CN211592921U

CN211592921U - Unmanned aerial vehicle with solar charging function

Info

Publication number: CN211592921U
Application number: CN201922337356.5U
Authority: CN
Inventors: 张军山
Original assignee: Lequini Shanghai Intelligent Technology Co ltd
Current assignee: Lequini Shanghai Intelligent Technology Co ltd
Priority date: 2019-12-23
Filing date: 2019-12-23
Publication date: 2020-09-29
Anticipated expiration: 2029-12-23

Abstract

The utility model discloses an unmanned aerial vehicle with solar charging function, including the unmanned aerial vehicle organism, the equal fixedly connected with wing in four corners of unmanned aerial vehicle organism, the center department fixedly connected with support column at unmanned aerial vehicle organism top, the top fixedly connected with solar panel of support column, the top of unmanned aerial vehicle organism and the equal fixedly connected with bracing piece in both sides that is located the support column, solar panel and fixedly connected with convex lens are run through at the top of bracing piece. The utility model discloses a set up fixed block, dead lever, connecting rod, photovoltaic inverter, convex lens, support column, solar panel, bracing piece, strong magnet, movable rod, cylinder, emergent battery, counter weight iron plate and torsional spring cooperation and use, have solar charging and the good advantage of buffering stability, solved current unmanned aerial vehicle and generally adopted the battery to be the driving energy, be unfavorable for lasting development, and buffering stability is relatively poor, the problem of damaging when leading to unmanned aerial vehicle to descend very easily.

Description

Unmanned aerial vehicle with solar charging function

Technical Field

The utility model relates to an unmanned air vehicle technique field specifically is an unmanned aerial vehicle with solar charging function.

Background

The unmanned plane is an unmanned plane for short, and is abbreviated as UAV in English, the unmanned plane is an unmanned plane operated by utilizing a radio remote control device and a self-contained program control device, or is completely or intermittently and autonomously operated by an on-board computer, continuous development and new energy gradually become mainstream along with the progress of science and technology and the development of society, the existing unmanned plane generally adopts a storage battery as driving energy, is not beneficial to continuous development, has poor buffering stability and is easy to cause damage of the unmanned plane during landing.

SUMMERY OF THE UTILITY MODEL

An object of the utility model is to provide an unmanned aerial vehicle with solar charging function possesses solar charging and the good advantage of buffering stability, has solved current unmanned aerial vehicle and has generally adopted the battery for driving energy, is unfavorable for lasting development, and buffering stability is relatively poor, the problem of damaging when leading to unmanned aerial vehicle to descend very easily.

In order to achieve the above object, the utility model provides a following technical scheme: an unmanned aerial vehicle with solar charging function comprises an unmanned aerial vehicle body, wings are fixedly connected to four corners of the unmanned aerial vehicle body, a support column is fixedly connected to the center of the top of the unmanned aerial vehicle body, a solar panel is fixedly connected to the top of the support column, support rods are fixedly connected to the top of the unmanned aerial vehicle body and two sides of the support column, the top of each support rod penetrates through the solar panel and is fixedly connected with a convex lens, a transparent frame body is fixedly connected to the top of the unmanned aerial vehicle body and the outer side of the solar panel, four corners of the transparent frame body are movably connected with a box door through hinges, a photovoltaic inverter is fixedly connected to the front side of the right side of the top of the unmanned aerial vehicle body, an emergency storage battery is fixedly connected to the left rear side of the top of the unmanned, the top of strong magnet is provided with the counter weight iron plate, the equal fixedly connected with fixed block in four corners of unmanned aerial vehicle bottom of the body, vertical one side that two fixed blocks are relative runs through and is provided with the movable rod, both sides all overlap around the movable rod surface are equipped with the torsional spring, both sides all overlap around the movable rod surface are equipped with the connecting rod, the bottom fixedly connected with dead lever of the relative one side of two connecting rods, the surface cover of dead lever is equipped with the cylinder.

Preferably, solar panel is the slope setting, solar panel's top is seted up with the recess that the bracing piece cooperation was used.

Preferably, the center of one side of the box door, which is far away from the transparent frame body, is fixedly connected with a handle, and the surface of the movable rod is movably connected with the joint of the fixed block.

Preferably, one side that the torsional spring is close to the movable rod is connected with the fixed surface of movable rod, one side that the movable rod was kept away from to the torsional spring is connected with the bottom fixed of unmanned aerial vehicle organism.

Preferably, the surface of the fixed rod is movably connected with the inner ring of the roller, the number of the support rods is several, and the connecting rods are arranged in an inclined manner.

Compared with the prior art, the beneficial effects of the utility model are as follows:

1. the utility model discloses a set up fixed block, dead lever, connecting rod, photovoltaic inverter, convex lens, support column, solar panel, bracing piece, strong magnet, movable rod, cylinder, emergent battery, counter weight iron plate and torsional spring cooperation and use, have solar charging and the good advantage of buffering stability, solved current unmanned aerial vehicle and generally adopted the battery to be the driving energy, be unfavorable for lasting development, and buffering stability is relatively poor, the problem of damaging when leading to unmanned aerial vehicle to descend very easily.

