CN110001984B - Unmanned aerial vehicle based on wind-force and two-way influence of flash light can long-range judgement - Google Patents
Unmanned aerial vehicle based on wind-force and two-way influence of flash light can long-range judgement Download PDFInfo
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- CN110001984B CN110001984B CN201910273601.2A CN201910273601A CN110001984B CN 110001984 B CN110001984 B CN 110001984B CN 201910273601 A CN201910273601 A CN 201910273601A CN 110001984 B CN110001984 B CN 110001984B
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- 230000002457 bidirectional effect Effects 0.000 claims abstract description 10
- 230000001681 protective effect Effects 0.000 claims abstract description 8
- 239000011521 glass Substances 0.000 claims description 36
- 230000006698 induction Effects 0.000 claims description 29
- 229920003023 plastic Polymers 0.000 claims description 14
- 239000000463 material Substances 0.000 claims description 13
- 238000004140 cleaning Methods 0.000 claims description 12
- 239000004033 plastic Substances 0.000 claims description 11
- 230000005540 biological transmission Effects 0.000 claims description 9
- 239000000428 dust Substances 0.000 claims description 5
- 238000007789 sealing Methods 0.000 claims description 4
- 239000002184 metal Substances 0.000 claims description 3
- 230000001680 brushing effect Effects 0.000 claims description 2
- 230000008878 coupling Effects 0.000 claims description 2
- 238000010168 coupling process Methods 0.000 claims description 2
- 238000005859 coupling reaction Methods 0.000 claims description 2
- 230000005611 electricity Effects 0.000 claims description 2
- 230000000694 effects Effects 0.000 description 6
- 229920000742 Cotton Polymers 0.000 description 3
- 241000628997 Flos Species 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 239000004744 fabric Substances 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 230000001012 protector Effects 0.000 description 1
- 230000000007 visual effect Effects 0.000 description 1
Images
Classifications
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- B08B1/12—
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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
- B64D45/00—Aircraft indicators or protectors not otherwise provided for
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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
- B64D47/02—Arrangements or adaptations of signal or lighting devices
Abstract
The invention provides an unmanned aerial vehicle capable of being remotely judged based on bidirectional influence of wind power and a flash lamp, which comprises an unmanned aerial vehicle body, wherein a supporting arm is fixedly connected to the surface of the unmanned aerial vehicle body, an unmanned aerial vehicle driving motor is fixedly mounted at one end, far away from the unmanned aerial vehicle body, of the supporting arm, a supporting protective cover is fixedly connected to the outer surface of the unmanned aerial vehicle driving motor, and the surface of the supporting protective cover is fixedly connected with the surface of the supporting arm, so that the unmanned aerial vehicle field is involved. This but unmanned aerial vehicle based on wind-force and flash light two-way influence long-range judgement is through the outer lane re-creation to the unmanned aerial vehicle wing, make people can long-range directly perceived understanding unmanned aerial vehicle flight situation, the various weather flight unmanned aerial vehicle of reply that people can be better, strengthen the interest of unmanned aerial vehicle amusement simultaneously, thereby the effectual unmanned aerial vehicle remote control who has solved general amusement receives the wind direction more easily, the interference of wind-force and cloudy day, people are difficult for directly perceivedly discovering unmanned aerial vehicle's flight, easy erroneous judgement probably causes unmanned aerial vehicle's the problem of crash.
Description
Technical Field
The invention relates to the technical field of unmanned aerial vehicles, in particular to an unmanned aerial vehicle capable of being remotely judged based on bidirectional influence of wind power and a flash lamp.
Background
More and more people enjoy outdoor activities, unmanned aerial vehicles are also very popular entertainment toys outdoors, along with the rapid development of unmanned aerial vehicles, the unmanned aerial vehicles are more and more large in remote control range, but the control difficulty of people is also more and more large when the unmanned aerial vehicles fly far away, the unmanned aerial vehicles are easily interfered by wind direction and wind power in flight, people can only physically feel wind power and wind speed nearby the periphery, the people cannot well feel the wind of the unmanned aerial vehicles far away, the people can only sense the flight of the airplanes through remote control, the feeling is similar to the existence of the sixth feeling, the people are not very visual and accurate, most of people fly the unmanned aerial vehicles in good weather, even if the people still easily damage the unmanned aerial vehicles, and in some cloudy days, the unmanned aerial vehicles are more difficult to control, the general entertainment unmanned aerial vehicles are easily controlled by remote control of the wind direction, Interference of wind power and cloudy days, people are difficult for perceivedly perceiving the flight of unmanned aerial vehicle, and easy erroneous judgement probably causes the crash of unmanned aerial vehicle, so need one kind based on but the unmanned aerial vehicle of wind power and the two-way influence of flash light remote judgement.
