CN113619799A - High-altitude water taking device - Google Patents
High-altitude water taking device Download PDFInfo
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- CN113619799A CN113619799A CN202110989544.5A CN202110989544A CN113619799A CN 113619799 A CN113619799 A CN 113619799A CN 202110989544 A CN202110989544 A CN 202110989544A CN 113619799 A CN113619799 A CN 113619799A
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D47/00—Equipment not otherwise provided for
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/04—Helicopters
- B64C27/08—Helicopters with two or more rotors
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C39/00—Aircraft not otherwise provided for
- B64C39/02—Aircraft not otherwise provided for characterised by special use
- B64C39/024—Aircraft not otherwise provided for characterised by special use of the remote controlled vehicle type, i.e. RPV
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
- B64U10/10—Rotorcrafts
-
- E—FIXED CONSTRUCTIONS
- E03—WATER SUPPLY; SEWERAGE
- E03B—INSTALLATIONS OR METHODS FOR OBTAINING, COLLECTING, OR DISTRIBUTING WATER
- E03B3/00—Methods or installations for obtaining or collecting drinking water or tap water
- E03B3/28—Methods or installations for obtaining or collecting drinking water or tap water from humid air
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U2101/00—UAVs specially adapted for particular uses or applications
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- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
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- Environmental & Geological Engineering (AREA)
- Health & Medical Sciences (AREA)
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- Air-Conditioning For Vehicles (AREA)
Abstract
The invention provides a high-altitude water taking device which comprises an unmanned aerial vehicle, a storage bin, an induced air unit, a water absorbing unit, a heating unit, a refrigerating unit and a condensation bin, wherein the unmanned aerial vehicle is provided with an accommodating cavity, and the accommodating cavity is provided with a ventilation opening and a water passing opening; the storage bin is arranged in the accommodating cavity and is provided with an air inlet, an air outlet and a water vapor outlet, and the air inlet and the air outlet are respectively communicated with the ventilation opening; the air inducing unit is communicated with the air inlet and/or the air outlet; the water absorption unit is arranged in the storage bin; the heating unit is used for heating the water absorption unit; the condensation bin is arranged in the accommodating cavity and is provided with a water vapor inlet communicated with the water vapor outlet and a water outlet, the water outlet is communicated with the water passing opening, and the condensation bin is used for receiving liquid water formed by condensation of the refrigeration unit. The invention provides a high-altitude water taking device, which aims to convert high-altitude water vapor in a desert area into liquid water and convey the liquid water to the ground, so that the problem of water resource shortage in the desert area is solved.
Description
Technical Field
The invention belongs to the technical field of high-altitude water taking, and particularly relates to a high-altitude water taking device.
Background
The land surface and the underground water resources in the desert and other regions are deficient, so that the development of the desert region is limited. The research shows that the water vapor content in the high altitude of the desert area is rich, for example, in the Ili valley area, the water vapor content in the area from the ground to the atmospheric pressure of 850hPa is 3.5mm, and accounts for about 29.5 percent of the whole layer; the water vapor content in the area with the atmospheric pressure of 850hPa to 700hPa reaches 4.8mm, which accounts for 40 percent of the whole layer, and the area corresponds to the altitude of about 2000 m. If the high-altitude water vapor in the desert area can be fully utilized to act as a water source, the development of the desert area can be greatly promoted.
Disclosure of Invention
The invention aims to provide a high-altitude water taking device, which aims to convert high-altitude water vapor in a desert area into liquid water and convey the liquid water to the ground, so that the problem of water resource shortage in the desert area is solved.
In order to achieve the purpose, the invention adopts the technical scheme that: provided is a high altitude water taking device, comprising:
the unmanned aerial vehicle is provided with an accommodating cavity, the accommodating cavity is provided with a ventilation opening and a water passing opening, and the unmanned aerial vehicle can fly at high altitude and stays at a high altitude designated position;
the storage bin is arranged in the accommodating cavity and is provided with an air inlet, an air outlet and a water vapor outlet, and the air inlet and the air outlet are respectively communicated with the ventilation opening;
the air inducing unit is communicated with the air inlet and/or the air outlet so as to provide ventilation power;
the water absorption unit is arranged in the storage bin and is used for absorbing water vapor in the air;
a heating unit for heating the water absorbing unit;
a refrigeration unit; and
the condensation bin is arranged in the accommodating cavity and is provided with a water vapor inlet communicated with the water vapor outlet and a water outlet, the water outlet is communicated with the water passing opening, and the condensation bin is used for receiving liquid water formed by condensation of the refrigeration unit.
