CN212255281U - Water quality testing sampling equipment - Google Patents

Water quality testing sampling equipment Download PDF

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Publication number
CN212255281U
CN212255281U CN201922356363.XU CN201922356363U CN212255281U CN 212255281 U CN212255281 U CN 212255281U CN 201922356363 U CN201922356363 U CN 201922356363U CN 212255281 U CN212255281 U CN 212255281U
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CN
China
Prior art keywords
water
shell
aerial vehicle
unmanned aerial
fixedly arranged
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Expired - Fee Related
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CN201922356363.XU
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Chinese (zh)
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不公告发明人
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Cloud Smart Fujian Technology Co ltd
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Cloud Smart Fujian Technology Co ltd
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Priority to CN201922356363.XU priority Critical patent/CN212255281U/en
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Abstract

The utility model discloses a water quality testing sampling device, include: an unmanned aerial vehicle main body; the number of the support frames is two, and the two support frames are fixedly arranged on the front side and the rear side of the bottom end of the unmanned aerial vehicle main body; the shell is fixedly arranged at the bottom end of the unmanned aerial vehicle main body; the water taking mechanism is arranged on the front side of the inner cavity of the shell; the coiling mechanism is arranged on the rear side of the inner cavity of the shell; the camera is fixed to be set up bottom one side of casing, just the camera with the internal control system electric connection of unmanned aerial vehicle main part. This water quality testing sampling equipment when taking a sample to the water, can control the volume of getting water, and can make the water in the bottle of getting water not spill when the transportation to ensure to get the water yield sufficient, and can directly control unmanned aerial vehicle and take off the bottle of getting after falling again, easy operation has improved the device's practicality widely.

