CN212195900U - Unmanned aerial vehicle formula pollution sources monitoring devices based on satellite positioning - Google Patents
Unmanned aerial vehicle formula pollution sources monitoring devices based on satellite positioning Download PDFInfo
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- CN212195900U CN212195900U CN202020554467.1U CN202020554467U CN212195900U CN 212195900 U CN212195900 U CN 212195900U CN 202020554467 U CN202020554467 U CN 202020554467U CN 212195900 U CN212195900 U CN 212195900U
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Abstract
The utility model discloses an unmanned aerial vehicle formula pollution sources monitoring devices based on satellite positioning, including the unmanned aerial vehicle body, the screw is installed respectively all around to the surface of unmanned aerial vehicle body, and the bottom fixed mounting of its unmanned aerial vehicle body has first module box body, and the preceding terminal surface fixedly connected with camera of first module box body, sampling mechanism is installed to the bottom of first module box body, and sampling mechanism's inside including the sampling tube, the bottom gomphosis of sampling tube is connected with the feed inlet, and the rubber buffer has been cup jointed in the inside activity of sampling tube, the top fixedly connected with electric telescopic handle of rubber buffer. The utility model discloses in, under sampling mechanism's effect, can drive the rubber stopper and go up and down to remove in the sampling tube through electric telescopic handle, place the sampling tube in water, can make the sampling tube take a sample to the water in pollution sources through the rubber buffer, change the phenomenon of artifical sample in the past, the staff of being convenient for carries out the test analysis to the water in pollution sources.
Description
Technical Field
The utility model relates to an unmanned aerial vehicle monitoring facilities technical field especially relates to an unmanned aerial vehicle formula pollution sources monitoring devices based on satellite positioning.
Background
A piloted aircraft, called unmanned aerial vehicle for short, is an unmanned aircraft operated by a radio remote control device and a self-contained program control device, or is completely or intermittently and autonomously operated by an on-board computer, and in the process of environmental monitoring, the environment is usually monitored by a camera unmanned aerial vehicle with satellite positioning.
Current unmanned aerial vehicle formula pollution sources monitoring devices at its in-process that uses, though can carry out real-time supervision to the environment through camera and display device, nevertheless can't take a sample to the water of its pollution sources, and unmanned aerial vehicle can't stop at the surface of water.
SUMMERY OF THE UTILITY MODEL
An object of the utility model is to prior art's weak point, provide an unmanned aerial vehicle formula pollution sources monitoring devices based on satellite positioning to reach the purpose in the pollution sources sample.
In order to achieve the above purpose, the utility model adopts the following technical scheme: an unmanned aerial vehicle type pollution source monitoring device based on satellite positioning comprises an unmanned aerial vehicle body, wherein propellers are respectively arranged on the periphery of the surface of the unmanned aerial vehicle body, a component module box body is fixedly arranged at the bottom end of the unmanned aerial vehicle body, a camera is fixedly connected with the front end face of the component module box body, a sampling mechanism is arranged at the bottom end of the component module box body, a sampling tube is arranged in the sampling mechanism, the bottom end of the sampling tube is connected with a feed inlet in an embedded mode, a rubber plug is movably sleeved in the sampling tube, an electric telescopic rod is fixedly connected with the top end of the rubber plug, the electric telescopic rod penetrates through the bottom end of the component module box body and is fixedly sleeved with the interior of the component module box body, one side of the electric telescopic rod is electrically connected with a PLC control panel, the PLC control panel is fixedly connected with the interior of the component module box body, and the rubber plug forms a, and an adjusting mechanism is arranged between the sampling tube and the element device module box body.
As a further description of the above technical solution:
the top gomphosis of unmanned aerial vehicle body is connected with the signal structure module, the bottom fixedly connected with bracing piece of its unmanned aerial vehicle body, and the bottom fixedly connected with backing plate of bracing piece, the relocation mechanism is installed to the bottom of backing plate.
As a further description of the above technical solution:
the inside of relocation mechanism is including the spout, and is connected for the gomphosis between the bottom of spout and backing plate, the inside cup joint of spout is inserted and is equipped with the slider, and the bottom fixed welding of its slider has the mounting panel, and the bottom fixedly connected with air cushion of mounting panel, the top threaded connection of backing plate has the hand to twist the bolt, and the hand is twisted the bolt and is passed for swing joint between spout and the slider.
As a further description of the above technical solution:
be the parallel form between mounting panel and the unmanned aerial vehicle body, and the mounting panel passes through to constitute sliding structure between slider and the spout.
