CN113371217A - Unmanned aerial vehicle with anti-fog function based on remote patrol - Google Patents
Unmanned aerial vehicle with anti-fog function based on remote patrol Download PDFInfo
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- CN113371217A CN113371217A CN202110916508.6A CN202110916508A CN113371217A CN 113371217 A CN113371217 A CN 113371217A CN 202110916508 A CN202110916508 A CN 202110916508A CN 113371217 A CN113371217 A CN 113371217A
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- 229920003023 plastic Polymers 0.000 claims description 6
- 239000004033 plastic Substances 0.000 claims description 6
- 230000017525 heat dissipation Effects 0.000 claims description 3
- 239000003292 glue Substances 0.000 claims 3
- 238000007689 inspection Methods 0.000 abstract description 7
- 230000000694 effects Effects 0.000 description 4
- 238000010586 diagram Methods 0.000 description 3
- 238000001035 drying Methods 0.000 description 2
- 239000013013 elastic material Substances 0.000 description 2
- 238000012544 monitoring process Methods 0.000 description 2
- 210000003437 trachea Anatomy 0.000 description 2
- 238000004026 adhesive bonding Methods 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000003139 buffering effect Effects 0.000 description 1
- 238000013016 damping Methods 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 238000001125 extrusion Methods 0.000 description 1
- 239000012634 fragment Substances 0.000 description 1
- 230000005484 gravity Effects 0.000 description 1
- 230000002093 peripheral effect Effects 0.000 description 1
- 230000001846 repelling effect Effects 0.000 description 1
- 210000005077 saccule Anatomy 0.000 description 1
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D47/00—Equipment not otherwise provided for
- B64D47/08—Arrangements of cameras
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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
-
- 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
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
- B64U10/10—Rotorcrafts
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F26—DRYING
- F26B—DRYING SOLID MATERIALS OR OBJECTS BY REMOVING LIQUID THEREFROM
- F26B21/00—Arrangements or duct systems, e.g. in combination with pallet boxes, for supplying and controlling air or gases for drying solid materials or objects
- F26B21/001—Drying-air generating units, e.g. movable, independent of drying enclosure
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F26—DRYING
- F26B—DRYING SOLID MATERIALS OR OBJECTS BY REMOVING LIQUID THEREFROM
- F26B21/00—Arrangements or duct systems, e.g. in combination with pallet boxes, for supplying and controlling air or gases for drying solid materials or objects
- F26B21/004—Nozzle assemblies; Air knives; Air distributors; Blow boxes
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- 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
- B64U2101/30—UAVs specially adapted for particular uses or applications for imaging, photography or videography
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Remote Sensing (AREA)
- Toys (AREA)
- Studio Devices (AREA)
Abstract
The invention discloses an unmanned aerial vehicle with an anti-fog function based on remote inspection, which comprises an unmanned aerial vehicle body and two undercarriage, wherein the unmanned aerial vehicle body is connected with the two undercarriage through bolts, the two undercarriage are symmetrically distributed on the unmanned aerial vehicle body, the outer wall of the bottom of the unmanned aerial vehicle body is provided with a fixing mechanism, the outer wall of the bottom of the fixing mechanism is provided with an inspection mechanism, one side of the outer wall of the bottom of the fixing mechanism is provided with an anti-fog mechanism, the anti-fog mechanism comprises a balloon and a box body, and the balloon and the box body are spliced. The invention can prevent the temperature difference between the unmanned aerial vehicle and the external environment from being larger due to cold weather or foggy days, so that fog is generated on the surface of the patrol mechanism, the patrol work of the patrol mechanism is further interfered, hot air can be diffused, the contact range of heat and the fog is improved, and the influence of the fog on the patrol of the unmanned aerial vehicle can be effectively prevented.
Description
Technical Field
The invention relates to the technical field of unmanned aerial vehicles, in particular to an unmanned aerial vehicle with an anti-fog function based on remote inspection.
Background
Unmanned aerial vehicle is the unmanned vehicles who utilizes radio remote control equipment and the program control device of self-contained to control, and the very big work that has made things convenient for people of appearance of unmanned aerial vehicle, unmanned aerial vehicle's kind can be regarded as plant protection unmanned aerial vehicle, patrol unmanned aerial vehicle and fire control unmanned aerial vehicle etc..