Description

Water quality testing sampling equipment
Technical Field
The utility model relates to a water treatment technical field specifically is a water quality testing sampling equipment.
Background
The water quality detection is part of environmental detection, and comprises the steps of detecting domestic wastewater, industrial wastewater, domestic drinking water, underground water, industrial cooling water, central air conditioning water and seawater to detect the chromaticity, turbidity, acidity, alkalinity, transparency, total residues, pH value and the like of effluent;
water quality testing need take a sample to water, the emerging development of unmanned aerial vehicle industry in recent years, people also begin to look at and adopt unmanned aerial vehicle water intaking, nevertheless utilize unmanned aerial vehicle water intaking to be perfect inadequately at present, can't control the water intaking volume, and can't protect the water after the sample when the transportation, the not enough condition of water intaking often can appear, need take off the sample bottle and just can descend unmanned aerial vehicle, troublesome poeration.
SUMMERY OF THE UTILITY MODEL
An object of the utility model is to provide a water quality testing sampling device to at least, solve among the prior art unable water intaking volume to control, and can't protect the water after the sample when the transportation, the condition that the water intaking is not enough often can appear, need take off the sample bottle after just can descend unmanned aerial vehicle, troublesome poeration's problem.
In order to achieve the above object, the utility model provides a following technical scheme: a water quality testing sampling device comprising:
an unmanned aerial vehicle main body;
the number of the support frames is two, and the two support frames are fixedly arranged on the front side and the rear side of the bottom end of the unmanned aerial vehicle main body;
the shell is fixedly arranged at the bottom end of the unmanned aerial vehicle main body;
the water taking mechanism is arranged on the front side of the inner cavity of the shell;
the coiling mechanism is arranged on the rear side of the inner cavity of the shell;
the camera is fixed to be set up bottom one side of casing, just the camera with the internal control system electric connection of unmanned aerial vehicle main part.
Preferably, the water intake mechanism includes: the water pump is fixedly arranged on the left side of the bottom end of the inner cavity of the shell and is electrically connected with an internal control system of the unmanned aerial vehicle main body; the water outlet of the water pump is connected with one end of the water outlet pipe in a threaded manner, and the other end of the water outlet pipe extends out of the bottom end of the shell; the circular frame is fixedly arranged at the bottom end of the shell, and the bottom end of the outer wall of the water outlet pipe is positioned in the circular frame; and the water taking bottle is in threaded connection with the inner wall of the circular frame.
Preferably, the water intake mechanism further includes: the supporting column is fixedly arranged on the left side of the bottom end of the inner cavity of the shell; the inlet tube, the one end of inlet tube and the water inlet spiro union of water pump, and the other end of inlet tube extends the right side surface of support column and with support column fixed connection.
Preferably, the outer wall of the water taking bottle is provided with size scales.
Preferably, the winding mechanism includes: the speed reducing motor is fixedly arranged on the right side of the top end of the shell and is electrically connected with an internal control system of the unmanned aerial vehicle main body; the output end of the speed reducing motor is locked with one end of the cylindrical rod arranged along the left-right direction through a coupler, the other end of the cylindrical rod is rotatably connected with the inner wall of the water inlet pipe through a sealing bearing, an inner ring of the sealing bearing is in interference fit with the outer wall of the cylindrical rod, and an outer ring of the sealing bearing is fixedly arranged on the inner wall of the water inlet pipe; the water taking pipe is wound on the outer wall of the cylindrical rod, a groove communicated with the inner cavity of the water inlet pipe is formed in the left side of the cylindrical rod, and one end of the water taking pipe is fixedly arranged on the outer wall of the cylindrical rod and communicated with the inner cavity of the groove.
Preferably, the rear side of the bottom end of the shell starts to be provided with a limiting hole along the left and right directions, and the other end of the water taking pipe extends out of the bottom end of the inner cavity of the limiting hole; the take-up mechanism includes: the balancing weight is fixedly arranged at the bottom end of the outer wall of the water taking pipe; the number of the baffle plates is two, and the two baffle plates are fixedly arranged on the left side and the right side of the outer wall of the cylindrical rod.
