CN212530070U - Unmanned aerial vehicle water intaking device - Google Patents
Unmanned aerial vehicle water intaking device Download PDFInfo
- Publication number
- CN212530070U CN212530070U CN202020884086.XU CN202020884086U CN212530070U CN 212530070 U CN212530070 U CN 212530070U CN 202020884086 U CN202020884086 U CN 202020884086U CN 212530070 U CN212530070 U CN 212530070U
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- bin
- water taking
- water
- wall
- taking bin
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Abstract
The utility model provides an unmanned aerial vehicle water intaking device which characterized in that: including connecting plate (1), fixed storehouse (2), layering water intaking device (3) and landing gear (4), fixed storehouse (2) connect in connecting plate (1) lower part, fixed storehouse (2) lower part is equipped with joint mouth (5), the utility model provides an unmanned aerial vehicle water intaking device can use unmanned aerial vehicle to treat the water sample of each level in detection waters and take a sample, and unmanned aerial vehicle floats on the surface of water in the sampling process, reduces unmanned aerial vehicle's energy resource consumption.
Description
Technical Field
The utility model relates to a water intaking device, in particular to unmanned aerial vehicle water intaking device.
Background
Water quality testing is the comparatively commonly used data collection means in aquatic products farming and environmental monitoring, and at present mostly through waiting to detect the waters and go to different positions through driving the ship, use the water sampler to carry out water sample collection, this method often needs to consume more manpower and materials, is not convenient for people's use, and current unmanned aerial vehicle sampling method, most can only gather surface water, therefore, application scope is less.
SUMMERY OF THE UTILITY MODEL
In order to solve the technical scheme, the utility model provides an unmanned aerial vehicle water intaking device can use unmanned aerial vehicle to treat the water sample of each level in detection waters and take a sample, and unmanned aerial vehicle floats on the surface of water in the sampling process, reduces unmanned aerial vehicle's energy resource consumption.
In order to realize the above functions, the utility model discloses the technical scheme who takes as follows: an unmanned aerial vehicle water intaking device comprises a connecting plate (1), a fixed bin (2), a layered water intaking device (3) and a lifting device (4), wherein the connecting plate (1) is connected with the lower part of an unmanned aerial vehicle main body, the fixed bin (2) is connected with the lower part of the connecting plate (1), a clamping opening (5) is arranged at the lower part of the fixed bin (2), the layered water intaking device (3) comprises a driving motor (6), a rotating shaft (7), a wire barrel (8), a bearing seat (9), a first check valve (10), a second check valve (11), a third check valve (12), a water outlet (13), a fixed block (14), a connecting wire (15), a floating ball (16), an inductor (17), a deep water intaking bin (18), a middle water intaking bin (19) and a shallow water intaking bin (20), the driving motor (6) is connected with the inner wall of one side of the fixed bin (2), and the bearing seat (9) is connected with the inner wall, the utility model discloses a water taking device, including bearing frame (9), pivot (7), line bucket (8), rope (21), shallow water taking bin (20), superficial water taking bin (19), deep water taking bin (18), middle layer water taking bin (19), check valve II (11), middle layer water taking bin (19), bearing frame (9), pivot (6) output, the other end of pivot (7) connect in bearing frame (9), line bucket (8) are located pivot (7) lateral wall, line bucket (8) winding has rope (21), shallow water taking bin (20) connect in rope (21), middle layer water taking bin (19) connect in shallow water taking bin (20) lower wall, deep water taking bin (18) connect in deep water taking bin (18) lower wall, deep water taking bin (18) is linked together through check valve II (10), check valve II (11) connect in middle layer water taking bin (19) lower wall, middle layer water taking bin (19) pass through check valve II (11) are linked together with, the three check valves (12) are connected to the lower wall of the shallow water taking bin (20), the shallow water taking bin (20) is communicated with the outside through the three check valves (12), the fixed block (14) is connected to the inner wall of the lower part of the deep water taking bin (18), the floating ball (16) is connected with the fixed block (14) through the connecting line (15), the water outlet (13) is connected to the side wall of the deep water taking bin (18), the sensor (17) is connected to the side wall of the shallow water taking bin (20), the water taking bin is sunk into the deep water area through a rope, the first check valve is opened, water enters the deep water taking bin through the first check valve, the floating ball floats up, when the sensor senses that the first check valve is closed, the floating ball is driven by the reverse rotation of the driving motor to bring the water taking bin to the middle water area, the second check valve is opened, and the operations are repeated until the sensor in the shallow water taking bin senses the floating ball, the driving motor lifts the water taking bin out of the water surface through a rope and is clamped on the clamping opening.