Patrol unmanned aerial vehicle mainly used remote monitoring to in time handle emergency, current patrol unmanned aerial vehicle can accomplish the remote monitoring to this region through manual operation at appointed regional class, thereby effectively avoid this regional emergency's emergence.
Current tour unmanned aerial vehicle does not possess antifog function, consequently, when the weather is clear, can not lead to the fact the influence to unmanned aerial vehicle's work, but, when meetting cold weather or fog day, because unmanned aerial vehicle just begins work and unmanned aerial vehicle and external environment between the difference in temperature is great, consequently, can produce one deck fog on unmanned aerial vehicle's that cruises camera surface, and fog can lead to the fact the interference to unmanned aerial vehicle's tour.
Disclosure of Invention
The invention aims to solve the defect that the existing patrol unmanned aerial vehicle does not have an anti-fog function and fog can interfere with patrol of the unmanned aerial vehicle, and provides the unmanned aerial vehicle with the anti-fog function based on remote patrol.
In order to achieve the purpose, the invention adopts the following technical scheme:
the utility model provides an unmanned aerial vehicle that has antifog function based on long-range tour, includes unmanned aerial vehicle body and two undercarriage, through bolted connection, two between unmanned aerial vehicle body and two undercarriage landing gear be the symmetric distribution on the unmanned aerial vehicle body, the bottom outer wall of unmanned aerial vehicle body is provided with fixed establishment, fixed establishment's bottom outer wall is provided with tour mechanism, one side of fixed establishment bottom outer wall is provided with antifog mechanism, antifog mechanism includes sacculus and box, splice between sacculus and the box, the inlet port has been seted up to one side outer wall of box, the louvre has been seted up to one side of unmanned aerial vehicle body bottom outer wall, fixedly connected with trachea between louvre and the inlet port, the gas vent has been seted up to the bottom outer wall of box, and the shape of gas vent is the splayed.
Preferably, fixed establishment includes first mount and second mount, the first spring of fixedly connected with between first mount and the second mount, through bolted connection between first mount and the unmanned aerial vehicle body, the equal fixedly connected with locating piece of both sides outer wall of first mount, the equal fixedly connected with location slide rail of both sides outer wall of second mount, form sliding connection between location slide rail and the locating piece.
Preferably, the tour mechanism includes support frame and camera, the both sides outer wall of support frame set up threaded hole, and the inner wall threaded connection of two screw holes has the fastening bolt, the both sides outer wall fixedly connected with thread bush of camera, threaded connection between thread bush and the fastening bolt, pass through bolted connection between support frame and the second mount.
Preferably, the bottom outer wall of support frame and the top outer wall of camera all fixedly connected with magnet, two attract each other between the magnet.
Preferably, an air guide mechanism is arranged on the outer wall of one side of the second fixing frame, the air guide mechanism comprises an air guide plate and a top block, the air guide plate is connected with the top block through a bolt, the air guide plate is connected with the second fixing frame through a hinge, a third spring is fixedly connected between the air guide plate and the second fixing frame, and the top block is naturally contacted with the balloon.
Preferably, the edge of the inner wall of the air inlet hole is fixedly connected with an overflow block, the overflow block is conical, and the overflow block is composed of a plurality of plastic elastic sheets.
Preferably, the top outer wall of undercarriage is provided with supporting mechanism, supporting mechanism includes backup pad, first gasbag and second gasbag, through bolted connection between backup pad and the undercarriage, be provided with the pipe between first gasbag and the second gasbag, bond between first gasbag and the backup pad, the fixed orifices has been seted up to the bottom outer wall of undercarriage, and the inner wall sliding connection of fixed orifices has the slider, the equal fixedly connected with second spring in both sides of slider top outer wall, the top outer wall fixedly connected with roof of second spring, fixedly connected with fixed plate between the relative both sides outer wall of undercarriage, the second gasbag is located between roof and the fixed plate, splices between second gasbag and the roof.
Preferably, the top outer wall of the first balloon is provided with a plurality of vesicles, and the vesicles are hemispherical in shape.