In a possible implementation manner, the water absorbing unit is a spiral member and is formed with a spiral water absorbing surface, and the outer edge of the water absorbing unit is connected with the inner wall of the storage bin.
In a possible implementation manner, the storage bin is arranged outside the condensation bin, the water vapor outlet is communicated with the water vapor inlet through a connecting pipe, and a third valve is arranged on the connecting pipe.
In one possible implementation, an airbag is provided on the unmanned aerial vehicle.
In a possible implementation manner, the high-altitude water taking device further comprises a solar panel and a battery, the solar panel is arranged outside the unmanned aerial vehicle, the solar panel is connected with the battery, and the battery is further respectively connected with the induced air unit, the heating unit and the refrigerating unit.
In a possible implementation manner, the high-altitude water taking device further comprises a controller, a first valve arranged on the air inlet, a second valve arranged on the air outlet, and a humidity detector arranged in the storage bin, wherein the first valve, the second valve, the humidity detector and the heating unit are respectively in communication connection with the controller.
In a possible implementation manner, a liquid level detector is further arranged in the condensation bin, the water outlet is provided with a switch piece which can be opened and closed, and the liquid level detector and the switch piece are respectively in communication connection with the controller.
In one possible implementation, the unmanned aerial vehicle includes a main body and a plurality of propellers, the main body is a disc-shaped structure, the propellers rotate with a first axis as a rotating shaft and are connected to the periphery of the main body, the propellers are symmetrically arranged with the axis of the main body as a symmetry axis, and the first axis is parallel to the axis of the main body.
In a possible implementation manner, the air inlet, the air outlet and the water outlet are all arranged at the bottom of the accommodating cavity, and the ventilation opening and the water passing opening are communicated to form a circulation opening.
In a possible implementation manner, the top of the condensation bin is formed with a conical diversion surface.
The high-altitude water taking device provided by the invention has the beneficial effects that: compared with the prior art, the unmanned aerial vehicle of the high-altitude water taking device can fly into the air and stay in a region rich in water vapor, the air inducing unit pumps air into the storage bin from the air inlet of the storage bin, the water vapor in the air is adsorbed by the water absorbing unit, the dry air is discharged from the air outlet of the storage bin, after the water absorbing unit continuously adsorbs the water vapor for a period of time, the heating unit is started to heat the storage bin, so that the water vapor on the water absorbing unit is evaporated and separated out, the water vapor enters the condensation bin, after a period of time, the refrigerating unit is started to condense and cool the water vapor, and the water vapor is cooled and liquefied in the condensation bin. After a certain amount of liquid water is collected, the unmanned aircraft lands on the ground, and the water in the condensation bin is discharged from the water outlet. The invention can liquefy the water vapor in the high air of the desert area and send the liquefied water vapor to the ground, thereby relieving the problem of water shortage in the desert area and being beneficial to the development of the arid area.
Drawings
In order to more clearly illustrate the technical solutions in the embodiments of the present invention, the drawings needed for the embodiments or the prior art descriptions will be briefly described below, and it is obvious that the drawings in the following description are only some embodiments of the present invention, and it is obvious for those skilled in the art to obtain other drawings without creative efforts.
Fig. 1 is a top view of an aerial water intake device according to a first embodiment of the present invention;
fig. 2 is a bottom view of the aerial water intake device according to the first embodiment of the present invention;
FIG. 3 is a schematic structural diagram of a storage bin and a condensing bin according to an embodiment of the present invention;
FIG. 4 is a schematic structural diagram of a storage bin and a condensation bin according to a second embodiment of the present invention;
fig. 5 is a top view of a high altitude water intake device according to a third embodiment of the present invention.