Optionally, landing gear (4) includes spliced pole (22), spring storehouse (23), spring (24), pillar (25), bottom plate (26), gas generator (27), solid fuel (28), gasbag storehouse (29) and gasbag (30), spliced pole (22) one end connect in connecting plate (1), spring storehouse (23) connect in the spliced pole (22) other end, spring (24) one end connect in spring storehouse (23) upper portion inner wall, pillar (25) pass spring storehouse (23) sub-unit connect in spring (24) the other end, bottom plate (26) are located pillar (25) lower part, gasbag storehouse (29) connect in bottom plate (26) upper wall, bottom plate (26) lateral wall is equipped with water and invades inductor (31), gasbag (30) connect in gasbag storehouse (29) lateral wall just gasbag (30) with gasbag storehouse (29) are linked together, the gas generator (27) is connected to the inner wall of the lower portion of the air bag bin (29), the solid fuel (28) is connected to the side wall of the gas generator (27), impact force of the unmanned aerial vehicle during landing can be relieved through elastic deformation of the spring, when the water invasion sensor senses that water enters, the gas generator is started, the gas generator generates ignition action, the fixed fuel is ignited, generated gas enters the air bag through the air bag bin, the air bag is filled instantly, and the air bag is ejected;
optionally, the water outlet (13), the fixing block (14), the connecting line (15), the floating ball (16) and the inductor (17) are respectively provided with one group in the deep water taking bin (18), the middle water taking bin (19) and the shallow water taking bin (20);
optionally, the landing gear (4) is provided with two sets of gears by taking the central axis of the connecting plate (1) as a symmetry axis.
The utility model adopts the above structure to gain beneficial effect as follows: the utility model provides an unmanned aerial vehicle water intaking device, the water sample that can use unmanned aerial vehicle's water intaking device to treat each level in detection waters takes a sample, once can extract multiple level water sample, improves work efficiency, and unmanned aerial vehicle floats on the surface of water through the gasbag in the sample process, lowers unmanned aerial vehicle's energy resource consumption, when subaerial descending, the impact that receives when the elastic deformation of the spring through landing gear alleviateed unmanned aerial vehicle descending.
Drawings
Fig. 1 is an overall structure diagram of a water intake device of an unmanned aerial vehicle according to the present invention;
fig. 2 is a structural diagram of a water intake bin of the unmanned aerial vehicle water intake device of the present invention;
fig. 3 is the utility model relates to a local enlarger that unmanned aerial vehicle water intaking device's pillar and bottom plate are connected.
The water intake device comprises a connecting plate 1, a connecting plate 2, a fixed bin 3, a layered water intake device 4, a lifting device 5, a clamping opening 6, a driving motor 7, a rotating shaft 8, a thread barrel 9, a bearing seat 10, a one-way valve I, a one-way valve II, a one-way valve III, a one-way valve 13, a water outlet 14, a fixed block 15, a connecting wire 16, a floating ball 17, a sensor 18, a deep water intake bin 19, a middle water intake bin 20, a shallow water intake bin 21, a rope 22, a connecting column 23, a spring bin 24, a spring 25, a support column 26, a bottom plate 27, a gas generator 28, solid fuel 29, an air bag bin 30, an air bag 31 and a water invasion sensor.
Detailed Description
The technical solution of the present invention will be described in further detail with reference to the following embodiments, and the technical features or the connection relations of the present invention, which are not described in detail, are the prior art adopted.
In the description of the present invention, it should be noted that the terms "center", "upper", "lower", "left", "right", "vertical", "horizontal", "inner", "outer", and the like indicate orientations or positional relationships based on the orientations or positional relationships shown in the drawings, and are only for convenience of description and simplification of description, but do not indicate or imply that the device or element referred to must have a specific orientation, be constructed and operated in a specific orientation, and thus, should not be construed as limiting the present invention. Furthermore, the terms "first," "second," and "third" are used for descriptive purposes only and are not to be construed as indicating or implying relative importance.
In the description of the present invention, it is to be noted that, unless otherwise explicitly specified or limited, the terms "disposed," "connected" and "connected" are to be construed broadly, and may be, for example, fixedly connected, detachably connected, or integrally connected; can be mechanically or electrically connected; they may be connected directly or indirectly through intervening media, or they may be interconnected between two elements. The specific meaning of the above terms in the present invention can be understood in specific cases by those skilled in the art.
The present invention will be described in further detail with reference to the accompanying drawings.