Preferably, a plurality of sound holes are formed in the outer wall of one side of the air deflector, and the sound holes are conical.
Preferably, a plurality of baffles are fixedly connected between the inner walls of two opposite sides of the sound hole, a plurality of whistles are fixed on the outer walls of the baffles, and the baffles are in a blade shape.
The invention has the beneficial effects that:
according to the invention, through the arranged anti-fog mechanism, when the unmanned aerial vehicle starts to patrol, as the unmanned aerial vehicle emits heat when patrolling, the heat can be conveyed to the interior of the box body through the air pipe, and the heat is conveyed to the surface of the patrol mechanism through the air outlet, the fog adhered to the patrol mechanism is dried through hot air, so that the problem that the temperature difference between the unmanned aerial vehicle and the external environment is large due to cold weather or foggy days is prevented, the fog is generated on the surface of the patrol mechanism, and the patrol work of the patrol mechanism is further interfered is solved.
Drawings
Fig. 1 is a schematic structural diagram of an unmanned aerial vehicle with an anti-fog function based on remote tour, which is provided by the invention;
fig. 2 is a schematic view of a main view structure of an unmanned aerial vehicle with an anti-fog function based on remote tour, which is provided by the invention;
fig. 3 is a schematic structural view of a fixing mechanism of an unmanned aerial vehicle with an anti-fog function based on remote patrol, which is provided by the invention;
fig. 4 is a schematic structural view of an anti-fog mechanism of an unmanned aerial vehicle with an anti-fog function based on remote tour, which is provided by the invention;
fig. 5 is a schematic view of an internal structure of an anti-fog mechanism of an unmanned aerial vehicle with an anti-fog function based on remote patrol, which is provided by the invention;
fig. 6 is a schematic structural view of a supporting mechanism of an unmanned aerial vehicle with an anti-fog function based on remote patrol, which is provided by the invention;
fig. 7 is a schematic structural diagram of a first air bag and a second air bag of an unmanned aerial vehicle with an anti-fog function based on remote tour, which is provided by the invention;
fig. 8 is a schematic structural view of an air guide mechanism of an unmanned aerial vehicle with an anti-fog function based on remote patrol, which is provided by the invention;
fig. 9 is a schematic structural view of an air deflector of an unmanned aerial vehicle with an anti-fog function based on remote tour, which is provided by the invention;
fig. 10 is a schematic structural diagram of a position a of an unmanned aerial vehicle with an anti-fog function based on remote tour according to the present invention;
fig. 11 is a schematic structural view of a patrol mechanism of an unmanned aerial vehicle with an anti-fog function based on remote patrol, which is provided by the invention.
In the drawings: 1-an unmanned aerial vehicle body; 2-a landing gear; 3-a support mechanism; 4-an anti-fog mechanism; 5-a support plate; 6-a first balloon; 7-a patrol mechanism; 8-a catheter; 9-an air guide mechanism; 10-a fixing mechanism; 11-a first spring; 12-positioning blocks; 13-a first mount; 14-a second mount; 15-positioning the slide rail; 16-a balloon; 17-a box body; 18-trachea; 19-an exhaust port; 20-overflow block; 21-fixing the plate; 22-a second spring; 23-a slide block; 24-a top plate; 25-a second balloon; 26-vesicles; 27-a wind deflector; 28-a top block; 29-a third spring; 30-sound hole; 31-a baffle; 32-whistle; 33-a camera; 34-a support frame; 35-a magnet; 36-a threaded sleeve; 37-fastening bolt.
Detailed Description
Reference will now be made in detail to embodiments of the present patent, examples of which are illustrated in the accompanying drawings, wherein like or similar reference numerals refer to the same or similar elements or elements having the same or similar function throughout. The embodiments described below with reference to the drawings are exemplary only for the purpose of explaining the present patent and are not to be construed as limiting the present patent.
In the description of this patent, it is to be understood that the terms "center," "upper," "lower," "front," "rear," "left," "right," "vertical," "horizontal," "top," "bottom," "inner," "outer," and the like are used in the orientations and positional relationships indicated in the drawings for the convenience of describing the patent and for the simplicity of description, and are not intended to indicate or imply that the referenced devices or elements must have a particular orientation, be constructed and operated in a particular orientation, and are not to be considered limiting of the patent.
