CN212074422U - Multi-purpose sampling environment monitoring unmanned aerial vehicle - Google Patents
Multi-purpose sampling environment monitoring unmanned aerial vehicle Download PDFInfo
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- CN212074422U CN212074422U CN202020639062.8U CN202020639062U CN212074422U CN 212074422 U CN212074422 U CN 212074422U CN 202020639062 U CN202020639062 U CN 202020639062U CN 212074422 U CN212074422 U CN 212074422U
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Abstract
The utility model discloses a multi-dwelling sampling environment monitoring unmanned aerial vehicle in the technical field of environment monitoring, which comprises a frame, a flying mechanism, a body, a connecting column, a mounting plate, a connecting shell, a connecting block, a movable rod, a damping block, a spring, a damping plate, an air monitor, an electric telescopic rod, a guide rod, a lifting plate, a water resource monitor, a clamping mechanism, a filter, an exhaust fan, an inserting rod, a lifting block, a reset spring, a positioning hole, a controller and a storage battery, wherein the outer walls of the left side and the right side of the connecting shell are movably inserted with the inserting rod, the outer walls of the left side and the right side of the mounting plate are provided with the positioning hole matched with the inserting rod, when the unmanned aerial vehicle is installed, the connecting shell is only required to be inserted into the mounting plate, the inclined plane slowly pushes the inserting rod outwards in the inserting process, the reset spring at the moment is in a stretching state, when the connecting shell is continuously inserted, and fixing the connecting shell at the bottom of the mounting plate.
Description
Technical Field
The utility model relates to an environmental monitoring technical field specifically is a sampling environment monitoring unmanned aerial vehicle perchs more.
Background
The existing unmanned aerial vehicle monitoring equipment is generally characterized in that a monitoring instrument is installed at the bottom of a rack, the environment is monitored after the unmanned aerial vehicle is lifted off, the monitoring equipment is complex to disassemble and assemble, the maintenance is time-consuming, the unmanned aerial vehicle is descended, the influence of the weight of the fuselage and the monitoring equipment is received, the impact force on the ground is large, the fuselage and circuit elements of the monitoring equipment are easily damaged, the maintenance period is shortened, the service life is prolonged, and therefore the multifunctional sampling environment monitoring unmanned aerial vehicle is provided.
SUMMERY OF THE UTILITY MODEL
An object of the utility model is to provide a sampling environmental monitoring unmanned aerial vehicle perchs more to solve the problem that proposes in the above-mentioned background art.
In order to achieve the above object, the utility model provides a following technical scheme: a multi-purpose sampling environment monitoring unmanned aerial vehicle comprises a frame, flight mechanisms, a body, connecting columns, mounting plates, a connecting shell, connecting blocks, movable rods, damping blocks, springs, damping plates, an air monitor, an electric telescopic rod, a guide rod, a lifting plate, a water resource monitor, a clamping mechanism, a filter, an exhaust fan, inserting rods, lifting blocks, reset springs, positioning holes, a controller and a storage battery, wherein the outer walls of the left side and the right side of the frame are respectively provided with a front group of flight mechanisms and a rear group of flight mechanisms, the body is arranged at the top of the frame, the four corners of the outer wall at the bottom of the frame are respectively provided with the connecting columns, the mounting plates are fixedly mounted at the bottoms of the four groups of connecting columns, the mounting plates are movably sleeved at the bottoms of the outer walls, the outer walls of the left side and the right side of the connecting shell are respectively movably inserted with the inserting rods, the two, the reset spring is sleeved on the outer wall of the inserted rod, the other end of the reset spring is fixedly connected with the outer wall of the connecting shell, the left side and the right side of the outer wall at the top of the mounting plate are both provided with inclined planes matched with the inserted rod, the outer walls at the left side and the right side of the mounting plate are both provided with positioning holes matched with the inserted rod, the center of the outer wall at the bottom of the connecting shell is provided with an air monitor, the left side and the right side of the outer wall at the bottom of the connecting shell are both provided with electric telescopic rods, the left side and the right side of the joint of the outer wall at the bottom of the connecting shell and the electric telescopic rods are both provided with guide rods, two adjacent groups of the outer walls of the guide rods are movably sleeved with lifting plates, the tops of the lifting plates are fixedly connected with the bottoms of the electric telescopic rods, the bottoms of the lifting, the storage battery, the air monitor, the water resource monitor, the clamping mechanism and the controller are electrically connected.
