CN216943549U

CN216943549U - Novel solar unmanned aerial vehicle

Info

Publication number: CN216943549U
Application number: CN202220206464.8U
Authority: CN
Inventors: 纪雷; 李青海; 田凯; 陈勇刚
Original assignee: Xi'an Yalong Aviation Electromechanical Co ltd
Current assignee: Xi'an Yalong Aviation Electromechanical Co ltd
Priority date: 2022-01-25
Filing date: 2022-01-25
Publication date: 2022-07-12
Anticipated expiration: 2032-01-25

Abstract

The utility model discloses a novel solar unmanned aerial vehicle, which comprises an unmanned aerial vehicle, wherein the upper end of the unmanned aerial vehicle is fixedly connected with a steering mechanism, the upper end of the steering mechanism is fixedly connected with an adjusting mechanism, the upper end of the adjusting mechanism is rotatably connected with a solar mechanism, the steering mechanism comprises an installation box, the upper end of the installation box is arranged in an open manner, and the novel solar unmanned aerial vehicle has the beneficial effects that: conveniently drive the steering panel through setting up step motor and rotate to stably drive the U-shaped board and rotate under the sliding action of ring channel and slide bar, thereby can adjust the orientation of solar energy conversion board, and drive the threaded rod through setting up driving motor and rotate, the threaded rod drives the thread bush and removes under the slip limiting displacement of slide and spout, it slides at the inside sliding groove portion to drive the slider under the rotational action of connecting rod when the thread bush removes, thereby can be under the rotational action of pivot the angle of stable regulation solar energy conversion board.

Description

Novel solar unmanned aerial vehicle

Technical Field

The utility model relates to the technical field of unmanned aerial vehicles, in particular to a novel solar unmanned aerial vehicle.

Background

The unmanned plane is called unmanned plane for short, and is an unmanned plane operated by radio remote control equipment and a self-contained program control device. The unmanned aerial vehicle is a general term of an unmanned aerial vehicle, and can be defined as follows from the technical point of view: unmanned helicopters, unmanned fixed wing aircraft, unmanned multi-rotor aircraft, unmanned airships, and unmanned parawing aircraft.

Present unmanned aerial vehicle all continues a journey through the battery, can increase solar panel in order to increase duration and continue a journey, but the solar panel of installation can not turn to, can only towards a direction, and present unmanned aerial vehicle solar panel board is only an angle after the installation finishes in addition, can not remove and change the angle according to the sun, and solar energy utilization is rateed lowly.

SUMMERY OF THE UTILITY MODEL

The utility model aims to provide a novel solar unmanned aerial vehicle to solve the problems in the background technology.

In order to achieve the purpose, the utility model provides the following technical scheme: a novel solar unmanned aerial vehicle comprises an unmanned aerial vehicle, wherein the upper end of the unmanned aerial vehicle is fixedly connected with a steering mechanism, the upper end of the steering mechanism is fixedly connected with an adjusting mechanism, and the upper end of the adjusting mechanism is rotatably connected with a solar mechanism;

steering mechanism includes that an upper end is the install bin that the opening form set up, install bin fixed connection is in unmanned aerial vehicle upper end, just an annular channel has been seted up to the tank wall in the install bin bottom, step motor of install bin bottom center department fixedly connected with, a steering panel of step motor output fixedly connected with.

Preferably, adjustment mechanism includes a U-shaped plate, U-shaped plate high connection is at the steering wheel upper surface, a spout has been seted up to U-shaped plate bottom, just driving motor of U-shaped plate one side fixedly connected with, a threaded rod of driving motor output fixedly connected with, threaded rod pole wall threaded connection has a thread bush, slide of thread bush lower extreme fixedly connected with, slide sliding connection is in the spout.

Preferably, solar energy mechanism includes a pivot, the pivot is rotated and is connected in U-shaped board upper end one side, just the pivot upper end is rotated and is connected with an regulating plate, solar energy change-over panel of regulating plate upper end fixedly connected with, a sliding tray has been seted up to the regulating plate lower extreme, sliding connection has a dysmorphism slider in the sliding tray, dysmorphism slider and thread bush rotate jointly and are connected with a connecting rod.

Preferably, two sliding rods are fixedly connected to two sides of the lower surface of the steering plate, and the lower ends of the two sliding rods extend to the annular groove and are connected in the annular groove in a sliding mode.

Preferably, two support plates are fixedly connected to two sides of the lower surface of the unmanned aerial vehicle.

Preferably, the lower surfaces of the two support plates are fixedly connected with a cushion pad.