In the description of this patent, it is noted that unless otherwise specifically stated or limited, the terms "mounted," "connected," and "disposed" are to be construed broadly and can include, for example, fixedly connected, disposed, detachably connected, disposed, or integrally connected and disposed. The specific meaning of the above terms in this patent may be understood by those of ordinary skill in the art as appropriate.
Example 1
Referring to fig. 1-5, 8 and 11, an unmanned aerial vehicle with an anti-fog function based on remote inspection comprises an unmanned aerial vehicle body 1 and two landing gears 2, the unmanned aerial vehicle body 1 and the two landing gears 2 are connected through bolts, the two landing gears 2 are symmetrically distributed on the unmanned aerial vehicle body 1, a fixing mechanism 10 is arranged on the outer wall of the bottom of the unmanned aerial vehicle body 1, an inspection mechanism 7 is arranged on the outer wall of the bottom of the fixing mechanism 10, an anti-fog mechanism 4 is arranged on one side of the outer wall of the bottom of the fixing mechanism 10, the anti-fog mechanism 4 comprises a balloon 16 and a box body 17, the balloon 16 is glued with the box body 17, an air inlet is arranged on the outer wall of one side of the box body 17, a heat dissipation hole is arranged on one side of the outer wall of the bottom of the unmanned aerial vehicle body 1, an air pipe 18 is fixedly connected between the heat dissipation hole and the air inlet, an air outlet 19 is arranged on the outer wall of the bottom of the box body 17, and the air outlet 19 is in a splayed shape, when unmanned aerial vehicle body 1 began to patrol the during operation, because unmanned aerial vehicle body 1 can give off the department heat when patrolling, and the heat can be carried to the inside of box 17 through trachea 18, and carry the heat to the surface of patrolling mechanism 7 through gas vent 19, thereby it handles to patrol the fog drying of adhering on the mechanism 7 through steam, thereby make fog disappear from patrolling the surface of mechanism 7, prevent to lead to the difference in temperature between unmanned aerial vehicle and the external environment great because cold weather or foggy day, thereby make the surface of patrolling mechanism 7 produce fog, and then cause the interference to the work of patrolling of mechanism 7, furthermore, the shape of gas vent 19 is the splayed, consequently, the heat can spread when passing through gas vent 19, improve the contact range of heat and fog, thereby can effectually prevent that fog from causing the influence to the patrol of unmanned aerial vehicle body 1.
In the invention, the fixing mechanism 10 comprises a first fixing frame 13 and a second fixing frame 14, a first spring 11 is connected between the first fixing frame 13 and the second fixing frame 14 through bolts, the first fixing frame 13 is connected with the unmanned aerial vehicle body 1 through bolts, the outer walls of the two sides of the first fixing frame 13 are connected with positioning blocks 12 through bolts, the outer walls of the two sides of the second fixing frame 14 are connected with positioning slide rails 15 through bolts, the positioning slide rails 15 are in sliding connection with the positioning blocks 12, the unmanned aerial vehicle body 1 can generate recoil at the moment of taking off or landing, and the first spring 11 can play a role in buffering and damping on the inspection mechanism 7, thereby protect tour mechanism 7, simultaneously, can fix a position the processing to the direction of motion of first spring 11 through the cooperation between locating piece 12 and the location slide rail 15, prevent that first spring 11 from taking place the swing and causing the influence to the tour work of tour mechanism 7.
In the invention, the inspection mechanism 7 comprises a support frame 34 and a camera 33, threaded holes are formed in the outer walls of two sides of the support frame 34, fastening bolts 37 are in threaded connection with the inner walls of the two threaded holes, threaded sleeves 36 are in threaded connection with the outer walls of two sides of the camera 33 through bolts, the threaded sleeves 36 are in threaded connection with the fastening bolts 37, and the support frame 34 is in threaded connection with the second fixing frame 14, so that the camera 33 can be conveniently detached, and the camera 33 can be conveniently maintained.