As shown in fig. 1-2, an unmanned aerial vehicle water intake device comprises a connecting plate (1), a fixed bin (2), a layered water intake device (3) and a landing gear (4), wherein the fixed bin (2) is connected to the lower part of the connecting plate (1), a clamping opening (5) is arranged at the lower part of the fixed bin (2), the layered water intake device (3) comprises a driving motor (6), a rotating shaft (7), a line barrel (8), a bearing seat (9), a one-way valve I (10), a one-way valve II (11), a one-way valve III (12), a water outlet (13), a fixed block (14), a connecting wire (15), a floating ball (16), an inductor (17), a deep water intake bin (18), a middle water intake bin (19) and a shallow water intake bin (20), the driving motor (6) is connected to the inner wall at one side of the fixed bin (2), and the bearing seat (9) is connected to the inner wall at, the utility model discloses a water taking device, including bearing frame (9), pivot (7), line bucket (8), rope (21), shallow water taking bin (20), superficial water taking bin (19), deep water taking bin (18), middle layer water taking bin (19), check valve II (11), middle layer water taking bin (19), bearing frame (9), pivot (6) output, the other end of pivot (7) connect in bearing frame (9), line bucket (8) are located pivot (7) lateral wall, line bucket (8) winding has rope (21), shallow water taking bin (20) connect in rope (21), middle layer water taking bin (19) connect in shallow water taking bin (20) lower wall, deep water taking bin (18) connect in deep water taking bin (18) lower wall, deep water taking bin (18) is linked together through check valve II (10), check valve II (11) connect in middle layer water taking bin (19) lower wall, middle layer water taking bin (19) pass through check valve II (11) are linked together with, the three check valves (12) are connected to the lower wall of the shallow water taking bin (20), the shallow water taking bin (20) is communicated with the outside through the three check valves (12), the fixed block (14) is connected to the inner wall of the lower part of the deep water taking bin (18), the floating ball (16) is connected with the fixed block (14) through the connecting line (15), the water outlet (13) is connected to the side wall of the deep water taking bin (18), and the sensor (17) is connected to the side wall of the shallow water taking bin (20); landing gear (4) includes spliced pole (22), spring storehouse (23), spring (24), pillar (25), bottom plate (26), gas generator (27), solid fuel (28), gasbag storehouse (29) and gasbag (30), spliced pole (22) one end connect in connecting plate (1), spring storehouse (23) connect in the spliced pole (22) other end, spring (24) one end connect in spring storehouse (23) upper portion inner wall, pillar (25) pass spring storehouse (23) sub-unit connect in spring (24) other end, bottom plate (26) are located pillar (25) lower part, gasbag storehouse (29) connect in bottom plate (26) upper wall, bottom plate (26) lateral wall is equipped with water and invades inductor (31), gasbag (30) connect in gasbag storehouse (29) lateral wall just gasbag (30) with gasbag storehouse (29) are linked together, the gas generator (27) is connected to the lower inner wall of the airbag bin (29), and the solid fuel (28) is connected to the side wall of the gas generator (27); the water outlet (13), the fixing block (14), the connecting line (15), the floating ball (16) and the inductor (17) are respectively provided with one group in the deep water taking bin (18), the middle water taking bin (19) and the shallow water taking bin (20); the landing gear (4) is provided with two groups by taking the central axis of the connecting plate (1) as a symmetry axis.
When the unmanned aerial vehicle flies to a specified water area, the engine of the unmanned aerial vehicle is turned off, the unmanned aerial vehicle lands on the water surface, when the water intrusion sensor 31 senses that water enters, the gas generator 27 is started, the gas generator 27 generates an ignition action to ignite the fixed fuel 28, the generated gas enters the air bag 30 through the air bag bin 29 to be instantly filled with the air bag 30, the air bag 30 is popped up, the unmanned aerial vehicle floats on the water surface, then the driving motor 6 is started, the driving motor 6 drives the rotating shaft 7 to rotate, the rotating shaft 7 drives the wire barrel 8 to rotate, the water taking bin is sunk into the deep water area through the rope 21, the one-way valve I10 is opened, water enters the deep water taking bin 18 through the one-way valve I10, the floating ball 16 floats up, when the water taking floating ball 16 is sensed by the sensor 17, the one-way valve I10 is turned off, the driving motor 6 is turned over to bring the bin to the middle-layer water area, the floater 16 in the middle level sump 19 of fetching water floats, when the inductor 17 in the middle level sump 19 of fetching water senses the floater 16, check valve two 11 is closed, driving motor 6 reverses and takes the sump to the shallow waters, check valve three 12 is opened, water gets into shallow sump 20 through check valve three 12, the floater 16 in the shallow sump 20 of fetching water floats, when the inductor 17 in the shallow sump 20 of fetching water senses the floater 16, driving motor 6 offers the sump of fetching water through rope 21, the block is on block mouth 5, when unmanned aerial vehicle descends on ground, bottom plate 26 can give pillar 25 one to the thrust of connecting plate 1 direction, pillar 26 promotes spring 24, make spring 24 reduce the partial impact force of buffering, the impact force that receives when reducing unmanned aerial vehicle, increase unmanned aerial vehicle's life.
