CN113602502A

CN113602502A - Intelligent unmanned aerial vehicle with heat dissipation function

Info

Publication number: CN113602502A
Application number: CN202110780525.1A
Authority: CN
Inventors: 李政
Original assignee: Individual
Current assignee: Individual
Priority date: 2021-07-09
Filing date: 2021-07-09
Publication date: 2021-11-05

Abstract

The invention belongs to the technical field of unmanned aerial vehicles, and particularly relates to an intelligent unmanned aerial vehicle with a heat dissipation function, which comprises side wings fixedly connected to two ends of two sides of a shell respectively, wherein mounting feet are arranged on one sides of the side wings respectively, driving motors are fixedly connected inside the mounting feet respectively, output shafts of the driving motors penetrate through the top ends of the mounting feet through couplings and are fixedly connected with blades, the top ends of the mounting feet are fixedly connected with protective covers respectively, the protective covers are arranged outside the blades, heat dissipation devices are arranged on the side walls of the mounting feet, each heat dissipation device comprises an air inlet formed in the lower end of the mounting foot, the air inlets are communicated with the insides of the mounting feet, air deflectors are arranged in the air inlets, and fans are arranged on the side walls of the mounting feet; according to the invention, the fan is started to blow air to the shell of the unmanned aerial vehicle, heat is dissipated, part of air blown out by the fan enters the mounting feet through the air deflector to dissipate heat of the driving motor and the blades, the heat dissipation effect is good, and the working time of the unmanned aerial vehicle is prolonged.

Description

Intelligent unmanned aerial vehicle with heat dissipation function

Technical Field

The invention belongs to the technical field of unmanned aerial vehicles, and particularly relates to an intelligent unmanned aerial vehicle with a heat dissipation function.

Background

With the rapid development of economy, the unmanned aerial vehicle for civil use is rapidly developed, the civil unmanned aerial vehicle as one type of the unmanned aerial vehicle is widely applied to the fields of aerial photography of some photography enthusiasts in our lives, and some defects and shortcomings still exist in the using process of some existing intelligent unmanned aerial vehicles.

In the process of implementing the invention, the inventor finds that at least the following problems in the prior art are not solved:

(1) unmanned aerial vehicle is in needs continuous work, but unmanned aerial vehicle's thermal diffusivity is not good, influences unmanned aerial vehicle's continuous operating time, especially the heat in unmanned aerial vehicle's rotor and the unmanned aerial vehicle main part.

(2) The traditional intelligent unmanned aerial vehicle has no measure for conveniently carrying and accommodating the unmanned aerial vehicle in the use process;

(3) the traditional intelligent unmanned aerial vehicle does not have the function of supplementing electric quantity by utilizing solar energy in the using process;

(4) the traditional intelligent unmanned aerial vehicle has no measure for protecting the outside of the unmanned aerial vehicle, which is convenient to mount and dismount;

(5) the traditional intelligent unmanned aerial vehicle has no buffer and anti-collision measures with good use effect on the unmanned aerial vehicle during taking off and landing;

(6) traditional intelligent unmanned aerial vehicle does not have the convenient measure of carrying on article and carrying to hang in the in-process bottom of using.

Disclosure of Invention

Aiming at the problems in the prior art, the invention aims to provide an intelligent unmanned aerial vehicle with a heat dissipation function.

In order to achieve the purpose, the invention adopts the following technical scheme:

an intelligent unmanned aerial vehicle with heat dissipation function includes:

the fan blade comprises a shell, a driving motor, a fan blade blades, a fan blade cover, a fan blade and a heat dissipation device, wherein two ends of two sides of the shell are fixedly connected with side wings respectively;

the heat dissipation device comprises an air inlet arranged at the lower end of the mounting foot, the air inlet is communicated with the inside of the mounting foot, an air deflector is arranged in the air inlet, the air deflector is in clearance fit with the air inlet, the lower end of the side wall of the mounting foot is provided with a side hole communicated with the air inlet, a rotating rod is rotationally arranged in the side hole, one end of the rotating rod penetrates through the air deflector to be rotationally connected with the side wall of the air inlet, the air deflector is fixedly connected with the rotating rod, a side hole is extended from the other end of the rotating rod and is fixedly connected with a turntable, the turntable is provided with a sliding hole, a T-shaped rod is arranged in the sliding hole in a sliding way, the installation foot is provided with a plurality of fixing grooves around the side hole in a circumferential way, t type pole one end extends into in the fixed slot, T type pole cover is equipped with fixed spring, the fixed spring both ends respectively with T type pole and carousel rigid coupling, the fan is installed to the installation foot lateral wall.

Preferably, the fan upper end is provided with the mounting panel, the mounting panel passes through fixing bolt and installation foot lateral wall fixed connection, the fan air outlet is located the installation foot below and towards the shell, the exhaust vent with the inside intercommunication of installation foot is seted up to installation foot lateral wall upper end.

Preferably, an air guide groove is formed in one end, facing the fan, of the air guide plate, and the rotating rod is fixedly connected with the rear end of the air guide plate.