As a further description of the above technical solution:
adjustment mechanism's inside is including two axis of rotation, and is fixed connection between the bottom of axis of rotation component ware module box body respectively, the bottom of axis of rotation is rotated and is fixed with the sleeve pipe, and sheathed tube internal thread is connected with the threaded rod, fixedly connected with layer board between two threaded rods, and be gomphosis fixed connection between the surface of layer board and sampling tube.
As a further description of the above technical solution:
the layer board passes through to constitute elevation structure between threaded rod and the sleeve pipe, and the sleeve pipe passes through to constitute revolution mechanic between axis of rotation and the first ware module box body.
To sum up, owing to adopted above-mentioned technical scheme, the beneficial effects of the utility model are that:
1. the utility model discloses in, under sampling mechanism's effect, can drive the rubber stopper and go up and down to remove in the sampling tube through electric telescopic handle, place the sampling tube in water, can make the sampling tube take a sample to the water in pollution sources through the rubber buffer, change the phenomenon of artifical sample in the past, the staff of being convenient for carries out the test analysis to the water in pollution sources.
2. The utility model discloses in, under the effect of relocation mechanism, can make unmanned aerial vehicle body 1 carry out work at the surface of water through the air cushion, prevent that unmanned aerial vehicle from causing the damage in falling into water, and twist the bolt through the rotation hand, can be swift dismantle the air cushion, the unmanned aerial vehicle body of being convenient for monitors the operation under the operational environment of difference.
3. The utility model discloses in, under adjustment mechanism's effect, through rotating the sleeve pipe, can be so that sheathed tube inside threaded rod goes up and down to move, make its sampling tube that is driving in the layer board carry out altitude mixture control, prevent that the sampling tube can't contact with the surface of water at the in-process that uses to prevent that the sampling tube position from crossing low excessively, cause unmanned aerial vehicle's empting when the land stops to fall.
Drawings
FIG. 1 is a schematic structural view of the present invention;
FIG. 2 is a schematic structural view of a sampling mechanism and a floating mechanism according to the present invention;
fig. 3 is a schematic structural diagram of the floating mechanism of the present invention.
Illustration of the drawings:
1. an unmanned aerial vehicle body; 2. a propeller; 3. a component module box; 4. a camera; 5. a signal structure module; 6. a support bar; 7. a base plate; 8. a sampling mechanism; 801. a sampling tube; 802. a feed inlet; 803. a rubber plug; 804. an electric telescopic rod; 805. a PLC control panel; 9. a floating mechanism; 901. a chute; 902. a slider; 903. mounting a plate; 904. an air cushion; 905. screwing the bolt by hand; 10. an adjustment mechanism; 1001. a rotating shaft; 1002. a sleeve; 1003. a threaded rod; 1004. and (7) a supporting plate.
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 of the present invention, all other embodiments obtained by a person of ordinary skill in the art without creative efforts belong to the protection scope of the present invention.
Referring to fig. 1-3, an unmanned aerial vehicle type pollution source monitoring device based on satellite positioning comprises an unmanned aerial vehicle body 1, propellers 2 are respectively installed on the periphery of the surface of the unmanned aerial vehicle body 1, a component module box body 3 is fixedly installed at the bottom end of the unmanned aerial vehicle body 1, a camera 4 is fixedly connected to the front end face of the component module box body 3, a sampling mechanism 8 is installed at the bottom end of the component module box body 3, a sampling pipe 801 is arranged inside the sampling mechanism 8, a feed inlet 802 is connected to the bottom end of the sampling pipe 801 in an embedded mode, a rubber plug 803 is movably sleeved inside the sampling pipe 801, an electric telescopic rod 804 is fixedly connected to the top end of the rubber plug 803, the electric telescopic rod 804 penetrates through the bottom end of the component module box body 3 and is fixedly sleeved inside the component module box body, a PLC control panel 805 is electrically connected to one side of the electric telescopic rod 804, and the PLC control panel 805, rubber buffer 803 passes through electric telescopic handle 804 and constitutes elevation structure between the unit ware module box body 3, install adjustment mechanism 10 between sampling tube 801 and the unit ware module box body 3, be equipped with the control components and parts of unmanned aerial vehicle body 1 in the unit ware module box body 3, can make unmanned aerial vehicle body 1 accept satellite positioning information through current technique, can shoot the environment through camera 4, convey to the cell-phone of staff through current unlimited technique and show, unit ware module electric connection in PLC control panel 805 and the unit ware module box body 3, but control electric telescopic handle 804's work, make it drive rubber buffer 803 and move in sampling tube 801 that stretches out and draws back.