In the figure: 1. an unmanned aerial vehicle; 101. a main body; 102. a propeller; 103. a connecting member; 104. a flow-through opening; 2. a storage bin; 3. a water absorbing unit; 4. a heating unit; 5. an air inlet; 6. a first valve; 7. an air inducing unit; 8. a second valve; 9. an air outlet; 10. a connecting pipe; 11. a third valve; 12. a condensation bin; 13. a refrigeration unit; 14. a fourth valve; 15. a water outlet; 16. a solar panel.
Detailed Description
In order to make the technical problems, technical solutions and advantageous effects to be solved by the present invention more clearly apparent, the present invention is further described in detail below with reference to the accompanying drawings and embodiments. It should be understood that the specific embodiments described herein are merely illustrative of the invention and are not intended to limit the invention.
Referring to fig. 1 to 5, the aerial water intake device provided by the present invention will now be described. The high-altitude water taking device comprises an unmanned aerial vehicle 1, a storage bin 2, an induced draft unit 7, a water absorbing unit 3, a heating unit 4, a condensation bin 12 and a refrigerating unit 13, wherein the unmanned aerial vehicle 1 is provided with an accommodating cavity which is provided with a ventilation opening and a water passing opening, and the unmanned aerial vehicle 1 can fly at high altitude and stays at a high-altitude designated position; the storage bin 2 is arranged in the accommodating cavity, an air inlet 5, an air outlet 9 and a water vapor outlet are formed in the storage bin 2, and the air inlet 5 and the air outlet 9 are respectively communicated with the ventilation opening; the induced draft unit 7 is communicated with the air inlet 5 and/or the air outlet 9 to provide ventilation power; the water absorption unit 3 is arranged in the storage bin 2 and is used for absorbing water vapor in the air; the heating unit 4 is used for heating the water absorption unit 3; the condensation bin 12 is arranged in the accommodating cavity and is provided with a water vapor inlet communicated with the water vapor outlet and a water outlet 15, the water outlet 15 is communicated with the water passing opening, and the condensation bin 12 is used for receiving liquid water formed by condensation of the refrigeration unit 13.
Compared with the prior art, the high-altitude water taking device provided by the invention has the advantages that the unmanned aerial vehicle 1 of the high-altitude water taking device can fly into the air and stay in a region rich in water vapor, the air inducing unit 7 pumps air into the storage bin 2 from the air inlet 5 of the storage bin 2, the water vapor in the air is adsorbed by the water absorbing unit 3, the dry air is discharged from the air outlet 9 of the storage bin 2, after the water absorbing unit 3 continuously adsorbs the water vapor for a period of time, the heating unit 4 is started to heat the storage bin 2, the water vapor on the water absorbing unit 3 is evaporated and separated out, the water vapor enters the condensation bin 12, the refrigerating unit 13 is started to condense and cool the water vapor after a period of time, and the water vapor is cooled and liquefied in the condensation bin 12. After a certain amount of liquid water is collected, the unmanned aerial vehicle 1 lands on the ground, and the water in the condensation bin 12 is discharged through the water outlet 15. The invention can liquefy the water vapor in the high air of the desert area and send the liquefied water vapor to the ground, thereby relieving the problem of water shortage in the desert area and being beneficial to the development of the arid area.
Specifically, the high-altitude water intake device may be provided with a water vapor detector capable of detecting the water vapor content in the air, and when it is detected that the water vapor content in the air is rich, the unmanned aerial vehicle 1 is caused to stay in the area.
In some embodiments, referring to fig. 3 to 4, the water absorption unit 3 is a spiral member and is formed with a spiral water absorption surface, and the outer edge of the water absorption unit 3 is connected with the inner wall of the storage bin 2.
Spiral helicine water absorption unit 3 in this embodiment can make the air admission store 2 back along water absorption unit 3 flows, forms the whirl, and the dwell time of extension air in storing up cun storehouse 2 makes the air fully with water absorption unit 3 contact, has also increased the area of contact of water absorption unit 3 with vapor simultaneously, makes the vapor in the better adsorbed air of water absorption unit 3, improves absorption efficiency.
Optionally, the water absorbing unit 3 is a plate-shaped member made of MOF, where MOF is an organic-inorganic hybrid material having intramolecular pores formed by self-assembly of organic ligands and metal ions or clusters through coordination bonds. The material has the advantages of high porosity, low density, large specific surface area, regular pore channels, adjustable pore diameter, diversity and tailorability of a topological structure and the like. Wherein, the porosity is an important property of the material applied to catalysis, gas adsorption and separation, and the specific surface area is another important index for evaluating the catalytic performance and the adsorption capacity of the porous material. The high porosity and large specific surface area of the MOF material allows it to repeatedly absorb water vapor from air.