Further, connect shell left and right sides outer wall bottom all to be equipped with around two sets of connecting blocks, the connecting block bottom articulates there is the movable rod, controls two sets of homonymy the center of the relative one side outer wall of movable rod all is equipped with the damping piece, and the relative one side outer wall of two sets of damping pieces all is equipped with the spring, connect shell bottom outer wall left and right sides symmetry and be provided with the shock attenuation board, control two sets of homonymy the relative one end of spring and shock attenuation board fixed connection, air monitor, water resource monitor and clamp are got the mechanism and all are located two sets of shock attenuation inboard.
Furthermore, the centers of the outer walls of the left side and the right side of the connecting shell are respectively provided with a left mounting hole and a right mounting hole which are communicated, and a filter and an exhaust fan are respectively arranged in the left mounting hole and the right mounting hole.
Further, the movable rod bottom articulates there is the snubber block, the snubber block is cellular rubber piece, just snubber block bottom outer wall evenly is equipped with unsmooth form anti-skidding line.
Furthermore, control two sets of the homonymy the ball is installed through rotating the connecting piece to the relative one end of inserted bar, the mounting panel longitudinal section is isosceles trapezoid, and its top cross-sectional width is less than bottom cross-sectional width.
Compared with the prior art, the beneficial effects of the utility model are that:
1. when the connecting shell is installed, the connecting shell is only required to be inserted into the installing plate, the inclined surface slowly pushes out the inserting rod outwards in the inserting process, the reset spring is in a stretching state at the moment, when the connecting shell is continuously inserted, and the positioning hole is aligned with the inserting rod, the inserting rod is inserted into the positioning hole under the reset driving of the reset spring, the connecting shell is fixed at the bottom of the installing plate, and when the connecting shell is overhauled, the inserting rod is directly pulled outwards to be separated from the positioning hole and can be taken down;
2. the controller controls the electric telescopic rod to stretch out and draw back, so that the water resource monitor and the clamping mechanism cannot stretch out simultaneously, the clamping mechanism cannot stretch into water, the water resource monitor cannot collide with the ground, the controller controls the electric telescopic rod to shrink when the electric telescopic rod descends, the water resource monitor and the clamping mechanism retract, collision avoidance can be performed on the clamping mechanism, the air monitor detects the air quality, the water resource monitor monitors the water resource when the unmanned aerial vehicle stays on the water surface, the monitored data are fed back to the controller, the controller transmits the data to the ground computer through the wireless transmission module, the controller controls the clamping mechanism to act to clamp and clamp solid samples on the ground or at a high position, and multi-dwelling sampling is realized;
3. when unmanned aerial vehicle descends, the movable rod at first with ground contact, two sets of movable rods of the homonymy open to the outside this moment with the spring extension, the movable rod opens and decomposes into the horizontal force with the vertical impact that unmanned aerial vehicle descends, weakens through the elasticity that spring deformation produced and the frictional force between ground and the snubber block, plays the shock attenuation effect, protection unmanned aerial vehicle and monitoring facilities.
Drawings
FIG. 1 is a schematic structural view of the present invention;
fig. 2 is the installation schematic diagram of the installation plate and the connection shell of the present invention.
In the figure: 1. a frame; 2. a flying mechanism; 3. a body; 4. connecting columns; 5. mounting a plate; 6. a connecting shell; 7. connecting blocks; 8. a movable rod; 9. a damper block; 10. a spring; 11. a damper plate; 12. an air monitor; 13. an electric telescopic rod; 14. a guide bar; 15. a lifting plate; 16. a water resource monitor; 17. a gripping mechanism; 18. a filter; 19. an exhaust fan; 20. inserting a rod; 21. lifting the block; 22. a return spring; 23. positioning holes; 24. a controller; 25. and (4) a storage battery.