Disclosure of Invention
Technical problem to be solved
Aiming at the defects of the prior art, the invention provides the unmanned aerial vehicle capable of being remotely judged based on the bidirectional influence of wind power and a flash lamp, and solves the problems that the common unmanned aerial vehicle for entertainment is easily interfered by wind direction, wind power and cloudy days in remote control, people are not easy to visually perceive the flight of the unmanned aerial vehicle, and the unmanned aerial vehicle is likely to crash due to easy misjudgment.
(II) technical scheme
In order to realize the purpose, the invention is realized by the following technical scheme: the utility model provides an unmanned aerial vehicle based on two-way influence of wind-force and flash light can long-rangely judge, includes the unmanned aerial vehicle body, the fixed surface of unmanned aerial vehicle body is connected with the support arm, the one end fixed mounting that the unmanned aerial vehicle body was kept away from to the support arm has unmanned aerial vehicle driving motor, and unmanned aerial vehicle driving motor's external surface is connected with the support safety cover, the surface of supporting the safety cover is connected with the fixed surface of support arm, unmanned aerial vehicle driving motor's output shaft passes through shaft coupling fixedly connected with pivot, the fixed surface of pivot is connected with the unmanned aerial vehicle wing, the fixed surface who supports the safety cover is connected with the supporting shoe, the fixed surface of supporting shoe is connected with the wing guard circle.
The inner wall of the wing protection ring is provided with a negative charge concentration groove, the width of the inner wall of the negative charge concentration groove is larger than that of the wing of the unmanned aerial vehicle, the horizontal height of the wing of the unmanned aerial vehicle is closer to the horizontal height of the inner bottom wall of the negative charge concentration groove, the inner wall of the negative charge concentration groove is fixedly connected with a negative charge induction coil, the outer ring surface of the negative charge induction coil is fixedly connected with a negative charge tip, the outer surface of the wing protection ring is provided with a positive charge generation groove, the inner wall of the positive charge generation groove is fixedly connected with an induced air net, the surface of the induced air net is fixedly connected with a friction wire, the friction wire is made of silk fabric, the friction wire is positioned inside the positive charge generation groove, the inner wall of the positive charge generation groove is fixedly connected with friction glass, the surface of the friction wire is in contact with the friction glass, and the inner wall of the positive charge generation groove is fixedly connected with a positive charge induction coil, the inner ring inner wall of the positive charge induction coil is fixedly connected with positive charge tips, the surface of the wing protection coil is fixedly connected with a flash glass tube, the flash glass tube penetrates through the upper surface and the lower surface of the wing protection coil, the surfaces of the positive charge tips and the negative charge tips are respectively sleeved with a power transmission tube, the power transmission tubes and the flash glass tube are integrally formed, the surfaces of the positive charge tips and the negative charge tips are respectively fixedly connected with a discharge needle, the discharge needles extend into the flash glass tube and are positioned in the positive charge tips and the discharge needles in the negative charge tips, rare gas is filled in the flash glass tube, the inner wall of the power transmission tube is fixedly connected with a sealing ring, the number of the flash glass tube, the number of the positive charge tips and the negative charge tips is eight, the number of the flash glass tube, the number of the positive charge tips and the number of the negative charge tips are eight, the number of the positive charge tips and the eight negative charge tips are in one-to-one correspondence, and the center of the wing protection coil is used for the center of the wing protection coil Are distributed in a circle as the center of a circle.
The inner bottom wall in positive charge generation groove has been seted up and has been brushed the groove, the hole of placing has been seted up to the inner bottom wall in positive charge generation groove, the hole of clearing has been seted up to the inner bottom wall in positive charge generation groove, the inner wall of placing the hole is pegged graft and is had the go-between, the top fixedly connected with brush dirt silk floss of go-between, the bottom fixedly connected with protrusion pole of go-between, the diameter of protrusion pole is less than the diameter of go-between, the diameter of go-between is less than the diameter in clearance hole, the diameter of protrusion pole is less than the width in clearance groove, the clearance groove, place hole and clearance hole intercommunication each other.