Optionally, the absorption unit 3 includes a spiral casing and an adsorption filler filled in the casing, and the adsorption filler can adsorb water vapor in the air and evaporate and separate out the water vapor at high temperature.
In some embodiments, referring to fig. 3, the storage bin 2 is disposed outside the condensation bin 12, the water vapor outlet and the water vapor inlet are communicated through a connecting pipe 10, and the connecting pipe 10 is provided with a third valve 11.
Closing the third valve 11, opening the induced air unit 7, the induced air unit 7 pumps air into the storage bin 2 from the air inlet 5 of the storage bin 2, the water vapor in the air is adsorbed by the water absorption unit 3, the dry air is discharged from the air outlet 9 of the storage bin 2, after the water absorption unit 3 continuously adsorbs the water vapor for a period of time, the heating unit 4 is opened to heat the storage bin 2, the third valve 11 is opened, the water vapor on the water absorption unit 3 is evaporated and separated out, and is introduced into the condensation bin 12 along the connecting pipe 10, and the water vapor is cooled and liquefied in the condensation bin 12. After a while, the third valve 11 and the heating unit 4 are closed, so that the water vapor in the condensation chamber 12 is completely liquefied. And then the process is circulated until the liquid in the condensation bin 12 reaches the preset liquid level, the unmanned aerial vehicle 1 lands on the ground, and the water in the condensation bin 12 is discharged from the water outlet 15.
Optionally, the refrigeration unit 13 is a semiconductor refrigeration piece, a heat absorption end of the semiconductor refrigeration piece is communicated with the condensation bin 12, and a heat release end of the semiconductor refrigeration piece is communicated with the storage bin 2.
The semiconductor refrigeration piece does not have sliding part, holds the intracavity volume limited, uses the semiconductor refrigeration piece can reduce occupation space, and the semiconductor refrigeration piece reliability is high moreover, need not the refrigerant, avoids taking place danger in the high altitude, has also avoided using the refrigerant to cause environmental pollution. The heat absorption end of the refrigeration semiconductor refrigeration piece can adsorb the hot gas in the condensation bin 12, then releases the hot gas into the storage bin 2 through the heat release end, and the heat released by the heat release end can improve the temperature in the storage bin 2, so that the water vapor can be separated out from the absorption piece. In addition, the energy consumption of the heating unit 4 can also be reduced.
In some embodiments, referring to fig. 4, the condensation chamber 12 is disposed in the storage chamber 2, and the top of the storage chamber 2 is connected to the condensation chamber 12 and the bottom is sealed from the storage chamber 2.
In the air got into storage storehouse 2 under induced air unit 7's effect, vapor in the air was adsorbed by water absorption unit 3, after water absorption unit 3 adsorbs saturation, open heating unit 4 and heat water absorption unit 3, make the vapor evaporation in the water absorption unit 3 separate out, in vapor got into condensation storehouse 12 from storage storehouse 2's top, open refrigerating unit 13 and cool off condensation storehouse 12, make the vapor condensation liquefaction, then to the bottom drippage of condensation storehouse 12.
Optionally, the condensation chamber 12 is a heat insulation member to avoid heat exchange between the condensation chamber 12 and the storage chamber 2.
In some embodiments, not shown in the figures, the unmanned aerial vehicle 1 is provided with an airbag.
The airbag can assist the unmanned aerial vehicle 1 to stay at a designated position in the high air, and energy consumption of the unmanned aerial vehicle 1 during parking is reduced. After a certain amount of liquid water is accumulated in the condensation bin 12, the weight of the unmanned aerial vehicle 1 is increased, and the energy consumption generated by overcoming the buoyancy of the air bag is reduced when the unmanned aerial vehicle 1 lands.
Alternatively, the airbag is an annular member, and may be disposed on the top or bottom of the unmanned aerial vehicle 1, or may be disposed at another position.
Optionally, helium is filled in the air bag, the density of the helium is smaller than that of air, buoyancy can be provided for the unmanned aerial vehicle 1, and the helium is good in stability and not prone to danger.