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.
The utility model provides a technical scheme: a multi-dwelling sampling environment monitoring unmanned aerial vehicle, please refer to fig. 1-2, which comprises a frame 1, a flying mechanism 2, a machine body 3, a connecting column 4, a mounting plate 5, a connecting shell 6, a connecting block 7, a movable rod 8, a damping block 9, a spring 10, a damping plate 11, an air monitor 12, an electric telescopic rod 13, a guide rod 14, a lifting plate 15, a water resource monitor 16, a clamping mechanism 17, a filter 18, an exhaust fan 19, an inserting rod 20, a lifting block 21, a reset spring 22, a positioning hole 23, a controller 24 and a storage battery 25, wherein the outer walls of the left side and the right side of the frame 1 are respectively provided with a front flying mechanism and a rear flying mechanism 2, the machine body 3 is arranged at the top of the frame 1, the connecting columns 4 are respectively arranged at the four corners of the outer wall of the bottom of the frame 1, the mounting plates 5 are fixedly arranged at the bottoms of the four, a lifting block 21 is fixedly arranged at the opposite end of two groups of insertion rods 20 at the left and right sides, a reset spring 22 is fixedly arranged at the joint of the lifting block 21 and the insertion rod 20, the reset spring 22 is sleeved on the outer wall of the insertion rod 20, the other end of the reset spring 22 is fixedly connected with the outer wall of the connecting shell 6, inclined planes matched with the insertion rod 20 are arranged at the left and right sides of the outer wall at the top of the mounting plate 5, positioning holes 23 matched with the insertion rod 20 are arranged at the outer walls at the left and right sides of the mounting plate 5, when the mounting plate is mounted, the connecting shell 6 only needs to be inserted into the mounting plate 5, the inclined planes slowly push the insertion rod 20 outwards in the insertion process, the reset spring 22 is in a stretching state, when the connecting shell 6 is continuously inserted and the positioning holes 23 are aligned with the insertion rods 20, the insertion rod 20 is driven by the reset of the reset spring 22, the inserting rod 20 is directly pulled outside to make the inserting rod 20 leave the positioning hole 23, and then the inserting rod can be taken down;
referring to fig. 1-2, an air monitor 12 is disposed at the center of the outer wall at the bottom of the connecting shell 6, electric telescopic rods 13 are disposed on the left and right sides of the outer wall at the bottom of the connecting shell 6, a controller 24 controls the electric telescopic rods 13 to extend and retract so that the water resource monitor 16 and the clamping mechanism 17 do not extend out at the same time and can be protected (the clamping mechanism 17 does not extend into the water and the water resource monitor 16 does not collide with the ground, the controller 24 controls the electric telescopic rods 13 to retract when descending so that the water resource monitor 16 and the clamping mechanism 17 retract and can perform anti-collision protection), guide rods 14 are disposed on the left and right sides of the joint of the outer wall at the bottom of the connecting shell 6 and the electric telescopic rods 13, lifting plates 15 are movably sleeved on the outer walls of two adjacent groups of the guide rods 14, the tops of the lifting plates 15 are fixedly connected with the bottoms, the air monitor 12 detects the air quality, the water resource monitor 16 detects when the unmanned aerial vehicle is stopped on the water surface, monitoring water resources, feeding monitored data back to the controller 24, transmitting the data to a ground computer by the controller 24 through a wireless transmission module, controlling the clamping mechanism 17 to move to clamp and take solid samples on the ground or at a high position (an unmanned aerial vehicle generally has a camera and carries out positioning clamping through the camera), wherein the clamping mechanism 17 is a common electric clamp, the controller 24 is arranged in the center of the inner wall of the bottom of the connecting shell 6, storage batteries 25 are arranged on the left side and the right side of the joint of the inner wall of the bottom of the connecting shell 6 and the controller 24, the storage batteries 25, the air monitor 12, the water resource monitor 16, the clamping mechanism 17 are electrically connected with the controller 24, and the air monitor 12, the water resource monitor 16 and the clamping mechanism 17 are all existing equipment and are not described further;