Further, the top gomphosis of unmanned aerial vehicle body 1 is connected with signal structure module 5, and the bottom fixedly connected with bracing piece 6 of its unmanned aerial vehicle body 1, and the bottom fixedly connected with backing plate 7 of bracing piece 6, and relocation mechanism 9 is installed to the bottom of backing plate 7, through backing plate 7 and bracing piece 6, can be so that unmanned aerial vehicle body 1 stops to ground.
Further, the inside of floating machanism 9 is including spout 901, and be connected for the gomphosis between spout 901 and backing plate 7's the bottom, the inside of spout 901 is cup jointed and is inserted and is equipped with slider 902, the bottom mounting welding of its slider 902 has mounting panel 903, and the bottom fixedly connected with air cushion 904 of mounting panel 903, the top end threaded connection of backing plate 7 has hand to twist bolt 905, and hand is twisted bolt 905 and is passed for swing joint between spout 901 and the slider 902, can support unmanned aerial vehicle body 1 through air cushion 904, make it float on the surface of water and stop.
Further, be the parallel form between mounting panel 903 and the unmanned aerial vehicle body 1, and mounting panel 903 passes through and constitutes sliding structure between slider 902 and the spout 901, the installation and the dismantlement of the air cushion 904 of being convenient for.
Further, adjustment mechanism 10's inside is including two axis of rotation 1001, and is fixed connection between the axis of rotation 1001 is the bottom of first ware module box body 3 respectively, and the bottom of axis of rotation 1001 is rotated and is fixed with sleeve pipe 1002, and the internal thread of sleeve pipe 1002 is connected with threaded rod 1003, fixedly connected with layer board 1004 between two threaded rod 1003, and be gomphosis fixed connection between the surface of layer board 1004 and sampling tube 801, and the axis of rotation sleeve 1002 can make inside threaded rod 1003 lift and drop.
Further, the supporting plate 1004 forms a lifting structure through the threaded rod 1003 and the sleeve 1002, the sleeve 1002 forms a rotating structure through the rotating shaft 1001 and the element module box body 3, and the threaded rod 1003 can drive the sampling tube 801 to perform height adjustment.
The working principle is as follows: when in use, firstly, the sliding blocks 902 at the top ends of the two mounting plates 903 are manually inserted into the sliding grooves 901 at the bottom ends of the backing plates 7 respectively, then the bolts 905 are manually turned to fix and lock the sliding blocks 902, by manually rotating the sleeve 1002, the sleeve 1002 rotates through the rotating shaft 1001, the internal threaded rod 1003 moves up and down, the threaded rod 1003 drives the sampling tube 801 in the supporting plate 1004 to adjust the height of the sampling tube 801 to a position parallel to the bottom end of the air cushion 904, when the unmanned aerial vehicle body 1 encounters a pollution source in the monitoring process, the unmanned aerial vehicle body 1 stops on the water surface through the air cushion 904 at the bottom end, through PLC control panel 805 control electric telescopic handle 804 operation, electric telescopic handle 804 drives rubber buffer 803 rebound in sampling tube 801, with water through feed inlet 802 inhale sampling tube 801 in, take a sample to the water in pollution sources, just so accomplished the utility model discloses a theory of operation.
The above, only be the concrete implementation of the preferred embodiment of the present invention, but the protection scope of the present invention is not limited thereto, and any person skilled in the art is in the technical scope of the present invention, according to the technical solution of the present invention and the utility model, the concept of which is equivalent to replace or change, should be covered within the protection scope of the present invention.
Claims (6)
1. An unmanned aerial vehicle type pollution source monitoring device based on satellite positioning comprises an unmanned aerial vehicle body (1) and is characterized in that propellers (2) are respectively installed on the periphery of the surface of the unmanned aerial vehicle body (1), a component module box body (3) is fixedly installed at the bottom end of the unmanned aerial vehicle body (1), a camera (4) is fixedly connected to the front end face of the component module box body (3), a sampling mechanism (8) is installed at the bottom end of the component module box body (3), a sampling tube (801) is arranged inside the sampling mechanism (8), a feed inlet (802) is connected to the bottom end of the sampling tube (801) in an embedded mode, a rubber plug (803) is sleeved on the inner portion of the sampling tube (801) in a movable mode, an electric telescopic rod (804) is fixedly connected to the top end of the rubber plug (803), and the electric telescopic rod (804) penetrates through the bottom end of the component module box body (3) and, one side electric connection of electric telescopic handle (804) has PLC control panel (805), and is fixed connection between the inside of PLC control panel (805) and first ware module box body (3), rubber buffer (803) pass through and constitute elevation structure between electric telescopic handle (804) and first ware module box body (3), install adjustment mechanism (10) between sampling tube (801) and first ware module box body (3).