Compared with the prior art, the utility model has the beneficial effects that: conveniently drive the steering panel through setting up step motor and rotate, thereby it rotates to stably drive the U-shaped board under the sliding action of ring channel and slide bar, thereby can adjust the orientation of solar energy conversion board, and it rotates to drive the threaded rod through setting up driving motor, the threaded rod drives the thread bush and removes under the slip limiting displacement of slide and spout, it slides at the sliding tray inside to drive the slider under the rotating action of connecting rod when the thread bush removes, thereby can be under the rotating action of pivot the angle of stable regulation solar energy conversion board.

Drawings

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

FIG. 2 is a schematic view of the internal structure of the mounting box of the present invention;

FIG. 3 is an enlarged view of portion A of FIG. 2;

FIG. 4 is a schematic cross-sectional view taken along line B-B of FIG. 2 in accordance with the present invention;

fig. 5 is a schematic bottom perspective view of the adjustment plate of the present invention.

In the figure: 1. an unmanned aerial vehicle;

2. a steering mechanism; 21. installing a box; 22. an annular groove; 23. a stepping motor; 24. a steering plate; 25. a slide bar;

3. an adjustment mechanism; 31. a U-shaped plate; 32. a chute; 33. a drive motor; 34. a threaded rod; 35. a threaded sleeve; 36. a slide plate;

4. a solar mechanism; 41. a rotating shaft; 42. an adjusting plate; 43. a solar energy conversion panel; 44. a sliding groove; 45. a profiled slide block; 46. a connecting rod;

5. and (4) a support plate.

Detailed Description

The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only a part of the embodiments of the present invention, and not all of the embodiments. All other embodiments, which can be derived by a person skilled in the art from the embodiments given herein without making any creative effort, shall fall within the protection scope of the present invention.

Referring to fig. 1-5, the present invention provides a technical solution: a novel solar unmanned aerial vehicle comprises an unmanned aerial vehicle 1, wherein the upper end of the unmanned aerial vehicle 1 is fixedly connected with a steering mechanism 2, the upper end of the steering mechanism 2 is fixedly connected with an adjusting mechanism 3, and the upper end of the adjusting mechanism 3 is rotatably connected with a solar mechanism 4;

steering mechanism 2 includes that an upper end is the install bin 21 that the opening form set up, and install bin 21 fixed connection is in unmanned aerial vehicle 1 upper end, and install bin 21 bottom inner tank wall has seted up an annular channel 22, and install bin 21 bottom center department fixedly connected with a step motor 23, step motor 23 output end fixedly connected with a steering panel 24.

Adjustment mechanism 3 includes a U-shaped plate 31, and U-shaped plate 31 high connection is at 24 upper surfaces of steering wheel, and a spout 32 has been seted up to U-shaped plate 31 bottom, and 31 one side fixedly connected with of U-shaped plate a driving motor 33, a driving motor 33 output end fixedly connected with threaded

rod

34, 34 pole wall threaded connection of threaded rod has a thread bush 35, slide 36 of fixedly connected with of thread bush 35 lower extreme, slide 36 sliding connection is in spout 32.

Solar energy mechanism 4 includes a pivot 41, pivot 41 rotates to be connected in U-shaped plate 31 upper end one side, and pivot 41 upper end rotates and is connected with an regulating plate 42, a solar energy converter 43 of regulating plate 42 upper end fixedly connected with, a sliding tray 44 has been seted up to regulating plate 42 lower extreme, sliding tray 44 sliding connection has a dysmorphism slider 45, dysmorphism slider 45 rotates jointly with thread bush 35 and is connected with a connecting rod 46, can drive dysmorphism slider 45 when being favorable to removing through connecting rod 46 and slide in sliding tray 44 is inside, thereby the angle of regulating plate 42 and solar energy converter 43 is adjusted under pivot 41's effect.

The two sides of the lower surface of the steering plate 24 are fixedly connected with the sliding rods 25, the lower ends of the two sliding rods 25 extend to the annular groove 22 and are connected in the annular groove 22 in a sliding mode, sliding in the annular groove 22 through the sliding rods 25 is facilitated, rotation of the steering plate 24 is increased, and the orientation of the solar energy conversion plate 43 is convenient to adjust.

Two support plates 5 are fixedly connected to two sides of the lower surface of the unmanned aerial vehicle 1, and the two support plates 5 are favorable for stably supporting the unmanned aerial vehicle 1.

The two support plates 5 are fixedly connected with a cushion pad on the lower surface, so that the two cushion pads can buffer the unmanned aerial vehicle 1 when landing, and the damage is avoided.