referring to fig. 1-2, the bottoms of the outer walls of the left side and the right side of the connecting shell 6 are respectively provided with a front connecting block 7 and a rear connecting block 7, the bottoms of the connecting blocks 7 are hinged with movable rods 8, the centers of the outer walls of the two groups of movable rods 8 on the same left side and the right side are respectively provided with a damping block, the outer walls of the two groups of damping blocks on the opposite sides are respectively provided with a spring 10, the damping plates 11 are symmetrically arranged on the left side and the right side of the outer wall of the bottom of the connecting shell 6, the opposite ends of the two groups of springs 10 on the same left side and the right side are fixedly connected with the damping plates 11, an air monitor 12, a water resource monitor 16 and a clamping mechanism 17 are positioned inside the two groups of damping plates 11, when the unmanned aerial vehicle descends, the movable rods 8;
referring to fig. 2, the centers of the outer walls of the left and right sides of the connecting shell 6 are provided with left and right through mounting holes, the left and right two sets of mounting holes are respectively provided with a filter 18 and an exhaust fan 19, the exhaust fan 19 can draw out air in the inner cavity of the connecting shell 6, and cool the working storage battery 25 and the controller 24;
referring to fig. 1, the bottom of the movable rod 8 is hinged with a damping block 9, the damping block 9 is a honeycomb rubber block, the damping block 9 also deforms when colliding with the ground, so that the impact force generated when the unmanned aerial vehicle lands can be further weakened, the outer wall of the bottom of the damping block 9 is uniformly provided with concave-convex anti-slip lines, the friction with the ground is increased, the movable rod 8 opens to decompose the vertical impact force generated when the unmanned aerial vehicle lands into horizontal force, the elastic force generated by the deformation of the spring 10 and the friction between the ground and the damping block 9 are weakened, and the damping effect is achieved;
referring to fig. 2, the opposite ends of the two sets of insertion rods 20 on the same side are provided with balls through the rotating connecting piece, the longitudinal section of the mounting plate 5 is isosceles trapezoid, the width of the top section is smaller than that of the bottom section, so that the friction force generated when the connecting shell 6 is inserted is reduced, and the connecting shell is smoothly disassembled.
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 (5)
1. The utility model provides a many dwelling sampling environmental monitoring unmanned aerial vehicle, including frame (1), flight mechanism (2), fuselage (3), spliced pole (4), mounting panel (5), joint housing (6), connecting block (7), movable rod (8), snubber block (9), spring (10), snubber plate (11), air monitor (12), electric telescopic handle (13), guide bar (14), lifter plate (15), water resource monitor (16), press from both sides and get mechanism (17), filter (18), air discharge fan (19), inserted bar (20), carry and draw piece (21), reset spring (22), locating hole (23), controller (24) and battery (25), its characterized in that: the aircraft is characterized in that the outer walls of the left side and the right side of the rack (1) are respectively provided with a front group of flight mechanisms and a rear group of flight mechanisms (2), the top of the rack (1) is provided with a machine body (3), four groups of connecting columns (4) are respectively arranged at four corners of the outer wall of the bottom of the rack (1), the mounting plates (5) are movably sleeved at the bottoms of the outer walls of the annular walls of the mounting plates (5), the outer walls of the left side and the right side of the connecting shell (6) are respectively movably inserted with an inserting rod (20), the opposite ends of the two groups of the inserting rods (20) at the same side are fixedly provided with a lifting block (21), a reset spring (22) is fixedly arranged at the joint of the lifting block (21) and the inserting rod (20), the reset spring (22) is sleeved at the outer wall of the inserting rod (20), the other end of the reset spring (22) is fixedly connected with the outer wall of the connecting shell, the mounting plate (5) is characterized in that positioning holes (23) matched with the inserting rods (20) are formed in the outer walls of the left side and the right side of the mounting plate (5), an air monitor (12) is arranged in the center of the outer wall of the bottom of the connecting shell (6), electric telescopic rods (13) are arranged on the left side and the right side of the outer wall of the bottom of the connecting shell (6), guide rods (14) are arranged on the left side and the right side of the joint of the outer wall of the bottom of the connecting shell (6) and the electric telescopic rods (13), lifting plates (15) are movably sleeved on the outer walls of two adjacent groups of the guide rods (14), the tops of the lifting plates (15) are fixedly connected with the bottoms of the electric telescopic rods (13), water resource monitors (16) and clamping mechanisms (17) are arranged at the bottoms of the lifting plates (15), a controller (24) is arranged at the center of the inner wall of the bottom of the connecting shell (, the storage battery (25), the air monitor (12), the water resource monitor (16), the clamping mechanism (17) and the controller (24) are electrically connected.