2. The unmanned aerial vehicle type pollution source monitoring device based on satellite positioning as claimed in claim 1, wherein the top end of the unmanned aerial vehicle body (1) is connected with a signal structure module (5) in an embedded manner, the bottom end of the unmanned aerial vehicle body (1) is fixedly connected with a support rod (6), the bottom end of the support rod (6) is fixedly connected with a backing plate (7), and the bottom end of the backing plate (7) is provided with a floating mechanism (9).
3. The unmanned aerial vehicle type pollution source monitoring device based on satellite positioning as claimed in claim 2, wherein the floating mechanism (9) comprises a sliding groove (901), the sliding groove (901) is connected with the bottom end of the backing plate (7) in an embedded manner, a sliding block (902) is inserted into the sliding groove (901), a mounting plate (903) is fixedly welded to the bottom end of the sliding block (902), an air cushion (904) is fixedly connected to the bottom end of the mounting plate (903), a hand-screwed bolt (905) is connected to the top end of the backing plate (7) in a threaded manner, and the hand-screwed bolt (905) penetrates through the sliding groove (901) and is movably connected with the sliding block (902).
4. The unmanned aerial vehicle type pollution source monitoring device based on satellite positioning as claimed in claim 3, wherein the mounting plate (903) and the unmanned aerial vehicle body (1) are parallel, and the mounting plate (903) passes through a sliding structure formed between the sliding block (902) and the sliding groove (901).
5. The unmanned aerial vehicle type pollution source monitoring device based on satellite positioning as claimed in claim 1, wherein the inside of the adjusting mechanism (10) comprises two rotating shafts (1001), the rotating shafts (1001) are respectively fixedly connected with the bottom ends of the element module box bodies (3), the bottom ends of the rotating shafts (1001) are rotatably fixed with sleeves (1002), the internal threads of the sleeves (1002) are connected with threaded rods (1003), a supporting plate (1004) is fixedly connected between the two threaded rods (1003), and the supporting plate (1004) is fixedly connected with the surface of the sampling tube (801) in an embedded manner.
6. The unmanned aerial vehicle type pollution source monitoring device based on satellite positioning as claimed in claim 5, wherein the supporting plate (1004) passes through a threaded rod (1003) to form a lifting structure with the sleeve (1002), and the sleeve (1002) passes through a rotating shaft (1001) to form a rotating structure with the element module box (3).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202020554467.1U CN212195900U (en) | 2020-04-15 | 2020-04-15 | Unmanned aerial vehicle formula pollution sources monitoring devices based on satellite positioning |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202020554467.1U CN212195900U (en) | 2020-04-15 | 2020-04-15 | Unmanned aerial vehicle formula pollution sources monitoring devices based on satellite positioning |
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| CN212195900U true CN212195900U (en) | 2020-12-22 |
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| CN202020554467.1U Active CN212195900U (en) | 2020-04-15 | 2020-04-15 | Unmanned aerial vehicle formula pollution sources monitoring devices based on satellite positioning |
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Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113465984A (en) * | 2021-07-29 | 2021-10-01 | 海南三友海洋科技有限公司 | Wetland ecological remediation monitoring devices |
| CN114114426A (en) * | 2021-10-28 | 2022-03-01 | 中国地质调查局烟台海岸带地质调查中心 | Coastal zone salt water invasion intelligent monitoring and identification method and system |
-
2020
- 2020-04-15 CN CN202020554467.1U patent/CN212195900U/en active Active
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113465984A (en) * | 2021-07-29 | 2021-10-01 | 海南三友海洋科技有限公司 | Wetland ecological remediation monitoring devices |
| CN113465984B (en) * | 2021-07-29 | 2023-03-10 | 海南三友海洋科技有限公司 | Wetland ecological remediation monitoring devices |
| CN114114426A (en) * | 2021-10-28 | 2022-03-01 | 中国地质调查局烟台海岸带地质调查中心 | Coastal zone salt water invasion intelligent monitoring and identification method and system |
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