According to the unmanned aerial vehicle, the magnets 35 are connected to the outer wall of the bottom of the support frame 34 and the outer wall of the top of the camera 33 through the bolts, the two magnets 35 attract each other, and when the unmanned aerial vehicle body 1 is used for patrolling, due to the fact that the resistance of wind is large, the camera 33 can be pushed backwards when the unmanned aerial vehicle body 1 takes off, the camera 33 can be further fixed through the attraction between the two magnets 35, and therefore the stability of the camera 33 during working is improved.
In the invention, the air guide mechanism 9 is arranged on the outer wall of one side of the second fixing frame 14, the air guide mechanism 9 comprises an air guide plate 27 and a top block 28, the air guide plate 27 is connected with the top block 28 through a bolt, the air guide plate 27 is connected with the second fixing frame 14 through a hinge, a third spring 29 is connected between the air guide plate 27 and the second fixing frame 14 through a bolt, the top block 28 is naturally contacted with the balloon 16, when heat enters the box body 17 through the air pipe 18, part of hot air can be discharged through the air outlet 19, and other part of hot air can remain in the box body 17 and can not be utilized, therefore, when the unmanned aerial vehicle body 1 takes off, the air guide plate 27 and the top block 28 can compress the balloon 16 through the action force of wind, and when the balloon 16 is compressed, the air pressure in the box body 17 can be increased, therefore, the hot air can be rapidly ejected through the air outlet 19 after being compressed, thereby can improve the drying rate of hot gas to the fog, and when the elasticity of third spring 29 was greater than wind-force, aviation baffle 27 can resume under the effect of third spring 29, at this moment, sacculus 16 can recover, and because the effect of wind can continuously be used in aviation baffle 27, consequently, aviation baffle 27 can carry out reciprocating swing under the effect of wind-force and the effect of third spring 29 elasticity, thereby can be constantly erupt hot gas from the inside of box 17 through sacculus 16, and then improve the treatment effeciency of hot gas to the fog.
In the invention, the edge of the inner wall of the air inlet is connected with an overflow block 20 through a bolt, the overflow block 20 is in a conical shape, the overflow block 20 is composed of a plurality of plastic elastic sheets, when the balloon 16 is used for conveying hot air, part of the hot air can flow back to the inside of the unmanned aerial vehicle body 1, so that the internal elements of the unmanned aerial vehicle body 1 can be damaged, and the heat can be prevented from flowing back through the overflow block 20, because the overflow block 20 is made up of a plurality of plastic elastic pieces, when the balloon 16 is compressed, the internal air pressure will increase, and the plastic elastic pieces will be gathered under the action of the air flow, thereby preventing hot air from flowing back to the inside of the unmanned aerial vehicle body 1 through the air inlet holes, and when the saccule 16 is recovered, the air pressure inside the box body 17 can be reduced, thereby can make the plastics shell fragment expand, and then can carry the inside of box 17 with the inside heat of unmanned aerial vehicle body 1.
Example 2
Referring to fig. 1, 2, 6 and 7, in comparison with embodiment 1, on the basis of embodiment 1, a supporting mechanism 3 is arranged on the outer wall of the top of an undercarriage 2, the supporting mechanism 3 includes a supporting plate 5, a first air bag 6 and a second air bag 25, the supporting plate 5 is connected with the undercarriage 2 through bolts, a conduit 8 is arranged between the first air bag 6 and the second air bag 25, the first air bag 6 is bonded with the supporting plate 5, a fixing port is arranged on the outer wall of the bottom of the undercarriage 2, a sliding block 23 is connected to the inner wall of the fixing port in a sliding manner, second springs 22 are connected to two sides of the outer wall of the top of the sliding block 23 through bolts, top plates 24 are connected to the outer wall of the top of the second springs 22 through bolts, and fixing plates 21 are connected to the outer walls of two opposite sides of the undercarriage 2 through bolts, the second airbag 25 is located between the top plate 24 and the fixing plate 21, the second airbag 25 is connected with the top plate 24 in a gluing mode, the unmanned aerial vehicle body 1 can generate large impact force with the ground when landing, the camera 33 can be damaged or offset when being impacted, and accordingly the patrol of the unmanned aerial vehicle body 1 can be affected, therefore, the camera 33 can be protected through the arrangement of the supporting mechanism 3, when the unmanned aerial vehicle body 1 is in contact with the ground when landing, the sliding block 23 can ascend through the self gravity of the unmanned aerial vehicle body 1, the top plate 24 compresses the second airbag 25, gas in the second airbag 25 can be conveyed to the inside of the first airbag 6 through the guide pipe 8 after being compressed, the inside of the first airbag 6 swells due to the input of the gas, so that the first airbag 6 is in contact with the inside of the camera 33, and along with the increase of the gas in the first airbag 6, first gasbag 6 can extrude camera 33 to the extrusion through first gasbag 6 can improve camera 33's stability, prevent because unmanned aerial vehicle body 1 when the whereabouts and the effort between the ground is great, thereby lead to camera 33's stability relatively poor.