2. The utility model discloses a set up the chamber door, can be convenient for maintain and change photovoltaic inverter and counter weight iron plate, use through setting up bracing piece and recess cooperation, can play the effect of stable connection to convex lens, and play spacing effect to solar panel, prevent that solar panel from rocking at will, use through setting up strong magnet and counter weight iron plate cooperation, can play balanced effect, unmanned aerial vehicle's stability has been improved, through setting up the cylinder, can become to slide for the roll, the dead lever of being convenient for removes the extension support, through setting up convex lens, can play the effect of gathering sunshine, the solar panel of being convenient for converts, through setting up emergent battery, can play the effect of power supply when the unexpected outage of unmanned aerial vehicle organism.

Drawings

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

FIG. 2 is a top cross-sectional view of the transparent frame structure of the present invention;

fig. 3 is a left view of the connecting rod structure of the present invention.

In the figure: 1 unmanned aerial vehicle organism, 2 fixed blocks, 3 dead levers, 4 connecting rods, 5 wings, 6 transparent frame, 7 photovoltaic inverter, 8 convex lens, 9 support columns, 10 solar panel, 11 bracing pieces, 12 strong magnets, 13 movable rod, 14 cylinders, 15 emergent batteries, 16 counter weight iron plate, 17 chamber doors, 18 torsional springs.

Detailed Description

The technical solutions in the embodiments of the present invention will be described clearly and completely with reference to the accompanying drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only some embodiments of the present invention, not all embodiments. Based on the embodiments in the present invention, all other embodiments obtained by a person skilled in the art without creative work belong to the protection scope of the present invention.

Referring to fig. 1-3, an unmanned aerial vehicle with solar charging function comprises an unmanned aerial vehicle body 1, wings 5 are fixedly connected to four corners of the unmanned aerial vehicle body 1, a support pillar 9 is fixedly connected to the center of the top of the unmanned aerial vehicle body 1, a solar panel 10 is fixedly connected to the top of the support pillar 9, the solar panel 10 is disposed in an inclined manner, a groove matched with the support pillar 11 is formed in the top of the solar panel 10, support bars 11 are fixedly connected to the top of the unmanned aerial vehicle body 1 and located on two sides of the support pillar 9, the number of the support bars 11 is several, the top of each support bar 11 penetrates through the solar panel 10 and is fixedly connected with a convex lens 8, a transparent frame body 6 is fixedly connected to the top of the unmanned aerial vehicle body 1 and located on the outer side of the solar panel 10, a door 17 is movably connected to four, the front side of the right side of the top of the unmanned aerial vehicle body 1 is fixedly connected with a photovoltaic inverter 7, the rear side of the left side of the top of the unmanned aerial vehicle body 1 is fixedly connected with an emergency storage battery 15, the two sides of the top of the unmanned aerial vehicle body 1 and the inner cavity of the transparent frame body 6 are fixedly connected with a strong magnet 12, the top of the strong magnet 12 is provided with a counterweight iron block 16, the four corners of the bottom of the unmanned aerial vehicle body 1 are fixedly connected with fixed blocks 2, one side of each of the two vertical fixed blocks 2 opposite to each other is provided with a movable rod 13 in a penetrating way, the surface of the movable rod 13 is movably connected with the joint of the fixed blocks 2, the front side and the rear side of the surface of the movable rod 13 are respectively sleeved with a torsion spring 18, one side of each torsion spring 18 close to the movable rod 13 is fixedly connected with the, the bottom of one side of the two connecting rods 4 opposite to each other is fixedly connected with a fixed rod 3, the surface of the fixed rod 3 is sleeved with a roller 14, the surface of the fixed rod 3 is movably connected with the inner ring of the roller 14, the photovoltaic inverter 7 and the counterweight iron block 16 can be maintained and replaced conveniently by arranging a box door 17, the convex lens 8 can be stably connected by arranging a supporting rod 11 and a groove for matching use, the solar panel 10 can be limited to prevent the solar panel 10 from shaking randomly, the strong magnet 12 and the counterweight iron block 16 can be matched for use to play a balancing role, the stability of the unmanned aerial vehicle is improved, the roller 14 can be arranged to change sliding into rolling, the fixed rod 3 can be conveniently moved and expanded to support, the convex lens 8 can play a role of gathering sunlight, the solar panel 10 can be conveniently converted, and the emergency storage battery 15 is arranged, can play the effect of power supply when 1 unexpected outage of unmanned aerial vehicle organism, through setting up fixed block 2, dead lever 3, connecting rod 4, photovoltaic inverter 7, convex lens 8, support column 9, solar panel 10, bracing piece 11, strong magnet 12, movable rod 13, cylinder 14, emergent battery 15, counter weight iron plate 16 and the cooperation of torsional spring 18 are used, the advantage that solar charging and buffering stability are good has been solved, the current unmanned aerial vehicle generally adopts the battery to be the driving energy, be unfavorable for lasting development, and buffering stability is relatively poor, the problem of damaging when leading to unmanned aerial vehicle to descend very easily.