Preferably, a solar structure is arranged inside the top end of one end of the shell, protective structures are respectively arranged at the top end and the bottom end of two sides of the shell, a control module is arranged at the middle position inside the shell, buffer structures are respectively arranged inside two sides of the bottom end of the shell, an installation cavity is fixedly connected to the bottom end inside the shell, batteries are respectively arranged on two sides inside the batteries, hanging structures are respectively arranged on two sides of the middle position of the bottom end of the shell, support frames are respectively arranged at two ends of the bottom end of the shell, an operation panel is fixedly connected to the top end of the shell, and contraction structures are respectively arranged on one side of the side wing;

the retractable structure includes the inner chamber, inner chamber fixed connection is in the inside of flank respectively, one side of flank swing joint has the swivel respectively, the inside of swivel is provided with the telescopic link respectively, one side of telescopic link runs through the outside one side of swivel and extends to the inside one side of inner chamber, one side of telescopic link is fixedly connected with limiting plate respectively, the opposite side of telescopic link respectively with one side fixed connection of installation foot, the outside of telescopic link is provided with the external screw thread respectively, the inside of swivel is provided with respectively with external screw thread matched with internal thread, constitute threaded connection between swivel and the telescopic link respectively.

Preferably, the solar structure comprises draw-in groove, inside groove, installation pole, mounting panel, fixture block, solar panel, fixed plate, first slider and first spout, the installation pole sets up the top in the shell inside, the first slider of fixedly connected with respectively is distinguished to the both sides of installation pole, the one end fixedly connected with mounting panel of installation pole, and the top fixedly connected with solar panel of mounting panel, the outside and the fixedly connected with fixed plate on shell one end top are run through to the one end of mounting panel, and the both sides of fixed plate rear end fixedly connected with fixture block respectively, inside groove fixed connection is on the top of shell one end, the both sides difference fixedly connected with draw-in groove of the inside one end of inside groove.

Preferably, the first sliding blocks are respectively embedded in the first sliding grooves, the outer sizes of the clamping blocks and the fixing plates are respectively smaller than the inner sizes of the clamping grooves and the inner grooves, and clamping structures are formed between the clamping blocks and the fixing plates.

Preferably, protective structure comprises stopper, spacing groove, second spout, second slider and backplate, the backplate sets up the both ends in the shell both sides respectively, the top and the bottom of backplate one side are fixedly connected with stopper respectively, and one side of stopper is fixedly connected with second slider respectively, the spacing groove is fixed connection respectively in the inside of shell top and bottom both sides and the inside of both sides top and bottom, one side of spacing groove is provided with the second spout respectively.

Preferably, the external dimensions of the limiting block and the second sliding block are smaller than the external dimensions of the limiting groove and the second sliding groove, and the limiting block and the second sliding block are in sliding connection with the limiting groove and the second sliding groove respectively.

Preferably, buffer structure comprises compression spring, dog, endotheca, preformed groove, the preformed groove is fixed connection respectively in the inside at shell bottom both ends both sides, one side of the inside bottom of preformed groove is fixedly connected with endotheca respectively, the top of the inside of preformed groove is vertical fixedly connected with compression spring respectively, the inside and the fixedly connected with dog of preformed groove and endotheca are run through respectively to the support frame top, compression spring's bottom respectively with the top fixed connection of dog, the external diameter of dog is less than the internal diameter of preformed groove, compression spring is provided with four groups respectively in the inside of shell bottom both ends both sides, compression spring is the symmetric distribution about the horizontal center line of shell respectively.

Preferably, hang and hold the structure and constitute by snap ring, roll-over stand, logical groove, spacing area, cavity and mount pad, the both sides of mount pad difference fixed connection in shell bottom intermediate position department, the inside difference fixedly connected with cavity of mount pad, one side of the inside bottom of cavity articulates respectively has the roll-over stand, and the inside difference fixedly connected with of roll-over stand leads to the groove, the inside difference fixedly connected with snap ring that leads to the groove, the top difference fixedly connected with spacing area of roll-over stand, the top in spacing area respectively with one side fixed connection inside the cavity, the external dimension of roll-over stand is less than the internal dimension of cavity, the mount pad is symmetric distribution about the perpendicular center line of shell.

Compared with the prior art, the invention has the beneficial effects that: the intelligent unmanned aerial vehicle has the advantages that the good heat dissipation effect on the rotor and the unmanned aerial vehicle main body is realized, the working time of the unmanned aerial vehicle is prolonged, the unmanned aerial vehicle is convenient to carry and store, the electric quantity can be supplemented by solar energy, the external protection on the unmanned aerial vehicle is realized, the buffering and impact resistance of the unmanned aerial vehicle during taking off and landing are realized, the use effect is good, and the convenient carrying and hanging of articles are realized;

(1) pulling the T-shaped rod, moving the T-shaped rod out of the fixed groove, rotating the rotary table, driving the air deflector to rotate, forming the air deflector to form a certain angle according to requirements, loosening the T-shaped rod again, inserting the T-shaped rod into the fixed groove under the action of the fixed spring, fixing the air deflector, starting the fan to blow air to the shell of the unmanned aerial vehicle, dissipating heat, allowing part of air blown out by the fan to enter the installation foot through the air deflector to dissipate heat of the driving motor and the blades, achieving a good heat dissipation effect, prolonging the working time of the unmanned aerial vehicle, and arranging an air guide groove for further increasing the air guide effect;