In addition, the plurality of vesicles 26 are arranged on the outer wall of the top of the first air bag 6, the vesicles 26 are hemispherical, the vesicles 26 are made of flexible elastic materials, when the gas inside the second air bag 25 is compressed and then delivered into the first air bag 6, the vesicles 26 can be expanded due to the filling of the gas, and when the second air bag 25 is in contact with the camera 33, the vesicles 26 are made of flexible elastic materials, so that the second air bag 25 can cover the bottom of the camera 33 when being expanded, and the stability of the camera 33 can be further improved.
Example 3
Referring to fig. 1, fig. 2, fig. 9 and fig. 10, an unmanned aerial vehicle railway traffic control uses railway crossing gate system based on long-range tour has antifog function, compare with embodiment 1, on embodiment 1's basis, a plurality of sound holes 30 have been seted up to one side outer wall of aviation baffle 27, the shape of sound hole 30 is the toper, when unmanned aerial vehicle body 1 is taking off, when wind-force passes through sound hole 30, because the shape of sound hole 30 is the toper, therefore, wind-force has the coarse thinning, thereby can produce the noise, and then drive away the peripheral flying bird of unmanned aerial vehicle body 1 through the noise, prevent that the flying bird from circling around unmanned aerial vehicle body 1 and causing the influence to taking off of unmanned aerial vehicle body 1.
On the basis of the above, the inner walls of the two opposite sides of the sound hole 30 are connected with the plurality of baffles 31 through bolts, the plurality of whistles 32 are fixed on the outer walls of the baffles 31, the shape of the baffles 31 is blade-shaped, when wind force contacts the blade-shaped baffles 31, noise is generated, so that flying birds can be further repelled, and when the whistles 32 are made to sound through wind force, the repelling effect of the noise on the flying birds can be increased through the matching between the whistles 32 and the baffles 31.
The above description is only for the preferred embodiment of the present invention, but the scope of the present invention is not limited thereto, and any person skilled in the art should be considered to be within the technical scope of the present invention, and the technical solutions and the inventive concepts thereof according to the present invention should be equivalent or changed within the scope of the present invention.
Claims (10)
1. The utility model provides an unmanned aerial vehicle based on long-range tour has antifog function, includes unmanned aerial vehicle body (1) and two undercarriage (2), unmanned aerial vehicle body (1) and two pass through bolted connection between undercarriage (2), two undercarriage (2) are the symmetric distribution on unmanned aerial vehicle body (1), its characterized in that, the bottom outer wall of unmanned aerial vehicle body (1) is provided with fixed establishment (10), the bottom outer wall of fixed establishment (10) is provided with tour mechanism (7), one side of fixed establishment (10) bottom outer wall is provided with antifog mechanism (4), antifog mechanism (4) include sacculus (16) and box (17), glue joint between sacculus (16) and box (17), the inlet port has been seted up to one side outer wall of box (17), one side of unmanned aerial vehicle body (1) bottom outer wall has been seted up, the air pipe (18) is fixedly connected between the heat dissipation holes and the air inlet holes, an air outlet (19) is formed in the outer wall of the bottom of the box body (17), and the air outlet (19) is splayed.