When in use, the box door 17 is opened, the counterweight iron block 16 with proper weight is placed on the strong magnet 12, so that the unmanned aerial vehicle body 1 is in a balanced state, the sunlight irradiates on the convex lens 8, is collected by the convex lens 8 and is radiated to the surface of the solar panel 10, under the action of the solar panel 10, the light energy is converted into the electric energy and stored in the unmanned aerial vehicle body 1, under the action of the photovoltaic inverter 7, the electric energy in the unmanned aerial vehicle body 1 is converted into alternating current electric energy to realize power supply, when the unmanned aerial vehicle body 1 lands, the roller 14 firstly contacts with a landing surface, so that the roller 14 rolls, and because the connecting rod 4 is arranged obliquely in a natural state, so that the roller 14 drives the connecting rod 4 to move outwards, and drives the movable rod 13 to rotate, so that the torsion spring 18 is tightened, under the action of the torsion spring 18, a certain tension is exerted, so that the connecting rod 4 has a force of moving inwards, thereby achieving a good buffering effect.

All kinds of parts used in the application document are standard parts and can be purchased from the market, the specific connection mode of all parts adopts conventional means such as mature bolts, rivets, welding and the like in the prior art, the conventional models in the prior art are adopted for machinery, parts and electrical equipment, the conventional connection mode in the prior art is adopted for circuit connection, and detailed description is not given here.

In summary, the following steps: this unmanned aerial vehicle with solar charging function, through setting up fixed block 2, dead lever 3, connecting rod 4, photovoltaic inverter 7, convex lens 8, support column 9, solar panel 10, bracing piece 11, strong magnet 12, movable rod 13, cylinder 14, emergent battery 15, counter weight iron plate 16 and torsional spring 18 cooperation are used, have solar charging and the good advantage of buffering stability, it generally adopts the battery to be the driving energy to have solved current unmanned aerial vehicle, be unfavorable for lasting development, and buffering stability is relatively poor, lead to the problem of damage when unmanned aerial vehicle descends very easily.

Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that changes, modifications, substitutions and alterations can be made in these embodiments without departing from the principles and spirit of the invention, the scope of which is defined in the appended claims and their equivalents.

Claims

1. The utility model provides an unmanned aerial vehicle with solar charging function, includes unmanned aerial vehicle organism (1), its characterized in that: wings (5) are fixedly connected to four corners of the unmanned aerial vehicle body (1), a support column (9) is fixedly connected to the center of the top of the unmanned aerial vehicle body (1), a solar panel (10) is fixedly connected to the top of the support column (9), support rods (11) are fixedly connected to the top of the unmanned aerial vehicle body (1) and two sides of the support column (9), the top of each support rod (11) penetrates through the solar panel (10) and is fixedly connected with a convex lens (8), a transparent frame body (6) is fixedly connected to the top of the unmanned aerial vehicle body (1) and is positioned on the outer side of the solar panel (10), four corners of the transparent frame body (6) are movably connected with a box door (17) through hinges, a photovoltaic inverter (7) is fixedly connected to the front side of the right side of the top of the unmanned aerial vehicle body (1), and an emergency storage, the utility model discloses an unmanned aerial vehicle, including unmanned aerial vehicle organism (1), the both sides at unmanned aerial vehicle organism (1) top and be located inner chamber fixedly connected with strong magnet (12) of transparent frame body (6), the top of strong magnet (12) is provided with counter weight iron plate (16), the equal fixedly connected with fixed block in four corners (2) of unmanned aerial vehicle organism (1) bottom, vertical two fixed block (2) relative one side is run through and is provided with movable rod (13), both sides all overlap around movable rod (13) surface are equipped with torsional spring (18), both sides all overlap around movable rod (13) surface are equipped with connecting rod (4), the bottom fixedly connected with dead lever (3) of two relative one sides of connecting rod (4), the surface cover of dead lever (3) is equipped.

2. The unmanned aerial vehicle with solar charging function of claim 1, wherein: solar panel (10) are the slope setting, the recess that uses with bracing piece (11) cooperation is seted up at the top of solar panel (10).

3. The unmanned aerial vehicle with solar charging function of claim 1, wherein: the center of one side of the box door (17) far away from the transparent frame body (6) is fixedly connected with a handle, and the surface of the movable rod (13) is movably connected with the joint of the fixed block (2).

4. The unmanned aerial vehicle with solar charging function of claim 1, wherein: one side that torsional spring (18) are close to movable rod (13) is connected with the fixed surface of movable rod (13), one side that movable rod (13) were kept away from in torsional spring (18) and the bottom fixed connection of unmanned aerial vehicle organism (1).

5. The unmanned aerial vehicle with solar charging function of claim 1, wherein: the surface of the fixed rod (3) is movably connected with the inner ring of the roller (14), the number of the support rods (11) is a plurality, and the connecting rods (4) are arranged in an inclined mode.