(2) when the unmanned aerial vehicle is used and is stored and placed after being used, in a contraction structure arranged in the side wing respectively, the swivel connected with one side of the side wing is rotated respectively, the swivel rotates to drive a telescopic rod connected with the inside of the swivel to perform contraction motion in the inner cavity, the mounting foot fixed on one side of the telescopic rod and the blade arranged on the mounting foot are retracted to a distance adaptive to the outer part of the shell to adjust and reduce the wingspan size of the unmanned aerial vehicle, the unmanned aerial vehicle is convenient to carry and store, meanwhile, the wingspan lengths of the unmanned aerial vehicle can be adjusted, and the purposes of facilitating the carrying and the storage of the unmanned aerial vehicle are achieved;

(3) the solar energy structure is arranged to comprise a clamping groove, an inner groove, an installation rod, an installation plate, a clamping block, a solar panel, a fixed plate, a first sliding block and a first sliding groove, the installation plate is pulled out from the inside of the shell by the fixed plate in the solar energy structure arranged inside the top end of one end of the shell in the place where the unmanned aerial vehicle is inconvenient to supplement power supply outdoors, the solar panel on the top end of the installation plate is aligned to the sun for irradiation, the inside of the installation plate reacts for electricity generation, and the battery is supplemented with electricity by the connection between the installation plate and the battery, the installation plate greatly reduces the occupied space and is convenient to take and use by the telescopic design of the first sliding block and the first sliding groove, and the purpose of supplementing electricity by solar energy is achieved;

(4) by arranging the limiting blocks, the limiting grooves, the second sliding blocks and the protective plates, in the process of using the unmanned aerial vehicle, in the protective structures arranged at the top ends of the two sides of the shell, the protective plates are inserted from the limiting grooves in the four corners of one end of the shell and one end of the second sliding groove by utilizing the two groups of limiting blocks on one side and the second sliding blocks fixed on one side of the limiting blocks, the four groups of protective plates are fixed at the top ends and the bottom ends of the two sides of the shell, the outer part of the shell is protected in the using process of the shell, the integrity of the main body structure of the shell is protected, meanwhile, the installation, the disassembly and the use are convenient, and the purpose of conveniently installing and disassembling the outer protection of the unmanned aerial vehicle is achieved;

(5) through being provided with compression spring, the dog, the endotheca, the preformed groove, at unmanned aerial vehicle at the in-process of taking off and land, need frequently to support with the support frame of bottom, the shell has certain weight when taking off and land, bottom sprag frame can take shell direct impact ground, in the buffer structure of the inside setting of shell bottom, unmanned aerial vehicle is at the in-process of taking off and land, when the shell falls to the ground bottom sprag frame and contacts ground, the top of support frame can stretch to the inside of the inside preformed groove of shell, cushion with the impact on ground when going up and down with the shell through the totally four compression springs on the inside top of preformed groove, reduce the inside structural damage of unmanned aerial vehicle body shell, it is better to bottom buffering effect at the in-process of taking off and land, reached the better buffering crashproof to unmanned aerial vehicle when taking off and land of result of use.

(6) Through being provided with the snap ring, the roll-over stand, lead to the groove, spacing area, cavity and mount pad, carry out article with unmanned aerial vehicle when hanging to hold hanging in the hanging of the both sides setting of shell bottom intermediate position department holding structure, through respectively through articulating the inside at the cavity with the roll-over stand, pull out the back from the inside of cavity, the fixed spacing area in roll-over stand top can carry on spacingly to the pull-out position of roll-over stand, pull out the back with the roll-over stand, can be through hanging article and put in the inside snap ring of snap ring, can open the roll-over stand of one side wantonly according to actual demand and carry on article and hang and hold, convenience and practicality, reached the bottom and used convenient purpose of hanging to carrying of article and holding.

Additional features and advantages of the invention will be set forth in the detailed description which follows.

Drawings

FIG. 1 is a schematic front sectional view of the present invention;

FIG. 2 is a schematic top view of a partial structure of the present invention;

FIG. 3 is an enlarged elevational view, partially in section, of the collapsible structure of the present invention;

FIG. 4 is a schematic top view of an enlarged partial cross-sectional structure of the solar cell structure of the present invention;

FIG. 5 is an enlarged partial cross-sectional view taken at A in FIG. 1 according to the present invention;

FIG. 6 is an enlarged front view of a partial cross-section of the buffer structure of the present invention;

fig. 7 is an enlarged partial sectional view of the hanging structure of the present invention.

Fig. 8 is an enlarged side view of the heat sink according to the present invention.

FIG. 9 is an enlarged schematic view of position B of FIG. 1;

fig. 10 is a side view of the enlarged distribution structure of the fixing groove of the present invention.

The reference numbers in the figures illustrate: 1. a drive motor; 2. mounting a foot; 3. a blade; 4. a protective cover; 5. a side wing; 6. a solar structure; 601. a card slot; 602. an inner tank; 603. mounting a rod; 604. mounting a plate; 605. a clamping block; 606. a solar panel; 607. a fixing plate; 608. a first slider; 609. a first chute; 7. a control module; 8. a protective structure; 801. a limiting block; 802. a limiting groove; 803. a second chute; 804. a second slider; 805. a guard plate; 9. a buffer structure; 901. a compression spring; 902. a stopper; 903. an inner sleeve; 904. reserving a groove; 10. a mounting cavity; 11. a battery; 12. a hanging structure; 1201. a snap ring; 1202. a roll-over stand; 1203. a through groove; 1204. a limiting band; 1205. a cavity; 1206. a mounting seat; 13. a support frame; 14. a housing; 15. an operation panel; 16. an inner cavity; 17. a limiting plate; 18. rotating the ring; 19. a telescopic rod; 20. an air inlet; 21. a rotating rod; 22. an air deflector; 23. a T-shaped rod; 2301. a slide hole; 24. fixing the spring; 25. a side hole; 26. fixing grooves; 27. a wind guide groove; 28. a fan; 29. mounting a plate; 30. an air outlet; 31. a turntable.