In some embodiments, referring to fig. 5, the high altitude water intake device further includes a solar panel 16 and a battery, the solar panel 16 is disposed outside the unmanned aerial vehicle 1, the solar panel 16 is connected to the battery, and the battery is further electrically connected to the induced air unit 7, the heating unit 4, and the cooling unit 13, respectively.
The solar panel 16 converts the light energy into electric energy and stores the electric energy in the battery, and the battery can provide the electric energy for the induced air unit 7, the heating unit 4 and the refrigerating unit 13, so that the induced air unit 7, the heating unit 4 and the refrigerating unit 13 can continuously work. The operation of the high-altitude water taking device is prevented from being influenced when the electric quantity stored by the battery is insufficient, the unmanned aerial vehicle 1 is not required to carry multiple groups of batteries, the weight of the unmanned aerial vehicle 1 is reduced, and the energy consumption is reduced.
Optionally, solar panels 16 are provided on top of the unmanned aerial vehicle 1.
Alternatively, the battery may power the driver of the unmanned aerial vehicle 1, or may be provided separately from the power source of the driver of the unmanned aerial vehicle 1.
In some embodiments, not shown in the figures, the high altitude water intake device further comprises a controller, a first valve 6 disposed at the air inlet 5, and a second valve 8 disposed at the air outlet 9, and a humidity detector is further disposed in the storage chamber 2, and the first valve 6, the second valve 8, the humidity detector, and the heating unit 4 are respectively connected to the controller in a communication manner.
When the humidity in the storage bin 2 reaches a first preset value of the humidity detector, the humidity detector generates a heating signal, the controller controls the first valve 6 and the second valve 8 to be closed according to the heating signal, the heating unit 4 is started, so that the water vapor on the water absorbing unit 3 is evaporated and separated out, and is introduced into the condensation bin 12 for cooling and liquefaction. When the humidity in the storage bin 2 reaches the second preset value of the humidity detector, the humidity detector generates a heating stop signal, the controller controls the first valve 6 and the second valve 8 to be opened according to the heating stop signal, the heating unit 4 stops, the external air continues to enter the storage bin 2, and the water absorption unit 3 absorbs water vapor in the air. The controller automatically controls the opening and closing of the components, so that the operation process is simplified, and the energy consumption is saved.
It should be noted that the first preset value is greater than the second preset value.
Optionally, the induced draft unit 7 is in communication connection with the controller, when the humidity reaches a first preset value of the humidity detector, the humidity detector generates a heating signal, and the controller controls the induced draft unit 7 to be closed according to the heating signal; when the humidity in the storage bin 2 reaches a second preset value of the humidity detector, the humidity detector generates a heating stop signal, and the controller controls the air inducing unit 7 to be started according to the heating stop signal.
Optionally, a heat insulation layer 17 is arranged outside the storage bin 2 and used for heat insulation of the storage bin 2.
Optionally, when the storage bin 2 is disposed outside the condensation bin 12, the third valve 11 is in communication with the controller. When the humidity in the storage bin 2 reaches a first preset value of the humidity detector, the humidity detector generates a heating signal, the controller controls the third valve 11 to be started according to the heating signal, and water vapor enters the condensation bin 12 along the connecting pipe 10; when the humidity in the storage bin 2 reaches a second preset value of the humidity detector, the humidity detector generates a heating stop signal, and the controller closes the third valve 11 according to the heating stop signal.
Optionally, a temperature detector is further arranged in the storage bin 2, the temperature detector is in communication connection with the controller, when the temperature in the storage bin 2 reaches a fifth preset value, the temperature detector generates a first instruction, and the controller controls the heater to stop heating according to the first instruction; when the temperature in the storage bin 2 is lower than the sixth preset value, the temperature detector generates a second instruction, and the controller controls the heater to start heating according to the second instruction.
It should be noted that the fifth preset value is larger than the sixth preset value, and the fifth preset value is a temperature value enabling water vapor to evaporate and separate out.
In some embodiments, not shown in the figures, a liquid level detector is further arranged in the condensation bin 12, the water outlet 15 is provided with a switch piece which can be opened and closed, and the liquid level detector and the switch piece are respectively in communication connection with the controller.