2. The benthic sampling environment monitoring unmanned aerial vehicle of claim 1, wherein: connect shell (6) left and right sides outer wall bottom all to be equipped with around two sets of connecting block (7), connecting block (7) bottom articulates there is movable rod (8), controls two sets of homonymy the center of the relative one side outer wall of movable rod (8) all is equipped with the damping piece, and two sets of relative one side outer wall of damping piece all is equipped with spring (10), connect shell (6) bottom outer wall left and right sides symmetry is provided with shock attenuation board (11), controls two sets of homonymy the relative one end of spring (10) and shock attenuation board (11) fixed connection, air monitor (12), water resource monitor (16) and clamp are got mechanism (17) and all are located two sets of shock attenuation board (11) inboardly.
3. The benthic sampling environment monitoring unmanned aerial vehicle of claim 1, wherein: the connecting shell (6) is characterized in that the centers of the outer walls of the left side and the right side of the connecting shell are respectively provided with a left mounting hole and a right mounting hole which are communicated, and a filter (18) and an exhaust fan (19) are respectively arranged in the left mounting hole and the right mounting hole.
4. The benthic sampling environment monitoring unmanned aerial vehicle of claim 2, wherein: the utility model discloses a damping device, including movable rod (8), snubber block (9) are articulated to movable rod (8) bottom, snubber block (9) are cellular rubber block, just snubber block (9) bottom outer wall evenly is equipped with unsmooth form anti-skidding line.
5. The benthic sampling environment monitoring unmanned aerial vehicle of claim 1, wherein: control two sets of homonymy the ball is installed through rotating the connecting piece to the relative one end of inserted bar (20), mounting panel (5) longitudinal section is isosceles trapezoid, and its top cross-sectional width is less than bottom cross-sectional width.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202020639062.8U CN212074422U (en) | 2020-04-24 | 2020-04-24 | Multi-purpose sampling environment monitoring unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202020639062.8U CN212074422U (en) | 2020-04-24 | 2020-04-24 | Multi-purpose sampling environment monitoring unmanned aerial vehicle |
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| Publication Number | Publication Date |
|---|---|
| CN212074422U true CN212074422U (en) | 2020-12-04 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202020639062.8U Expired - Fee Related CN212074422U (en) | 2020-04-24 | 2020-04-24 | Multi-purpose sampling environment monitoring unmanned aerial vehicle |
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| CN (1) | CN212074422U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113866840A (en) * | 2021-09-11 | 2021-12-31 | 张君碧 | Dangerous solid waste detection equipment for building field |
-
2020
- 2020-04-24 CN CN202020639062.8U patent/CN212074422U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113866840A (en) * | 2021-09-11 | 2021-12-31 | 张君碧 | Dangerous solid waste detection equipment for building field |
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| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20201204 Termination date: 20210424 |
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| CF01 | Termination of patent right due to non-payment of annual fee |