Detailed Description

In order to make the technical means, the creation characteristics, the achievement purposes and the effects of the invention easy to understand, the invention is further clarified by combining the specific drawings.

It will be understood that when an element is referred to as being "secured to" another element, it can be directly on the other element or intervening elements may also be present. When an element is referred to as being "connected" to another element, it can be directly connected to the other element or intervening elements may also be present. The terms "vertical," "horizontal," "left," "right," and the like as used herein are for illustrative purposes only and do not denote a unique embodiment.

Unless defined otherwise, all technical and scientific terms used herein have the same meaning as commonly understood by one of ordinary skill in the art to which this invention belongs. The terminology used herein in the description of the invention is for the purpose of describing particular embodiments only and is not intended to be limiting of the invention. As used herein, the term "and/or" includes any and all combinations of one or more of the associated listed items.

Example 1: referring to fig. 1-7, the invention provides an intelligent unmanned aerial vehicle with a heat dissipation function, which comprises a housing 14, wherein two ends of two sides of the housing 14 are respectively and fixedly connected with a side wing 5, one side of each side wing 5 is respectively provided with a mounting foot 2, the interior of each mounting foot 2 is respectively and fixedly connected with a driving motor 1, the model of each driving motor 1 can be X2220, an output shaft of each driving motor 1 penetrates through the top end of each mounting foot 2 through a coupler and is fixedly connected with a blade 3, the top ends of the mounting feet 2 are respectively and fixedly connected with a protective cover 4, the protective covers 4 are arranged outside the blades 3, and the side walls of the mounting feet 2 are provided with heat dissipation devices;

the heat dissipation device comprises an air inlet 20 formed in the lower end of a mounting foot 2, the air inlet 20 is communicated with the inside of the mounting foot 2, an air deflector 22 is arranged in the air inlet 20, the air deflector 22 is in clearance fit with the air inlet 20, a side hole 25 communicated with the air inlet 20 is formed in the lower end of the side wall of the mounting foot 2, a rotating rod 21 is rotatably arranged in the side hole 20, one end of the rotating rod 21 penetrates through the air deflector 22 and is rotatably connected with the side wall of the air inlet 20, the air deflector 22 is fixedly connected with the rotating rod 21, a rotating disk 31 is fixedly connected with the side hole 21 and extends out of the other end of the rotating rod 21, a sliding hole 2301 is formed in the rotating disk 31, a T-shaped rod 23 is slidably arranged in the sliding hole 2301, a plurality of fixing grooves 26 are formed in the periphery of the mounting foot 2 around the side hole 25, one end of the T-shaped rod 23 extends into the fixing grooves 26, and a fixing spring 24 is sleeved on the T-shaped rod 23, two ends of the fixed spring 24 are fixedly connected with the T-shaped rod 23 and the rotary table 31 respectively, and the side wall of the mounting leg 2 is provided with a fan 28;

further, for the ease of installation change fan 28, fan 28 upper end is provided with mounting panel 29, mounting panel 29 passes through fixing bolt and 2 lateral wall fixed connection of installation foot, for improving the radiating effect, fan 28 air outlet is located 2 below of installation foot and towards

shell

14, 2 lateral wall upper ends of installation foot offer with the inside exhaust vent 30 that communicates of installation foot 2.

An air guide groove 27 is formed in one end, facing the fan 28, of the air guide plate 22, and the rotating rod 21 is fixedly connected with the rear side end of the air guide plate 22.

Concretely, pulling T type pole 23, make T type pole 23 shift out from fixed slot 26, rotate carousel 31, drive aviation baffle 22 and rotate, and form according to the requirement and make aviation baffle 22 form certain angle, loosen T type pole 23 again, under the effect of fixed spring 24, T type pole 23 inserts in fixed slot 26, it is fixed with aviation baffle 22, start fan 28 bloies unmanned aerial vehicle shell 14, the heat dissipation, some wind that fan 28 blew off gets into installation foot 2 inside through aviation baffle 22 and dispels the heat to driving motor 1 and blade 3, the radiating effect is good, increase unmanned aerial vehicle operating time, in order to further increase wind-guiding effect, set up guide slot 27.

Example 2: referring to fig. 1 and 7, on the basis of embodiment 1, a solar structure 6 is disposed inside the top end of one end of a housing 14, protective structures 8 are respectively disposed on the top end and the bottom end of two sides of the housing 14, a control module 7 is disposed in the middle position of the inside of the housing 14, buffer structures 9 are respectively disposed inside two sides of the bottom end of the housing 14, a mounting cavity 10 is fixedly connected to the bottom end of the inside of the housing 14, batteries 11 are respectively disposed on two sides of the inside of the batteries 11, hanging structures 12 are respectively disposed on two sides of the middle position of the bottom end of the housing 14, support frames 13 are respectively disposed at two ends of the bottom end of the housing 14, an operating panel 15 is fixedly connected to the top end of the housing 14, and a contraction structure is respectively disposed on one side of a side wing 5;