2. The unmanned aerial vehicle with the anti-fog function based on long-distance patrol as claimed in claim 1, wherein the fixing mechanism (10) comprises a first fixing frame (13) and a second fixing frame (14), a first spring (11) is fixedly connected between the first fixing frame (13) and the second fixing frame (14), the first fixing frame (13) and the unmanned aerial vehicle body (1) are connected through bolts, a positioning block (12) is fixedly connected to the outer walls of the two sides of the first fixing frame (13), a positioning slide rail (15) is fixedly connected to the outer walls of the two sides of the second fixing frame (14), and a sliding connection is formed between the positioning slide rail (15) and the positioning block (12).
3. The unmanned aerial vehicle with the anti-fog function based on the remote patrol as claimed in claim 2, wherein the patrol mechanism (7) comprises a support frame (34) and a camera (33), threaded holes are formed in the outer walls of the two sides of the support frame (34), fastening bolts (37) are in threaded connection with the inner walls of the two threaded holes, threaded sleeves (36) are fixedly connected to the outer walls of the two sides of the camera (33), the threaded sleeves (36) are in threaded connection with the fastening bolts (37), and the support frame (34) is in threaded connection with the second fixing frame (14).
4. The unmanned aerial vehicle with the anti-fog function based on the remote patrol as claimed in claim 3, wherein the bottom outer wall of the support frame (34) and the top outer wall of the camera (33) are both fixedly connected with magnets (35), and the magnets (35) attract each other.
5. The unmanned aerial vehicle with the anti-fog function based on the remote tour as claimed in claim 2, wherein an air guide mechanism (9) is arranged on an outer wall of one side of the second fixing frame (14), the air guide mechanism (9) comprises an air guide plate (27) and a top block (28), the air guide plate (27) is connected with the top block (28) through bolts, the air guide plate (27) is connected with the second fixing frame (14) through hinges, a third spring (29) is fixedly connected between the air guide plate (27) and the second fixing frame (14), and the top block (28) is naturally contacted with the balloon (16).
6. The unmanned aerial vehicle with the anti-fog function based on the remote patrol as claimed in claim 1, wherein an overflow block (20) is fixedly connected to an inner wall edge of the air inlet hole, the overflow block (20) is conical, and the overflow block (20) is composed of a plurality of plastic elastic pieces.
7. The unmanned aerial vehicle with the anti-fog function based on the long-distance patrol as claimed in claim 1, wherein the supporting mechanism (3) is arranged on the outer wall of the top of the undercarriage (2), the supporting mechanism (3) comprises a supporting plate (5), a first air bag (6) and a second air bag (25), the supporting plate (5) is connected with the undercarriage (2) through bolts, a guide pipe (8) is arranged between the first air bag (6) and the second air bag (25), the first air bag (6) is bonded with the supporting plate (5), a fixing opening is formed in the outer wall of the bottom of the undercarriage (2), a sliding block (23) is connected to the inner wall of the fixing opening in a sliding manner, the second spring (22) is fixedly connected to both sides of the outer wall of the top of the sliding block (23), and a top plate (24) is fixedly connected to the outer wall of the top of the second spring (22), fixed connection has fixed plate (21) between the relative both sides outer wall of undercarriage (2), second gasbag (25) are located roof (24) with glue between fixed plate (21), second gasbag (25) with glue between roof (24).
8. The unmanned aerial vehicle with the antifog function based on long-range tour of claim 7, characterized in that, the top outer wall of first gasbag (6) is provided with a plurality of vesicles (26), the shape of vesicle (26) is hemispherical.
9. The unmanned aerial vehicle with the anti-fog function based on the remote patrol as claimed in claim 5, wherein a plurality of sound holes (30) are formed in an outer wall of one side of the air deflector (27), and the shape of the sound holes (30) is a cone.
10. The unmanned aerial vehicle with the anti-fog function based on the long-distance patrol as claimed in claim 9, wherein a plurality of baffles (31) are fixedly connected between the inner walls of the two opposite sides of the sound hole (30), a plurality of whistles (32) are fixed on the outer walls of the baffles (31), and the baffles (31) are blade-shaped.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202110916508.6A CN113371217B (en) | 2021-08-11 | 2021-08-11 | Unmanned aerial vehicle with anti-fog function based on remote patrol |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
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