Preferably, the battery can be installed at the bottom of the unmanned aerial vehicle body, a guide wire can be penetrated in the supporting arm, and the input end of the unmanned aerial vehicle driving motor is electrically connected with the output end of the guide wire.
Preferably, the material of the unmanned aerial vehicle body comprises plastic, and the material of the unmanned aerial vehicle wing comprises plastic.
Preferably, the material of the wing protection ring comprises plastics, and the surface of the wing protection ring is black.
Preferably, the top view of the negative charge concentration groove is circular, and the side view of the negative charge concentration groove is curved and is the same as the curve of the rotation of the wing tip of the unmanned aerial vehicle.
Preferably, the positive charge induction coil and the negative charge induction coil are both made of metal conductive plates.
Preferably, the fixed ann in bottom of unmanned aerial vehicle body changes there is the supporting legs, the material of supporting legs includes transparent plastic.
Preferably, the shape of the positive charge generation groove is the same as the shape of the negative charge concentration groove.
Preferably, the diameter of the negative charge induction coil is smaller than that of the friction glass.
(III) advantageous effects
(1) The invention is provided with eight flashing glass tubes, when the unmanned aerial vehicle flies, wings of the unmanned aerial vehicle rapidly rotate to take off, the wings of the unmanned aerial vehicle made of plastic materials rub with air to generate negative charges, the negative charges are close to the edge tips of the wings of the unmanned aerial vehicle under the action of the tip effect, when the wings of the unmanned aerial vehicle rapidly rotate, the negative charges in the wings of the unmanned aerial vehicle are induced by a negative charge induction coil buried in a negative charge concentration groove and are concentrated on eight negative charge tips, meanwhile, friction wires in the flying direction swing against the wind to rub against the glass to generate positive charges, the positive charges are induced by a positive charge induction coil and are concentrated on a positive charge tip which is closest to the wind direction, positive and negative charges mutually induce and discharge the tips, and bright light is generated in the interior filled with rare gas, so that people can observe the position where light flickers, The brightness and the frequency are used for visually judging the flying state of the unmanned aerial vehicle.
(2) When the unmanned aerial vehicle is used, the unmanned aerial vehicle can be suspended and stopped after flying to a position, at the moment, the flashing can be generated through the mode, the flashing position is the windward position, and the effect of remotely judging the wind direction and even the strength of the wind force is achieved.
(3) According to the invention, the wing protection ring is arranged, so that the wings of the unmanned aerial vehicle can be protected, the wings of the unmanned aerial vehicle can be prevented from hurting people, and the wing protection ring is used as a carrier of a flashing effect, so that the overall appearance of the unmanned aerial vehicle is not changed, the attractiveness of the unmanned aerial vehicle is not influenced, and meanwhile, the entertainment interest of the unmanned aerial vehicle is enhanced.
(4) According to the invention, by arranging the dust cotton, when the positive charge generation groove needs to be cleaned, the protruding rod is pushed upwards, the connecting ring is separated from the placing hole and enters the positive charge generation groove, then the protruding rod is pushed to move away in the cleaning groove, the dust cotton is cleaned in the positive charge generation groove, and then the placing hole is taken out through the cleaning hole to be cleaned, so that the situation that flying dust in the positive charge generation groove is gathered is avoided.
(5) According to the unmanned aerial vehicle remote control system, the outer ring of the wings of the unmanned aerial vehicle is recreated, people can remotely and visually know the flight condition of the unmanned aerial vehicle, people can better deal with flying unmanned aerial vehicles in various weathers, and meanwhile, the entertainment interest of the unmanned aerial vehicle is enhanced, so that the problems that the general unmanned aerial vehicle for entertainment is easily interfered by wind direction, wind power and cloudy days in a remote control mode, people cannot easily and visually perceive the flight of the unmanned aerial vehicle, and the unmanned aerial vehicle is likely to crash due to misjudgment are solved.