the contraction structure comprises an inner cavity 16, the inner cavity 16 is fixedly connected with the inner parts of the side wings 5 respectively, one side of each side wing 5 is movably connected with a rotating ring 18 respectively, telescopic rods 19 are arranged in the rotating rings 18 respectively, one side of each telescopic rod 19 penetrates through one side of the outer part of each rotating ring 18 and extends to one side of the inner part of each inner cavity 16, one side of each telescopic rod 19 is fixedly connected with a limiting plate 17 respectively, and the other side of each telescopic rod 19 is fixedly connected with one side of each mounting foot 2 respectively;

the outer part of the telescopic rod 19 is respectively provided with an external thread, the inner part of the rotating ring 18 is respectively provided with an internal thread matched with the external thread, and the rotating ring 18 and the telescopic rod 19 are respectively in threaded connection;

specifically, as shown in fig. 1 and fig. 3, unmanned aerial vehicle is at the in-process that uses, when accomodating after the use and placing, respectively in the inside contraction structure who sets up of flank 5, through rotating 5 one side swing joint's swivel 18 respectively, swivel 18 rotates and drives inside telescopic link 19 with it threaded connection and carries out the shrink motion in the inside of inner chamber 16, with the blade 3 that sets up on 19 one side fixed installation foot 2 of telescopic link and the installation foot 2, it adjusts the back that diminishes with the outside adapted distance of shell 14 with unmanned aerial vehicle's span size to retrieve, be convenient for carry unmanned aerial vehicle and also be convenient for accomodate it, also can adjust each span length of unmanned aerial vehicle simultaneously, reached the mesh of being convenient for accomodate when being convenient for unmanned aerial vehicle's carrying.

Example 3: the mounting rod 603 is arranged at the top end of the inside of the outer shell 14, two sides of the mounting rod 603 are respectively and fixedly connected with a first sliding block 608, one end of the mounting rod 603 is fixedly connected with a mounting plate 604, the top end of the mounting plate 604 is fixedly connected with a solar panel 606, one end of the mounting plate 604 penetrates through the outside of the top end of the one end of the outer shell 14 and is fixedly connected with a fixing plate 607, two sides of the rear end of the fixing plate 607 are respectively and fixedly connected with a clamping block 605, the inner groove 602 is fixedly connected at the top end of the one end of the outer shell 14, and two sides of one end of the inside of the inner groove 602 are respectively and fixedly connected with a clamping groove 601;

the first sliding blocks 608 are respectively embedded in the first sliding grooves 609, the external dimensions of the fixture block 605 and the fixing plate 607 are respectively smaller than the internal dimensions of the clamping groove 601 and the internal groove 602, and a clamping structure is formed between the fixture block 605 and the fixing plate 607;

specifically, as shown in fig. 1 and 4, through the place that is not convenient for carry out supplementary power to unmanned aerial vehicle in the open air, utilize the fixed plate 607 to pull out the mounting panel 604 from the inside of shell 14 in the inside solar energy structure 6 that sets up in shell 14 one end top, aim at solar radiation with the solar panel 606 on mounting panel 604 top, the internal reaction generates electricity, and supply electric quantity to battery 11 through the connection with between the battery 11, the mounting panel 604 passes through the flexible design of first slider 608 and first spout 609, the occupation space that has significantly reduced, it is convenient to take, reached and to utilize solar energy to carry out the purpose of supplying electric quantity.

Example 4: the protective structure 8 is composed of a limiting block 801, a limiting groove 802, a second sliding groove 803, a second sliding block 804 and a protecting plate 805, the protecting plate 805 is respectively arranged at two ends of two sides of the shell 14, the limiting block 801 is respectively and fixedly connected to the top end and the bottom end of one side of the protecting plate 805, the second sliding block 804 is respectively and fixedly connected to one side of the limiting block 801, the limiting groove 802 is respectively and fixedly connected to the inside of two sides of the top end and the bottom end of the shell 14 and the inside of the top end and the bottom end of two sides, and the second sliding groove 803 is respectively arranged at one side of the limiting groove 802;

the external dimensions of the limiting block 801 and the second sliding block 804 are smaller than the external dimensions of the limiting groove 802 and the second sliding groove 803, and the limiting block 801 and the second sliding block 804 are in sliding connection with the limiting groove 802 and the second sliding groove 803 respectively;

specifically, as shown in fig. 1 and 5, at the in-process that unmanned aerial vehicle is using, in protective structure 8 that shell 14 both sides top set up, utilize two sets of stopper 801 and the fixed second slider 804 of stopper 801 one side of backplate 805, insert from the one end of the inside spacing groove 802 of four corners of shell 14 one end and second spout 803, fix four sets of backplate 805 at the top and the bottom of shell 14 both sides, the in-process that shell 14 used carries out outside protection to the outside of shell 14, the integrality of shell 14 major structure has been protected, convenient to use is dismantled in the installation simultaneously, reached the convenient outside protection purpose to unmanned aerial vehicle of installation dismantlement.