Compared with the prior art, the beneficial effects of the utility model are that: this water quality testing sampling device, through the winding mechanism, the cooperation of support column and inlet tube can make the intake pipe when receiving and releasing, the inner chamber of intake pipe communicates with each other all the time with the inner chamber of recess and inlet tube, and loop through the intake pipe with water under the suction effect of water pump, recess and inlet tube inhale the intake pump in, and collect in the intake bottle through the outlet pipe, and can ensure to carry out steady transportation to the water after the sample through the intake bottle with circular frame inner wall spiro union, can carry out accurate observation to the intake volume through camera and the size scale that sets up on the intake bottle outer wall, the device is when taking a sample to water, can control the intake volume, and can make the water in the intake bottle not spill when the transportation, in order to ensure the intake volume sufficient, and can directly control unmanned aerial vehicle and take off the intake bottle after falling, and easy operation, the practicality of the device is greatly improved.
Drawings
Fig. 1 is a schematic structural view of the present invention;
FIG. 2 is a right side cross-sectional view of the housing of FIG. 1 in accordance with the present invention;
figure 3 is a front cross-sectional view of the housing of figure 1 in accordance with the present invention;
fig. 4 is the structural schematic diagram of the cylinder rod of the present invention.
In the figure: 1. unmanned aerial vehicle main part, 2, support frame, 3, casing, 4, water intaking mechanism, 41, water pump, 42, outlet pipe, 43, circular frame, 44, water intaking bottle, 45, support column, 46, inlet tube, 5, winding mechanism, 51, gear motor, 52, cylinder pole, 53, water intaking pipe, 54, recess, 55, balancing weight, 56, baffle, 6, camera, 7, spacing hole.
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: the method comprises the following steps: the unmanned aerial vehicle comprises an unmanned aerial vehicle main body 1, two support frames 2, a shell 3, a water taking mechanism 4, a coiling mechanism 5 and a camera 6, the two support frames 2 are fixedly arranged at the front side and the rear side of the bottom end of the unmanned aerial vehicle main body 1, the shell 3 is fixedly arranged at the bottom end of the unmanned aerial vehicle main body 1, the unmanned aerial vehicle main body 1 is in the prior art, a power supply device and a control system are arranged in the unmanned aerial vehicle main body 1, the unmanned aerial vehicle model according with the scheme can be used, the water taking mechanism 4 is arranged at the front side of the inner cavity of the shell 3, the coiling mechanism 5 is arranged at the rear side of the inner cavity of the shell 3, the camera 6 is fixedly, and camera 6 and unmanned aerial vehicle main part 1's internal control system electric connection, camera 6 are prior art, not only can observe the removal of unmanned aerial vehicle main part 1, still can observe water intaking bottle 44 and water intaking pipe 46, and the camera model number that accords with the present case all can use.
Preferably, the water intake mechanism 4 further includes: the water pump 41 is fixedly arranged on the left side of the bottom end of the inner cavity of the shell 3, the water pump 41 is electrically connected with an internal control system of the unmanned aerial vehicle main body 1, the water pump 41 is in the prior art and can generate suction force to the water inlet pipe 46, the water pump can be used according with the model of the water pump in the scheme, water in a detection place can be sucked into the groove 54 through the water inlet pipe 53 under the suction force of the water pump 41 and sucked into the water inlet pump 41 through the water inlet pipe 46, the water outlet of the water pump 41 is screwed with one end of the water outlet pipe 42, the other end of the water outlet pipe 42 extends out of the bottom end of the shell 3, the circular frame 43 is fixedly arranged at the bottom end of the shell 3, the bottom end of the outer wall of the water outlet pipe 42 is positioned in the circular frame 43, the outer wall of the water outlet pipe 43 and the bottom end of the shell 3 are in a movable state so as to, get water bottle 44 and the inner wall looks spiro union of circular frame 43, get water bottle 44 through rotating and can be convenient for take off and install getting water bottle 44, and can not cause the water in getting water bottle 44 to spill when unmanned aerial vehicle main part 1 is flying.
Preferably, the water intake mechanism 4 further includes: support column 45 and inlet tube 46, support column 45 is fixed to be set up on the left side of the inner chamber bottom of casing 3, the one end of inlet tube 46 and the water inlet spiro union of water pump 41, and the other end of inlet tube 46 extend the right flank surface of support column 45 and with support column 45 fixed connection, support column 45 can play the supporting role to inlet tube 46 to can make circular pole 52 rotate around self axis under the cooperation of inlet tube 46 and support column 45.
Preferably, the outer wall of the water bottle 44 is provided with a dimension scale, so that the amount of water taken in the water bottle 44 can be observed conveniently.