Drawings
FIG. 1 is a schematic structural view of the present invention;
FIG. 2 is a cross-sectional view of a wing protector configuration of the present invention;
FIG. 3 is an enlarged view of the structure of FIG. 2;
FIG. 4 is an enlarged view of the structure of FIG. 2 at B in accordance with the present invention;
FIG. 5 is a perspective view of the dust sponge structure of the present invention.
Wherein, 1 unmanned aerial vehicle body, 2 support arms, 3 unmanned aerial vehicle driving motor, 4 support safety covers, 5 pivots, 6 unmanned aerial vehicle wings, 7 supporting shoes, 8 wing guard circle, 9 negative charge concentrated groove, 10 negative charge induction coil, 11 negative charge is most advanced, 12 positive charge generation groove, 13 induced air net, 14 friction silk, 15 friction glass, 16 positive charge induction coil, 17 positive charge is most advanced, 18 flashing glass pipe, 19 biography magnetron, 20 discharge needles, 21 sealing washer, 22 brushing groove, 23 place the hole, 24 clearance holes, 25 go-between, 26 brush dirt silk, 27 protruding pole, 28 supporting leggings.
Detailed Description
The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the accompanying drawings of the present invention, and it is obvious that the described embodiments are only a part of the embodiments of the present invention, and not all of the embodiments. All other embodiments, which can be derived by a person skilled in the art from the embodiments given herein without making any creative effort, shall fall within the protection scope of the present invention.
As shown in fig. 1-5, the embodiment of the invention provides an unmanned aerial vehicle capable of being remotely judged based on bidirectional influence of wind power and flash lamps, which comprises an unmanned aerial vehicle body 1, wherein supporting legs 28 are fixedly arranged and rotated at the bottom of the unmanned aerial vehicle body 1, the supporting legs 28 are made of transparent plastics, a supporting arm 2 is fixedly connected to the surface of the unmanned aerial vehicle body 1, an unmanned aerial vehicle driving motor 3 is fixedly installed at one end of the supporting arm 2, which is far away from the unmanned aerial vehicle body 1, a battery can be installed at the bottom of the unmanned aerial vehicle body 1, a guide wire can pass through the inside of the supporting arm 2, the input end of the unmanned aerial vehicle driving motor 3 is electrically connected with the output end of the guide wire, a supporting protective cover 4 is fixedly connected to the outer surface of the unmanned aerial vehicle driving motor 3, the surface of the supporting protective cover 4 is fixedly connected with the surface of the supporting arm 2, the output shaft of the unmanned aerial vehicle driving motor 3 is fixedly connected with a rotating shaft 5 through a coupler, and the surface of the rotating shaft 5 is fixedly connected with unmanned aerial vehicle wings 6, the material of unmanned aerial vehicle body 1 includes plastics, and the material of unmanned aerial vehicle wing 6 includes plastics, and the fixed surface of supporting safety cover 4 is connected with supporting shoe 7, and the fixed surface of supporting shoe 7 is connected with wing guard circle 8, and the material of wing guard circle 8 includes plastics, and the surface of wing guard circle 8 is black.
The inner wall of the wing protection ring 8 is provided with a negative charge concentration groove 9, the top view of the negative charge concentration groove 9 is circular, the side view of the negative charge concentration groove 9 is curved and is the same as the tip rotating curve shape of the wing 6 of the unmanned aerial vehicle, the width of the inner wall of the negative charge concentration groove 9 is larger than the width of the wing 6 of the unmanned aerial vehicle, the horizontal height of the wing 6 of the unmanned aerial vehicle is closer to the horizontal height of the inner bottom wall of the negative charge concentration groove 9, the inner wall of the negative charge concentration groove 9 is fixedly connected with a negative charge induction coil 10, the outer ring surface of the negative charge induction coil 10 is fixedly connected with a negative charge tip 11, the outer surface of the wing protection ring 8 is provided with a positive charge generation groove 12, the shape of the positive charge generation groove 12 is the same as that of the negative charge concentration groove 9, the inner wall of the positive charge generation groove 12 is fixedly connected with an air induction net 13, the surface of the air induction net 13 is fixedly connected with a friction wire 14, and the friction wire 14 comprises