Example 5: the buffer structure 9 is composed of a compression spring 901, a stop block 902, an inner sleeve 903 and a preformed groove 904, the preformed groove 904 is fixedly connected to the inner parts of two sides of the two ends of the bottom end of the outer shell 14 respectively, the inner sleeve 903 is fixedly connected to one side of the bottom end of the inner part of the preformed groove 904 respectively, the compression spring 901 is vertically and fixedly connected to the top end of the inner part of the preformed groove 904 respectively, the top end of the support frame 13 penetrates through the inner parts of the preformed groove 904 and the inner sleeve 903 respectively and is fixedly connected with the stop block 902, and the bottom end of the compression spring 901 is fixedly connected to the top end of the stop block 902 respectively; (ii) a

The outer diameter of the stop 902 is smaller than the inner diameter of the preformed groove 904, four groups of compression springs 901 are respectively arranged in the two sides of the two ends of the bottom end of the shell 14, and the compression springs 901 are respectively distributed symmetrically about the horizontal center line of the shell 14;

specifically, as shown in fig. 1 and fig. 6, at unmanned aerial vehicle in the in-process of taking off and landing, need frequently to use the support frame 13 of bottom to support, shell 14 has certain weight when taking off and landing, bottom support frame 13 can take shell 14 direct impact ground, in the inside buffer structure 9 that sets up in shell 14 bottom, unmanned aerial vehicle is at the in-process of taking off and landing, when shell 14 falls to ground bottom support frame 13 and contacts ground, the top of support frame 13 can stretch to the inside of the inside preformed groove 904 of shell 14, cushion with the impact on ground when lifting shell 14 through the total four group compression spring 901 on the inside top of preformed groove 904, reduce the structural damage to the inside of unmanned aerial vehicle main part shell 14, it is better to bottom buffering effect at the in-process of taking off and landing, the better buffering crashproof of unmanned aerial vehicle when taking off and landing of result of use has been reached.

Example 6: the hanging structure 12 comprises a clamping ring 1201, a turning frame 1202, through grooves 1203, limiting belts 1204, cavities 1205 and mounting seats 1206, the mounting seats 1206 are respectively and fixedly connected to two sides of the middle position of the bottom end of the shell 14, the cavities 1205 are respectively and fixedly connected to the inside of the mounting seats 1206, the turning frame 1202 is hinged to one side of the bottom end of the inside of the cavities 1205, the through grooves 1203 are respectively and fixedly connected to the inside of the turning frame 1202, the clamping rings 1201 are respectively and fixedly connected to the inside of the through grooves 1203, the limiting belts 1204 are respectively and fixedly connected to the top ends of the turning frame 1202, and the top ends of the limiting belts 1204 are respectively and fixedly connected to one side of the inside of the cavities 1205;

the external dimensions of the roll-over stand 1202 are smaller than the internal dimensions of the cavity 1205, and the mounts 1206 are symmetrically distributed about the vertical centerline of the housing 14;

specifically, as shown in fig. 1 and 7, in need using unmanned aerial vehicle to carry out article and carry the hanging structure 12 that sets up in the both sides of shell 14 bottom intermediate position department when hanging, through respectively through articulating the inside at cavity 1205 with roll-over stand 1202, after pulling out from the inside of cavity 1205, the fixed spacing area 1204 in roll-over stand 1202 top can carry on spacingly to the pull-out position of roll-over stand 1202, after pulling out roll-over stand 1202, can be through hanging article in the inside snap ring 1201 of snap ring 1201, can carry out article and carry and hang according to the roll-over stand 1202 that actual demand opened one side wantonly, convenient and practical, reached the bottom and used convenient purpose of hanging carrying to article.

The working principle is as follows: in the invention, before use, the T-shaped rod 23 is pulled to move the T-shaped rod 23 out of the fixed groove 26, the rotary disc 31 is rotated to drive the air deflector 22 to rotate, the air deflector 22 forms a certain angle according to requirements, then the T-shaped rod 23 is loosened, under the action of the fixed spring 24, the T-shaped rod 23 is inserted into the fixed groove 26 to fix the air deflector 22, the fan 28 is started to blow air to the shell 14 of the unmanned aerial vehicle, and heat is dissipated, when the unmanned aerial vehicle is used, firstly, in the process of use, when the unmanned aerial vehicle is stored and placed, in the contraction structure arranged in the side wing 5, the rotary ring 18 movably connected with one side of the side 5 is rotated respectively, the rotary ring 18 rotates to drive the telescopic rod 19 connected with the inside in a thread to perform contraction movement in the inner cavity 16, the installation foot 2 fixed on one side of the telescopic rod 19 and the blade 3 arranged on the installation foot 2 are contracted to the distance suitable for the outer part of the shell 14 to adjust the wingspan size of the unmanned aerial vehicle, be convenient for carry unmanned aerial vehicle and also be convenient for accomodate it, also can adjust each span length of unmanned aerial vehicle simultaneously, reached the unmanned aerial vehicle of being convenient for carry the purpose of being convenient for accomodate simultaneously.

Then, through the place that is not convenient for carry out supplementary power to unmanned aerial vehicle in the open air, utilize the fixed plate 607 to pull out the mounting panel 604 from the inside of shell 14 in the inside solar energy structure 6 that sets up in shell 14 one end top, aim at solar radiation with the solar panel 606 on mounting panel 604 top, the electricity is given birth to in the internal reaction, and supply electric quantity to battery 11 through the connection with between the battery 11, the mounting panel 604 is through the flexible design of first slider 608 and first spout 609, the occupation space that has significantly reduced, it is convenient to take, reached and to have utilized solar energy to carry out the purpose of supplying electric quantity.