Preferably, the winding mechanism 5 further includes: the speed reducing motor 5, the cylindrical rod 52, the water taking pipe 53 and the groove 54, the speed reducing motor 51 is fixedly arranged on the right side of the top end of the shell 3, the speed reducing motor 51 is electrically connected with an internal control system of the unmanned aerial vehicle main body 1, the speed reducing motor 51 is in the prior art, the speed reducing motor 51 can control the rotating rod 52 to rotate clockwise or anticlockwise around the axis of the speed reducing motor 51, the speed reducing motor model conforming to the scheme can be used, the output end of the speed reducing motor 51 is locked with one end of the cylindrical rod 52 arranged along the left and right directions through a coupler, the other end of the cylindrical rod 52 is rotatably connected with the inner wall of the water inlet pipe 46 through a sealing bearing, the inner ring of the sealing bearing is in interference fit with the outer wall of the cylindrical rod 52, the outer ring of the sealing bearing is fixedly arranged on the inner wall of the water inlet pipe 46, the cylindrical rod 52 can rotate in the inner cavity of the water inlet pipe 46, a groove 54 communicated with the inner cavity of the water inlet pipe 46 is formed at the left side of the cylindrical rod 52, and one end of the water taking pipe 53 is fixedly arranged on the outer wall of the cylindrical rod 52 and communicated with the inner cavity of the groove 54, so that the water taking pipe 53 is communicated with the inner cavity of the water inlet pipe 46.
As a preferable scheme, furthermore, the rear side of the bottom end of the shell 3 starts to be provided with a limiting hole 7 along the left and right directions, and the other end of the water taking pipe 53 extends out of the bottom end of the inner cavity of the limiting hole 7; the winding mechanism 5 includes: balancing weight 55 and baffle 56, balancing weight 55 are fixed to be set up in the outer wall bottom of intake pipe 53, and the quantity of baffle 56 is two, and two baffles 56 are fixed to be set up in the outer wall left and right sides of cylinder pole 52.
All the electrical components in the present application are connected with the power supply adapted to the electrical components through the wires, and an appropriate controller should be selected according to actual conditions to meet the control requirements, specific connection and control sequence.
When the unmanned aerial vehicle is used, the unmanned aerial vehicle main body 1 is controlled to be started through an external control system, the unmanned aerial vehicle main body can be controlled to fly above a detection place through the camera 6, the speed reducing motor 51 is controlled to be started, the cylindrical rod 52 can be driven to rotate anticlockwise around the axis of the cylindrical rod under the matching of the water inlet pipe 46 and the supporting column 45 after the speed reducing motor 51 is started, one end of the water taking pipe 53 is extended downwards under the action of the gravity of the balancing weight 55 until the water enters the water, the water pump 41 is controlled to be started, water in the detection place can be sucked into the groove 54 through the water taking pipe 53 under the suction action of the water pump 41 and is sucked into the water inlet pump 41 through the water inlet pipe 46, the water in the water pump 41 can be discharged into the water taking bottle 44 under the conveying of the water outlet pipe 42, the size scales of the water level in the water taking bottle 44 and, and get water bottle 44 spiro union on the inner wall of circular frame 43, when unmanned aerial vehicle main part 1 rocks in flight production, can not cause the water in getting water bottle 44 to spill, after getting water, accessible gear motor 51 control cylinder pole 52 clockwise rotates, thereby can twine water pipe 53 on cylinder pole 52 again, in taking water pipe 53 into casing 3, can ensure that unmanned aerial vehicle main part 1 normally flies and descends, get water bottle 44 through rotating and can take off the inner wall of getting water bottle from circular frame 43, thereby can accomplish the sample to water, therefore, the operation is simple, and the wide popularization is facilitated.
In the description of the present invention, it is to be understood that the terms "top end", "bottom end", "front side", "rear side", "outer wall", "inner cavity", 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 simplicity of description, and do not indicate or imply that the device or element being referred to must have a particular orientation, be constructed and operated in a particular orientation; also, unless expressly stated or limited otherwise, the terms "telescoped," "plugged," "threaded," "fixedly mounted," "interference fit," "disposed," and the like are to be construed broadly, e.g., as a fixed connection, a removable connection, or an integral part; can be mechanically or electrically connected; they may be directly connected or indirectly connected through an intermediate medium, and may be connected through the inside of two elements or in an interaction relationship between two elements, unless otherwise specifically defined, and the specific meaning of the above terms in the present invention will be understood by those skilled in the art according to specific situations.
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 (6)