silk, the friction wire 14 is positioned inside the positive charge generating groove 12, the inner wall of the positive charge generating groove 12 is fixedly connected with friction glass 15, the diameter of the negative charge induction coil 10 is smaller than that of the friction glass 15, the surface of the friction wire 14 is contacted with the friction glass 15, the inner wall of the positive charge generating groove 12 is fixedly connected with a positive charge induction coil 16, the positive charge induction coil 16 and the negative charge induction coil 10 are both made of metal conductive plates, the inner wall of the inner ring of the positive charge induction coil 16 is fixedly connected with a positive charge tip 17, the surface of the wing protection ring 8 is fixedly connected with a flash glass tube 18, the flash glass tube 18 penetrates through the upper surface and the lower surface of the wing protection ring 8, the surfaces of the positive charge tip 17 and the negative charge tip 11 are both sleeved with a current transmission tube 19, the current transmission tube 19 and the flash glass tube 18 are integrally formed, and the surfaces of the positive charge tip 17 and the negative charge tip 11 are both fixedly connected with discharge needles 20, the discharge needle 20 extends into the inside of the flash glass tube 18, the discharge needle 20 located at the positive charge tip 17 is opposite to and does not contact with the discharge needle 20 located at the negative charge tip 11, rare gas is filled in the inside of the flash glass tube 18, a sealing ring 21 is fixedly connected to the inner wall of the electricity transmission tube 19, the number of the flash glass tube 18, the number of the positive charge tips 17 and the number of the negative charge tips 11 are eight, and the eight flash glass tubes 18, the eight positive charge tips 17 and the eight negative charge tips 11 are in one-to-one correspondence and are circumferentially distributed by taking the center of the wing protection ring 8 as a circle center.
The inner bottom wall in positive charge generation groove 12 has been seted up and has been cleaned brush groove 22, the inner bottom wall in positive charge generation groove 12 has been seted up and has been placed hole 23, cleaning hole 24 has been seted up to the inner bottom wall in positive charge generation groove 12, the inner wall of placing hole 23 is pegged graft and is had go-between 25, the top fixedly connected with brush dirt cotton 26 of go-between 25, the bottom fixedly connected with protrusion pole 27 of go-between 25, the diameter of protrusion pole 27 is less than the diameter of go-between 25, the diameter of go-between 25 is less than cleaning hole 24's diameter, the diameter of protrusion pole 27 is less than the width of cleaning brush groove 22, clean brush groove 22, place hole 23 and cleaning hole 24 and communicate each other.
When the unmanned aerial vehicle flying, the wings 6 of the unmanned aerial vehicle rapidly rotate to take off, the wings 6 of the unmanned aerial vehicle made of plastic materials rub with air to generate negative charges, the negative charges are close to the edge tips of the wings 6 of the unmanned aerial vehicle under the action of the tip effect, when the wings 6 of the unmanned aerial vehicle rapidly rotate, the internal negative charges are induced by the negative charge induction coil 10 embedded in the negative charge concentration groove 9 and are concentrated on the eight negative charge tips 11, meanwhile, the friction wire 14 in the flying direction rubs against the friction glass 15 in a swinging mode facing the wind to generate positive charges, the positive charges are induced by the positive charge induction coil 16 and are concentrated on the positive charge tips 17 at the closest distance corresponding to the wind direction, the positive charges and the negative charges are mutually induced by the discharge needles 20 in the flasher tube 18 facing the wind direction and are discharged at the tips, and bright light is generated in the flasher tube 18 filled with rare gas, and people observe the flickering position of light, Luminance and frequency come the state of audio-visual judgement unmanned aerial vehicle flight, at unmanned aerial vehicle flight in-process, with unmanned aerial vehicle flying to a position after hang and stop, still can produce the flash of light through above-mentioned mode this moment, the situation through the light scintillation when hovering judges the flight environment of unmanned aerial vehicle position to accomplish whole unmanned aerial vehicle's use based on wind-force and the two-way influence of flash light can long-range judgement.