Secondly, at unmanned aerial vehicle in the in-process that uses, in the protective structure 8 that sets up on shell 14 both sides top, utilize two sets of stopper 801 and the fixed second slider 804 of stopper 801 one side of backplate 805, insert from the one end of the inside spacing groove 802 of four corners of shell 14 one end and second spout 803, fix the top and the bottom at shell 14 both sides with four groups of backplate 805, the outside protection is carried out to shell 14's outside at the in-process that shell 14 used, the integrality of 14 major structure of shell has been protected, convenient to use is dismantled in the installation simultaneously, reached the installation and dismantled convenient outside protection purpose to unmanned aerial vehicle.

Afterwards, at unmanned aerial vehicle at the in-process of taking off and land, need frequently to use the support frame 13 of bottom to support, shell 14 has certain weight when taking off and land, bottom support frame 13 can take shell 14 direct impact ground, in the inside buffer structure 9 that sets up in shell 14 bottom, unmanned aerial vehicle is at the in-process of taking off and land, shell 14 ground bottom support frame 13 contacts when ground, the top of support frame 13 can stretch to the inside of the inside reservation groove 904 of shell 14, buffer with the impact on ground when lifting shell 14 through the total four compression spring groups 901 on the inside top of reservation groove 904, reduce the structural damage to unmanned aerial vehicle main part shell 14 inside, it is better to bottom buffering effect at the in-process of taking off and land, the better buffering crashproof when taking off and land to unmanned aerial vehicle of result of use has been reached.

Finally, in need carry article with unmanned aerial vehicle and hang hanging holding structure 12 that sets up in the both sides of shell 14 bottom intermediate position department when holding, through with roll-over stand 1202 respectively through articulating the inside at cavity 1205, after pulling out from the inside of cavity 1205, the fixed spacing area 1204 in roll-over stand 1202 top can carry on spacingly to the pull-out position of roll-over stand 1202, after pulling out roll-over stand 1202, can carry out article carrying hanging holding through hanging article in the inside snap ring 1201 of snap ring 1201, can open the roll-over stand 1202 of one side wantonly according to actual demand, convenient and practical, the convenient mesh of hanging holding carrying article of bottom use has been reached.

The foregoing shows and describes the general principles, essential features, and inventive features of this invention. It will be understood by those skilled in the art that the present invention is not limited to the embodiments described above, which are described in the specification and illustrated only to illustrate the principle of the present invention, but that various changes and modifications may be made therein without departing from the spirit and scope of the present invention, which fall within the scope of the invention as claimed. The scope of the invention is defined by the appended claims and equivalents thereof.

Claims

1. The utility model provides an intelligent unmanned aerial vehicle with heat dissipation function which characterized in that includes:

two ends of two sides of the shell (14) are fixedly connected with side wings (5) respectively, one side of each side wing (5) is provided with a mounting foot (2), the interior of each mounting foot (2) is fixedly connected with a driving motor (1) respectively, an output shaft of each driving motor (1) penetrates through the top end of each mounting foot (2) through a coupling and is fixedly connected with a blade (3), the top ends of the mounting feet (2) are fixedly connected with protective covers (4) respectively, the protective covers (4) are arranged outside the blades (3), and the side walls of the mounting feet (2) are provided with heat dissipation devices;

the heat dissipation device comprises an air inlet (20) formed in the lower end of a mounting foot (2), the air inlet (20) is communicated with the inside of the mounting foot (2), an air deflector (22) is arranged in the air inlet (20), the air deflector (22) is in clearance fit with the air inlet (20), a side hole (25) communicated with the air inlet (20) is formed in the lower end of the side wall of the mounting foot (2), a rotating rod (21) is rotatably arranged in the side hole (20), one end of the rotating rod (21) penetrates through the air deflector (22) to be rotatably connected with the side wall of the air inlet (20), the air deflector (22) is fixedly connected with the rotating rod (21), a turntable (31) is fixedly connected with the other end of the rotating rod (21) in a manner of extending out of the side hole (21), a sliding hole (2301) is formed in the turntable (31), a T-shaped rod (23) is slidably arranged in the sliding hole (2301), and a plurality of fixing grooves (26) are formed in the periphery of the mounting foot (2) around the side hole (25), t type pole (23) one end extends into in fixed slot (26), T type pole (23) cover is equipped with fixed spring (24), fixed spring (24) both ends respectively with T type pole (23) and carousel (31) rigid coupling, fan (28) are installed to installation foot (2) lateral wall.

2. The intelligent unmanned aerial vehicle with the heat dissipation function of claim 1, characterized in that, fan (28) upper end is provided with mounting panel (29), mounting panel (29) pass through fixing bolt and installation foot (2) lateral wall fixed connection, fan (28) air outlet is located installation foot (2) below and towards shell (14), exhaust vent (30) with the inside intercommunication of installation foot (2) are seted up to installation foot (2) lateral wall upper end.

3. The intelligent unmanned aerial vehicle with the heat dissipation function as claimed in claim 1, wherein an air guide groove (27) is formed in one end, facing the fan (28), of the air deflector (22), and the rotating rod (21) is fixedly connected with the rear end of the air deflector (22).