1. A water quality testing sampling device, characterized by, includes:
an unmanned aerial vehicle main body (1);
the number of the support frames (2) is two, and the two support frames (2) are fixedly arranged on the front side and the rear side of the bottom end of the unmanned aerial vehicle main body (1);
the shell (3) is fixedly arranged at the bottom end of the unmanned aerial vehicle main body (1);
the water taking mechanism (4) is arranged on the front side of the inner cavity of the shell (3);
the coiling mechanism (5) is arranged on the rear side of the inner cavity of the shell (3);
camera (6), fixed the setting is in bottom one side of casing (3), just camera (6) with the internal control system electric connection of unmanned aerial vehicle main part (1).
2. The water quality detection sampling device of claim 1, wherein: the water intake mechanism (4) includes:
the water pump (41) is fixedly arranged on the left side of the bottom end of the inner cavity of the shell (3), and the water pump (41) is electrically connected with an internal control system of the unmanned aerial vehicle main body (1);
the water outlet of the water pump (41) is connected with one end of the water outlet pipe (42) in a threaded manner, and the other end of the water outlet pipe (42) extends out of the bottom end of the shell (3);
the round frame (43) is fixedly arranged at the bottom end of the shell (3), and the bottom end of the outer wall of the water outlet pipe (42) is positioned in the round frame (43);
and the water taking bottle (44) is in threaded connection with the inner wall of the circular frame (43).
3. A water quality testing and sampling device according to claim 2, characterized in that: the water intake mechanism (4) further comprises:
the supporting column (45) is fixedly arranged on the left side of the bottom end of the inner cavity of the shell (3);
the water inlet pipe (46), the water inlet spiro union of one end and water pump (41) of inlet tube (46), and the other end of inlet tube (46) extends the right side surface of support column (45) and with support column (45) fixed connection.
4. A water quality testing and sampling device according to claim 2, characterized in that: the outer wall of the water taking bottle (44) is provided with size scales.
5. The water quality detection sampling device of claim 1, wherein: the winding mechanism (5) includes:
the speed reducing motor (51) is fixedly arranged on the right side of the top end of the shell (3), and the speed reducing motor (51) is electrically connected with an internal control system of the unmanned aerial vehicle main body (1);
the output end of the speed reducing motor (51) is locked with one end of the cylindrical rod (52) arranged along the left-right direction through a coupler, the other end of the cylindrical rod (52) is rotatably connected with the inner wall of the water inlet pipe (46) through a sealing bearing, an inner ring of the sealing bearing is in interference fit with the outer wall of the cylindrical rod (52), and an outer ring of the sealing bearing is fixedly arranged on the inner wall of the water inlet pipe (46);
the water taking pipe (53) is wound on the outer wall of the cylindrical rod (52), a groove (54) communicated with the inner cavity of the water inlet pipe (46) is formed in the left side of the cylindrical rod (52), and one end of the water taking pipe (53) is fixedly arranged on the outer wall of the cylindrical rod (52) and communicated with the inner cavity of the groove (54).
6. The water quality detection sampling device of claim 5, wherein: a limiting hole (7) is formed in the rear side of the bottom end of the shell (3) along the left and right directions, and the other end of the water taking pipe (53) extends out of the bottom end of an inner cavity of the limiting hole (7); the winding mechanism (5) includes:
the balancing weight (55) is fixedly arranged at the bottom end of the outer wall of the water intake pipe (53);
the number of the baffle plates (56) is two, and the two baffle plates (56) are fixedly arranged on the left side and the right side of the outer wall of the cylindrical rod (52).
CN201922356363.XU 2019-12-25 2019-12-25 Water quality testing sampling equipment Expired - Fee Related CN212255281U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201922356363.XU CN212255281U (en) 2019-12-25 2019-12-25 Water quality testing sampling equipment

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201922356363.XU CN212255281U (en) 2019-12-25 2019-12-25 Water quality testing sampling equipment

Publications (1)

Publication Number Publication Date
CN212255281U true CN212255281U (en) 2020-12-29

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Family Applications (1)

Application Number Title Priority Date Filing Date
CN201922356363.XU Expired - Fee Related CN212255281U (en) 2019-12-25 2019-12-25 Water quality testing sampling equipment

Country Status (1)

Country Link
CN (1) CN212255281U (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN113607494A (en) * 2021-07-30 2021-11-05 华东理工大学 Automatic water taking device and method for unmanned aerial vehicle

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN113607494A (en) * 2021-07-30 2021-11-05 华东理工大学 Automatic water taking device and method for unmanned aerial vehicle

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Granted publication date: 20201229

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