When the liquid level in the condensation bin 12 reaches a third preset value of the liquid level detector, the liquid level detector generates a starting instruction, and the controller controls the switch piece to be started according to the starting instruction; when the liquid level in the condensation bin 12 reaches the fourth preset value of the liquid level detector, the liquid level detector generates a closing instruction, and the controller controls the switch piece to be closed according to the closing instruction.
It should be noted that the third preset value is greater than the fourth preset value.
Optionally, the switch is a cover plate which can be opened and closed, one side of the cover plate is rotatably connected with the condensation bin 12, and the other side of the cover plate can be opened and closed. The cover plate can also be connected with the condensation bin 12 in a sliding way, so as to shield the water outlet 15 or open the water outlet 15. In this embodiment, the switch member has a driver, and the driver can control the opening and closing of the cover plate.
Optionally, the water outlet 15 is connected to a water outlet pipe, the switch member is a fourth valve 14, and the switch member is disposed on the water outlet pipe.
Optionally, the water outlet 15 is arranged at the bottom of the condensation bin 12.
In some embodiments, referring to fig. 1 to 2, the unmanned aerial vehicle 1 includes a main body 101 and a plurality of propellers 102, the main body 101 is a disk-shaped structure, the propellers 102 are rotatably connected to the outer periphery of the main body 101 by taking a first axis as a rotating shaft, and the plurality of propellers 102 are symmetrically arranged by taking the axis of the main body 101 as a symmetry axis, and the first axis is parallel to the axis of the main body 101.
The propellers 102 rotate to fly the main body 101, and the plurality of propellers 102 are symmetrically arranged with respect to the axis of the main body 101 to make the main body 101 fly smoothly. The disc-shaped structure can reduce the resistance during flight, reduce the energy consumption of flight, and also can ensure the stability of the main body 101 when encountering airflow.
In some embodiments, referring to fig. 1 to 4, the air inlet 5, the air outlet 9 and the water outlet 15 are all disposed at the bottom of the accommodating cavity, and the ventilation opening and the water passing opening are communicated to form a circulation opening 104.
Alternatively, the airbag is disposed at the bottom of the unmanned aerial vehicle 1 and has an annular structure, and the flow opening 104 is disposed at the center of the annular structure without interfering with the airbag.
In some embodiments, referring to fig. 1 to 2, the main body 101 further has a connecting member 103 disposed on an outer periphery of the main body 101, the connecting member 103 is rotatably connected to the main body 101 by using a second axis as a rotating axis, the second axis is perpendicular to the axis of the main body 101, and the connecting member 103 is connected to the propeller 102.
The unmanned aerial vehicle 1 can be steered flexibly in high altitude by rotating the connecting member 103 about the second axis to produce an inclination angle of the propeller 102 with respect to the main body 101 to change the flight direction of the main body 101.
It should be noted that when the propeller 102 rotates with the connecting member 103, the first axis is no longer parallel to the axis of the main body 101.
In some embodiments, referring to fig. 3 to 4, the top of the condensation chamber 12 is formed with a conical diversion surface.
Water vapor gets into the upper portion of mainly distributing in condensation storehouse 12 behind the condensation storehouse 12, cool down through refrigerating unit 13 to condensation storehouse 12 and make the water vapor liquefaction, liquefied water vapor gathers in the bottom of condensation storehouse 12, then flow around towards along the toper water conservancy diversion under the action of gravity, lateral wall inflow bottom through condensation storehouse 12, the water droplet of having avoided the flat-plate top after the water vapor liquefaction directly drops into the bottom, long-time water droplet drips and causes condensation storehouse 12 bottom damaged easily.
Optionally, when the condensation bin 12 is arranged in the storage bin 2, the edge of the conical flow guide surface corresponds to the side wall of the condensation bin 12 up and down, and liquid water is prevented from entering the storage bin 2.
Specifically, when condensation storehouse 12 sets up in storing storehouse 2, the bottom of toper water conservancy diversion face is docked there is the guide plate, and the guide plate can be with the leading-in condensation storehouse 12 of the water droplet of condensation on the toper water conservancy diversion face in, avoid the water droplet to get into and store storehouse 2.