Claims (4)
1. The utility model provides an unmanned aerial vehicle water intaking device which characterized in that: the water taking device comprises a connecting plate (1), a fixed bin (2), a layered water taking device (3) and a lifting device (4), wherein the fixed bin (2) is connected to the lower part of the connecting plate (1), a clamping opening (5) is formed in the lower part of the fixed bin (2), the layered water taking device (3) comprises a driving motor (6), a rotating shaft (7), a line barrel (8), a bearing seat (9), a one-way valve I (10), a one-way valve II (11), a one-way valve III (12), a water outlet (13), a fixed block (14), a connecting line (15), a floating ball (16), an inductor (17), a deep water taking bin (18), a middle water taking bin (19) and a shallow water taking bin (20), the driving motor (6) is connected to the inner wall on one side of the fixed bin (2), the bearing seat (9) is connected to the inner wall on the other side of the fixed bin (2), one end of the rotating, the other end of the rotating shaft (7) is connected with the bearing seat (9), the line barrel (8) is arranged on the side wall of the rotating shaft (7), a rope (21) is wound on the line barrel (8), the superficial layer water taking bin (20) is connected with the rope (21), the middle layer water taking bin (19) is connected with the lower wall of the superficial layer water taking bin (20), the deep layer water taking bin (18) is connected with the lower wall of the middle layer water taking bin (19), the first check valve (10) is connected with the lower wall of the deep layer water taking bin (18), the deep layer water taking bin (18) is communicated with the outside through the first check valve (10), the second check valve (11) is connected with the lower wall of the middle layer water taking bin (19), the middle layer water taking bin (19) is communicated with the outside through the second check valve (11), and the third check valve (12) is connected with the lower wall of the superficial layer water taking bin (20), the shallow water taking bin (20) is communicated with the outside through the three check valves (12), the fixed block (14) is connected to the inner wall of the lower portion of the deep water taking bin (18), the floating ball (16) is connected with the fixed block (14) through the connecting line (15), the water outlet (13) is connected to the side wall of the deep water taking bin (18), and the inductor (17) is connected to the side wall of the shallow water taking bin (20).
2. The unmanned aerial vehicle water intaking device of claim 1, characterized in that: landing gear (4) includes spliced pole (22), spring storehouse (23), spring (24), pillar (25), bottom plate (26), gas generator (27), solid fuel (28), gasbag storehouse (29) and gasbag (30), spliced pole (22) one end connect in connecting plate (1), spring storehouse (23) connect in the spliced pole (22) other end, spring (24) one end connect in spring storehouse (23) upper portion inner wall, pillar (25) pass spring storehouse (23) sub-unit connect in spring (24) other end, bottom plate (26) are located pillar (25) lower part, gasbag storehouse (29) connect in bottom plate (26) upper wall, bottom plate (26) lateral wall is equipped with water and invades inductor (31), gasbag (30) connect in gasbag storehouse (29) lateral wall just gasbag (30) with gasbag storehouse (29) are linked together, the gas generator (27) is connected to the lower inner wall of the air bag bin (29), and the solid fuel (28) is connected to the side wall of the gas generator (27).
3. The unmanned aerial vehicle water intaking device of claim 1, characterized in that: the water outlet (13), the fixing block (14), the connecting line (15), the floating ball (16) and the inductor (17) are respectively provided with a group in the deep water taking bin (18), the middle water taking bin (19) and the shallow water taking bin (20).
4. The unmanned aerial vehicle water intaking device of claim 1, characterized in that: the landing gear (4) is provided with two groups by taking the central axis of the connecting plate (1) as a symmetry axis.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202020884086.XU CN212530070U (en) | 2020-05-25 | 2020-05-25 | Unmanned aerial vehicle water intaking device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202020884086.XU CN212530070U (en) | 2020-05-25 | 2020-05-25 | Unmanned aerial vehicle water intaking device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN212530070U true CN212530070U (en) | 2021-02-12 |
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ID=74542172
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202020884086.XU Expired - Fee Related CN212530070U (en) | 2020-05-25 | 2020-05-25 | Unmanned aerial vehicle water intaking device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN212530070U (en) |
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2020
- 2020-05-25 CN CN202020884086.XU patent/CN212530070U/en not_active Expired - Fee Related
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20210212 |