (95) is arranged on the surface of the shock absorption telescopic rod (94).
4. The unmanned aerial vehicle for environmental monitoring based on remote sensing image of claim 1, characterized in that: the camera is characterized in that a camera (11) is arranged in the middle of the lower end of the machine body shell (1), a camera sensor chip is arranged inside the camera (11), and an infrared inductor (12) is arranged on the surface of one side of the camera (11).
5. The unmanned aerial vehicle for environmental monitoring based on remote sensing image of claim 1, characterized in that: and a waterproof film (2) is arranged on the outermost side of the surface of the machine body shell (1).
6. The unmanned aerial vehicle for environmental monitoring based on remote sensing image of claim 5, characterized in that: the waterproof coating is characterized in that a coating layer (3) is arranged on the inner side of the waterproof film (2), and a breathable layer (4) is arranged on the inner side of the coating layer (3).
7. The unmanned aerial vehicle for environmental monitoring based on remote sensing image of claim 6, characterized in that: and a metal layer (5) is arranged on the inner side of the breathable layer (4).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202120091118.5U CN214165282U (en) | 2021-01-13 | 2021-01-13 | Unmanned aerial vehicle for environmental monitoring based on remote sensing image |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202120091118.5U CN214165282U (en) | 2021-01-13 | 2021-01-13 | Unmanned aerial vehicle for environmental monitoring based on remote sensing image |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN214165282U true CN214165282U (en) | 2021-09-10 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202120091118.5U Expired - Fee Related CN214165282U (en) | 2021-01-13 | 2021-01-13 | Unmanned aerial vehicle for environmental monitoring based on remote sensing image |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN214165282U (en) |
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2021
- 2021-01-13 CN CN202120091118.5U patent/CN214165282U/en not_active Expired - Fee Related
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| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20210910 |
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| CF01 | Termination of patent right due to non-payment of annual fee |