The above description is only for the purpose of illustrating the preferred embodiments of the present invention and is not to be construed as limiting the invention, and any modifications, equivalents and improvements made within the spirit and principle of the present invention are intended to be included within the scope of the present invention.
Claims (10)
1. High altitude water intaking device, its characterized in that includes:
the unmanned aerial vehicle is provided with an accommodating cavity, the accommodating cavity is provided with a ventilation opening and a water passing opening, and the unmanned aerial vehicle can fly at high altitude and stays at a high altitude designated position;
the storage bin is arranged in the accommodating cavity and is provided with an air inlet, an air outlet and a water vapor outlet, and the air inlet and the air outlet are respectively communicated with the ventilation opening;
the air inducing unit is communicated with the air inlet and/or the air outlet so as to provide ventilation power;
the water absorption unit is arranged in the storage bin and is used for absorbing water vapor in the air;
a heating unit for heating the water absorbing unit;
a refrigeration unit; and
the condensation bin is arranged in the accommodating cavity and is provided with a water vapor inlet communicated with the water vapor outlet and a water outlet, the water outlet is communicated with the water passing opening, and the condensation bin is used for receiving liquid water formed by condensation of the refrigeration unit.
2. The aerial water intake device of claim 1, wherein the water absorbing unit is a spiral member and is formed with a spiral water absorbing surface, and an outer edge of the water absorbing unit is connected to an inner wall of the storage chamber.
3. The high altitude water intake device according to claim 1, wherein the storage chamber is provided outside the condensation chamber, the water vapor outlet is communicated with the water vapor inlet through a connecting pipe, and a third valve is provided on the connecting pipe.
4. The aerial water intake device of claim 1, wherein the unmanned aerial vehicle is provided with an airbag.
5. The aerial water intake device of claim 1, further comprising a solar panel and a battery, wherein the solar panel is disposed outside the unmanned aerial vehicle, the solar panel is connected to the battery, and the battery is further electrically connected to the induced air unit, the heating unit, and the cooling unit, respectively.
6. The high altitude water intaking device according to claim 1, further comprising a controller, a first valve disposed at the air inlet, and a second valve disposed at the air outlet, wherein a moisture detector is disposed in the storage compartment, and the first valve, the second valve, the moisture detector, and the heating unit are respectively in communication with the controller.
7. The high altitude water taking device according to claim 6, wherein a liquid level detector is further arranged in the condensation bin, the water outlet is provided with a switch piece which can be opened and closed, and the liquid level detector and the switch piece are respectively in communication connection with the controller.
8. The high altitude water intake apparatus of claim 1, wherein the unmanned aerial vehicle comprises a main body and a plurality of propellers, the main body is a disc-shaped structure, the propellers are rotatably connected to the periphery of the main body by taking a first axis as a rotating shaft, and the propellers are symmetrically arranged by taking the axis of the main body as a symmetry axis, and the first axis is parallel to the axis of the main body.
9. The aerial water intake device of claim 8, wherein the air inlet, the air outlet and the water outlet are all arranged at the bottom of the accommodating cavity, and the ventilation opening and the water passing opening are communicated to form a circulation opening.
10. The high altitude water taking device according to claim 1, wherein the top of the condensation bin is formed with a conical flow guide surface.
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| CN202110989544.5A CN113619799A (en) | 2021-08-26 | 2021-08-26 | High-altitude water taking device |
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| CN202110989544.5A CN113619799A (en) | 2021-08-26 | 2021-08-26 | High-altitude water taking device |
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| JP2020115063A (en) * | 2019-01-18 | 2020-07-30 | 株式会社富士通ゼネラル | Air conditioner |
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| TW200712291A (en) * | 2005-09-14 | 2007-04-01 | Yu-Chien Cho | The reservoirs in the sky and the reservoirs in the sea |
| CN107447810A (en) * | 2017-08-01 | 2017-12-08 | 浙江大学 | Small air water fetching device and its method based on absorption and semiconductor refrigerating |
| CN108391578A (en) * | 2018-05-15 | 2018-08-14 | 李志平 | A kind of gardens watering device |
| JP2020115063A (en) * | 2019-01-18 | 2020-07-30 | 株式会社富士通ゼネラル | Air conditioner |
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Application publication date: 20211109 |