Claims (8)
1. The utility model provides an unmanned aerial vehicle based on two-way influence of wind-force and flash light can long-rangely judge, its characterized in that: the unmanned aerial vehicle comprises an unmanned aerial vehicle body (1), wherein a supporting arm (2) is fixedly connected to the surface of the unmanned aerial vehicle body (1), an unmanned aerial vehicle driving motor (3) is fixedly installed at one end, away from the unmanned aerial vehicle body (1), of the supporting arm (2), a supporting protective cover (4) is fixedly connected to the outer surface of the unmanned aerial vehicle driving motor (3), the surface of the supporting protective cover (4) is fixedly connected with the surface of the supporting arm (2), an output shaft of the unmanned aerial vehicle driving motor (3) is fixedly connected with a rotating shaft (5) through a shaft coupling, an unmanned aerial vehicle wing (6) is fixedly connected to the surface of the rotating shaft (5), a supporting block (7) is fixedly connected to the surface of the supporting protective cover (4), and a wing protective ring (8) is fixedly connected to the surface of the supporting block (7);
negative charge concentrated groove (9) has been seted up to the inner wall of wing guard circle (8), the width of negative charge concentrated groove (9) inner wall will be greater than the width of unmanned aerial vehicle wing (6), the horizontal height of unmanned aerial vehicle wing (6) level wall is more pressed close to negative charge concentrated groove (9) interior diapire, the inner wall fixedly connected with negative charge induction coil (10) of negative charge concentrated groove (9), the outer lane fixed surface of negative charge induction coil (10) is connected with negative charge pointed end (11), positive charge generation groove (12) has been seted up to the surface of wing guard circle (8), the inner wall fixedly connected with induced air net (13) of positive charge generation groove (12), the fixed surface of induced air net (13) is connected with friction silk (14), the material of friction silk (14) is silk, friction silk (14) are located the inside of positive charge generation groove (12), the inner wall of the positive charge generation groove (12) is fixedly connected with friction glass (15), the surface of the friction wire (14) is in contact with the friction glass (15), the inner wall of the positive charge generation groove (12) is fixedly connected with a positive charge induction coil (16), the inner ring inner wall of the positive charge induction coil (16) is fixedly connected with a positive charge tip (17), the surface of the wing protection ring (8) is fixedly connected with a flash glass tube (18), the flash glass tube (18) penetrates through the upper surface and the lower surface of the wing protection ring (8), the surfaces of the positive charge tip (17) and the negative charge tip (11) are respectively sleeved with a power transmission tube (19), the power transmission tube (19) and the flash glass tube (18) are integrally formed, the surfaces of the positive charge tip (17) and the negative charge tip (11) are respectively fixedly connected with a discharge needle (20), and the discharge needles (20) extend into the flash glass tube (18), the discharge needles (20) located at the positive charge tips (17) and the discharge needles (20) located at the negative charge tips (11) are opposite to each other and are not in contact with each other, rare gas is filled in the flash glass tubes (18), the inner walls of the power transmission tubes (19) are fixedly connected with sealing rings (21), the number of the flash glass tubes (18), the number of the positive charge tips (17) and the number of the negative charge tips (11) are eight, the eight flash glass tubes (18), the eight positive charge tips (17) and the eight negative charge tips (11) are in one-to-one correspondence, and the eight flash glass tubes, the eight positive charge tips (17) and the eight negative charge tips (11) are circumferentially distributed by taking the centers of the wing protection rings (8) as the circle centers;
the inner bottom wall of the positive charge generation groove (12) is provided with a cleaning groove (22), the inner bottom wall of the positive charge generation groove (12) is provided with a placing hole (23), the inner bottom wall of the positive charge generation groove (12) is provided with a cleaning hole (24), the inner wall of the placing hole (23) is inserted with a connecting ring (25), the top of the connecting ring (25) is fixedly connected with dust brushing sponge (26), the bottom of the connecting ring (25) is fixedly connected with a protruding rod (27), the diameter of the protruding rod (27) is smaller than that of the connecting ring (25), the diameter of the connecting ring (25) is smaller than that of the cleaning hole (24), the diameter of the protruding rod (27) is smaller than that of the cleaning groove (22), and the cleaning groove (22), the placing hole (23) and the cleaning hole (24) are communicated with each other;
the material of unmanned aerial vehicle body (1) is plastics, the material of unmanned aerial vehicle wing (6) is plastics.
2. The unmanned aerial vehicle based on wind power and flashlight bidirectional influence can be judged remotely according to claim 1, characterized in that: the battery is installed to unmanned aerial vehicle body (1) bottom, the inside threading wire of support arm (2), the input of unmanned aerial vehicle driving motor (3) is connected with the output electricity of wire.
3. The unmanned aerial vehicle based on wind power and flashlight bidirectional influence can be judged remotely according to claim 1, characterized in that: the wing protection ring (8) is made of plastic, and the surface of the wing protection ring (8) is black.