Specifically, when the utility model is used, after the unmanned aircraft 1 takes off, the stepping motor 23 is started, the output end of the stepping motor 23 drives the steering plate 24 to rotate, the steering plate 24 drives the two sliding rods 25 to slide in the annular groove 22 when rotating, so that the rotation stability of the steering plate 24 is increased, the steering plate 24 synchronously drives the U-shaped plate 31 to rotate, then the driving motor 33 is started, the output end of the driving motor 33 drives the threaded rod 34 to rotate, the threaded rod 34 drives the threaded sleeve 35, the threaded sleeve 35 moves under the sliding limiting effect of the sliding groove 32 and the sliding plate 36, at the moment, the threaded sleeve 35 pushes the special-shaped sliding block 45 to slide in the sliding groove 44 through the rotating connecting rod 46, the special-shaped sliding block 45 drives the adjusting plate 42 to rotate through the rotating shaft 41 when sliding, and the solar energy conversion plate 43 can be adjusted by the adjusting plate 42 when adjusting.

In the description of the present invention, it is to be understood that the terms "coaxial", "bottom", "one end", "top", "middle", "other end", "upper", "one side", "top", "inner", "front", "center", "both ends", and the like, indicate orientations or positional relationships based on those shown in the drawings, and are only for convenience of description and simplicity of description, and do not indicate or imply that the referenced device or element must have a particular orientation, be constructed and operated in a particular orientation, and thus, are not to be construed as limiting the present invention.

Furthermore, the terms "first", "second", "third", "fourth" are used for descriptive purposes only and are not to be construed as indicating or implying a relative importance or implicitly indicating the number of technical features indicated, whereby the features defined as "first", "second", "third", "fourth" may explicitly or implicitly include at least one such feature.

In the present invention, unless otherwise explicitly stated or limited, the terms "mounted," "disposed," "connected," "fixed," "screwed" and the like are to be understood broadly, for example, as being fixedly connected, detachably connected, or integrated; can be mechanically or electrically connected; the terms may be directly connected or indirectly connected through an intermediate, and may be communication between two elements or interaction relationship between two elements, unless otherwise specifically limited, and the specific meaning of the terms in the present invention will be understood by those skilled in the art according to specific situations.

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 utility model, the scope of which is defined in the appended claims and their equivalents.

Claims

1. The utility model provides a novel solar unmanned aerial vehicle which characterized in that: the solar unmanned plane comprises an unmanned plane (1), wherein the upper end of the unmanned plane (1) is fixedly connected with a steering mechanism (2), the upper end of the steering mechanism (2) is fixedly connected with an adjusting mechanism (3), and the upper end of the adjusting mechanism (3) is rotatably connected with a solar mechanism (4);

steering mechanism (2) are install bin (21) that the opening form set up including an upper end, install bin (21) fixed connection is in unmanned aerial vehicle (1) upper end, just one ring channel (22) have been seted up to the tank wall in install bin (21) bottom, install bin (21) bottom center department fixedly connected with one step motor (23), steering panel (24) of step motor (23) output fixedly connected with.

2. The novel solar unmanned aerial vehicle of claim 1, wherein: adjustment mechanism (3) include a U-shaped plate (31), U-shaped plate (31) high connection is at steering wheel (24) upper surface, a spout (32) have been seted up to U-shaped plate (31) bottom, just driving motor (33) of U-shaped plate (31) one side fixedly connected with, driving motor (33) output end fixedly connected with threaded rod (34), threaded rod (34) pole wall threaded connection has a thread bush (35), slide (36) of thread bush (35) lower extreme fixedly connected with, slide (36) sliding connection is in spout (32).

3. The novel solar unmanned aerial vehicle of claim 1, wherein: solar energy mechanism (4) are including a pivot (41), pivot (41) are rotated and are connected in U-shaped board (31) upper end one side, just pivot (41) upper end is rotated and is connected with an regulating plate (42), solar energy converter plate (43) of regulating plate (42) upper end fixedly connected with, a sliding tray (44) has been seted up to regulating plate (42) lower extreme, sliding tray (44) sliding connection has a dysmorphism slider (45), dysmorphism slider (45) and thread bush (35) rotate jointly and are connected with a connecting rod (46).

4. The novel solar unmanned aerial vehicle of claim 1, wherein: two sides of the lower surface of the steering plate (24) are fixedly connected with a sliding rod (25), and the lower ends of the two sliding rods (25) extend to the annular groove (22) and are connected in the annular groove (22) in a sliding mode.

5. The novel solar unmanned aerial vehicle of claim 1, wherein: two support plates (5) are fixedly connected to two sides of the lower surface of the unmanned aerial vehicle (1).

6. The novel solar unmanned aerial vehicle of claim 5, wherein: the lower surfaces of the two support plates (5) are fixedly connected with a cushion pad.