4. The intelligent unmanned aerial vehicle with the heat dissipation function according to claim 1, wherein a solar structure (6) is arranged inside the top end of one end of the housing (14), protective structures (8) are respectively arranged at the top end and the bottom end of two sides of the housing (14), a control module (7) is arranged in the middle position inside the housing (14), buffer structures (9) are respectively arranged inside two sides of the bottom end of the housing (14), a mounting cavity (10) is fixedly connected to the bottom end inside the housing (14), batteries (11) are respectively arranged on two sides inside the batteries (11), hanging structures (12) are respectively arranged on two sides of the middle position of the bottom end of the housing (14), supporting frames (13) are respectively arranged at two ends of the bottom end of the housing (14), and an operation panel (15) is fixedly connected to the top end of the housing (14), one side of each side wing (5) is provided with a contraction structure;

the retractable structure includes inner chamber (16), inner chamber (16) is fixed connection in the inside of flank (5) respectively, one side difference swing joint of flank (5) has swivel (18), the inside of swivel (18) is provided with telescopic link (19) respectively, one side of telescopic link (19) runs through swivel (18) outside one side and extends to the inside one side of inner chamber (16), one side difference fixedly connected with limiting plate (17) of telescopic link (19), the opposite side of telescopic link (19) respectively with one side fixed connection of installation foot (2), the outside of telescopic link (19) is provided with the external screw thread respectively, the inside of swivel (18) is provided with respectively with external screw thread matched with internal thread, constitute threaded connection between swivel (18) and telescopic link (19) respectively.

5. The intelligent unmanned aerial vehicle with the heat dissipation function according to claim 4, wherein the solar structure (6) is composed of a clamping groove (601), an inner groove (602), a mounting rod (603), a mounting plate (604), a clamping block (605), a solar panel (606), a fixing plate (607), a first sliding block (608) and a first sliding groove (609), the mounting rod (603) is arranged at the top end inside the housing (14), the first sliding block (608) is fixedly connected to two sides of the mounting rod (603), the mounting plate (604) is fixedly connected to one end of the mounting rod (603), the solar panel (606) is fixedly connected to the top end of the mounting plate (604), one end of the mounting plate (604) penetrates through the outside of the top end of one end of the housing (14) and is fixedly connected to the fixing plate (607), and the clamping block (605) is fixedly connected to two sides of the rear end of the fixing plate (607), the inner groove (602) is fixedly connected to the top end of one end of the shell (14), and clamping grooves (601) are fixedly connected to two sides of one end of the inner part of the inner groove (602) respectively.

6. The intelligent unmanned aerial vehicle with the heat dissipation function as claimed in claim 5, wherein the first sliding blocks (608) are respectively embedded inside the first sliding grooves (609), the outer dimensions of the clamping blocks (605) and the fixing plates (607) are respectively smaller than the inner dimensions of the clamping grooves (601) and the inner grooves (602), and the clamping structures are formed between the clamping blocks (605) and the fixing plates (607).

7. The intelligent unmanned aerial vehicle with the heat dissipation function according to claim 4, wherein the protection structure (8) is composed of a limiting block (801), a limiting groove (802), a second sliding groove (803), a second sliding block (804) and a protecting plate (805), the protecting plate (805) is respectively arranged at two ends of two sides of the housing (14), the limiting block (801) is fixedly connected to the top end and the bottom end of one side of the protecting plate (805) respectively, the second sliding block (804) is fixedly connected to one side of the limiting block (801) respectively, the limiting groove (802) is fixedly connected to the inside of two sides of the top end and the bottom end of the housing (14) respectively and the inside of the top end and the bottom end of the two sides respectively, and the second sliding groove (803) is respectively arranged at one side of the limiting groove (802).

8. The intelligent unmanned aerial vehicle with the heat dissipation function as claimed in claim 7, wherein the external dimensions of the limiting block (801) and the second slider (804) are smaller than the external dimensions of the limiting groove (802) and the second sliding groove (803), and sliding connections are respectively formed between the limiting block (801) and the second slider (804) and the limiting groove (802) and the second sliding groove (803).

9. The intelligent unmanned aerial vehicle with the heat dissipation function as claimed in claim 4, wherein the buffer structure (9) is composed of a compression spring (901), a stopper (902), an inner sleeve (903) and a preformed groove (904), the preformed groove (904) is fixedly connected to the inside of two sides of two ends of the bottom end of the housing (14) respectively, the inner sleeve (903) is fixedly connected to one side of the bottom end of the inside of the preformed groove (904) respectively, the compression spring (901) is vertically and fixedly connected to the top end of the inside of the preformed groove (904), the stopper (902) is fixedly connected to the top end of the support frame (13) and penetrates through the inside of the preformed groove (904) and the inner sleeve (903) respectively, and the bottom end of the compression spring (901) is fixedly connected to the top end of the stopper (902) respectively.

10. The intelligent unmanned aerial vehicle with heat dissipation function of claim 4, the hanging structure (12) consists of a clamping ring (1201), a turning frame (1202), a through groove (1203), a limiting belt (1204), a cavity (1205) and a mounting seat (1206), the mounting seats (1206) are respectively and fixedly connected with two sides of the middle position of the bottom end of the shell (14), cavities (1205) are respectively and fixedly connected in the mounting base (1206), a turning frame (1202) is respectively hinged on one side of the bottom end in the cavity (1205), and the interior of the roll-over stand (1202) is respectively and fixedly connected with a through groove (1203), the interior of the through groove (1203) is respectively and fixedly connected with a snap ring (1201), the top ends of the roll-over stands (1202) are respectively fixedly connected with limit belts (1204), the top end of the limiting belt (1204) is fixedly connected with one side of the interior of the cavity (1205) respectively.