4. The unmanned aerial vehicle based on wind power and flashlight bidirectional influence can be judged remotely according to claim 1, characterized in that: the top view of the negative charge concentration groove (9) is circular, the side view of the negative charge concentration groove (9) is in a curve shape, and the curve shape is the same as the rotation curve shape of the tip of the unmanned aerial vehicle wing (6).
5. The unmanned aerial vehicle based on wind power and flashlight bidirectional influence can be judged remotely according to claim 1, characterized in that: the positive charge induction coil (16) and the negative charge induction coil (10) are both made of metal conductive plates.
6. The unmanned aerial vehicle based on wind power and flashlight bidirectional influence can be judged remotely according to claim 1, characterized in that: the fixed ann in bottom of unmanned aerial vehicle body (1) changes there is supporting legs (28), the material of supporting legs (28) is transparent plastic.
7. The unmanned aerial vehicle based on but wind-force and flash light two-way influence remote judgement of claim 4 characterized in that: the shape of the positive charge generation grooves (12) is the same as that of the negative charge concentration grooves (9).
8. The unmanned aerial vehicle based on wind power and flashlight bidirectional influence can be judged remotely according to claim 1, characterized in that: the diameter of the negative charge induction coil (10) is smaller than that of the friction glass (15).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910273601.2A CN110001984B (en) | 2019-04-06 | 2019-04-06 | Unmanned aerial vehicle based on wind-force and two-way influence of flash light can long-range judgement |
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| CN201910273601.2A CN110001984B (en) | 2019-04-06 | 2019-04-06 | Unmanned aerial vehicle based on wind-force and two-way influence of flash light can long-range judgement |
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| CN110001984B true CN110001984B (en) | 2022-06-21 |
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Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB911787A (en) * | 1960-04-21 | 1962-11-28 | Meech Electric Drives London L | Improvements in and relating to ionizing air guns |
| US6199244B1 (en) * | 1998-10-07 | 2001-03-13 | Vorwerk & Co. Interholding Gmbh | Vacuum cleaner with electrostatically charged components |
| GB201310728D0 (en) * | 2013-06-17 | 2013-07-31 | Majoe Dennis | Lighter Than Air Drone |
| CN108686836A (en) * | 2017-04-12 | 2018-10-23 | 张航菲 | Unmanned aerial vehicle group sprays high-pressure electrostatic except haze method |
Family Cites Families (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB2443670B (en) * | 2006-11-13 | 2011-03-23 | Steven Martin Hudson | Aircraft and conductive bodies |
| GR20130100619A (en) * | 2013-10-25 | 2015-05-18 | Ιωαννης Γεωργιου Μικρος | Small-sized bird-like flying device and application thereof |
| US9993852B2 (en) * | 2014-08-20 | 2018-06-12 | Elwha Llc | Surface cleaning unmanned aerial vehicle |
| WO2018182944A1 (en) * | 2017-03-25 | 2018-10-04 | Yu Simon Siu Chi | Multi-function photo electro acoustic ions drone |
| CN107776901A (en) * | 2017-12-21 | 2018-03-09 | 南京菱亚汽车技术研究院 | A kind of unmanned plane using wind power generation |
| CN208325653U (en) * | 2018-03-13 | 2019-01-04 | 清远市巨劲科技有限公司 | A kind of unmanned plane of taking photo by plane with defencive function |
| CN108522472A (en) * | 2018-04-08 | 2018-09-14 | 吴李海 | A kind of plant protection multi-rotor unmanned aerial vehicle |
-
2019
- 2019-04-06 CN CN201910273601.2A patent/CN110001984B/en active Active
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB911787A (en) * | 1960-04-21 | 1962-11-28 | Meech Electric Drives London L | Improvements in and relating to ionizing air guns |
| US6199244B1 (en) * | 1998-10-07 | 2001-03-13 | Vorwerk & Co. Interholding Gmbh | Vacuum cleaner with electrostatically charged components |
| GB201310728D0 (en) * | 2013-06-17 | 2013-07-31 | Majoe Dennis | Lighter Than Air Drone |
| CN108686836A (en) * | 2017-04-12 | 2018-10-23 | 张航菲 | Unmanned aerial vehicle group sprays high-pressure electrostatic except haze method |
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