CN215323270U

CN215323270U - Aerial endurance system of solar unmanned aerial vehicle

Info

Publication number: CN215323270U
Application number: CN202121232503.3U
Authority: CN
Inventors: 杨皓
Original assignee: Sichuan Hanhang Technology Co ltd
Current assignee: Sichuan Hanhang Technology Co ltd
Priority date: 2021-06-03
Filing date: 2021-06-03
Publication date: 2021-12-28
Anticipated expiration: 2031-06-03

Abstract

The utility model is suitable for the technical field of unmanned aerial vehicle equipment, and provides an aerial cruising system of a solar unmanned aerial vehicle. According to the utility model, the flat light flow on the ground can be monitored through the ultrasonic identification module, when the unmanned aerial vehicle needs charging operation, a flat road section which is suitable for landing and has illumination and charging functions can be identified, the solar panel module in the containing cavity can be pushed out through the first hydraulic rod, so that the two solar panel modules are unfolded for solar charging operation, the unfolded solar panel can improve the charging speed, and can be contained in the flying process, the wind resistance is reduced, the flying operation is not hindered, in addition, through the infrared sensing camera, whether human beings and animals approach to the solar panel module can be monitored when the unmanned aerial vehicle stops on the ground, once adverse factors exist, the current position can be abandoned, and the unmanned aerial vehicle can take off and continue cruising and find a safe landing point.

Description

Aerial endurance system of solar unmanned aerial vehicle

Technical Field

The utility model belongs to the technical field of unmanned aerial vehicle equipment, and particularly relates to an aerial endurance system of a solar unmanned aerial vehicle.

Background

The unmanned plane is an unmanned plane operated by radio remote control equipment and a self-contained program control device, or is completely or intermittently and autonomously operated by a vehicle-mounted computer, power of a propeller of the unmanned plane is provided through a built-in storage battery, charging operation is usually carried out through a charging pile, and a charging mode through a solar cell panel is also provided.

Present solar unmanned aerial vehicle's aerial time of endurance system, in the in-process of its use, unmanned aerial vehicle is limited because of the power supply battery, there is the limited problem of time of endurance, lead to the unable long-time continuity of operation in work area, low efficiency, present a lot of solar unmanned aerial vehicle all charge by battery board limit overlap, but solar cell panel charges slowly, often fill several hours, probably just consume for a few minutes, or increase the electric capacity of panel and reach the purpose of time of endurance again, but the battery mass that electric capacity is bigger is heavier more, increase unmanned aerial vehicle's self weight, the electric quantity that needs during the flight is bigger, be the coexistent state of profit and disadvantage.

SUMMERY OF THE UTILITY MODEL

The utility model provides an aerial endurance system of a solar unmanned aerial vehicle, which aims to solve the technical problem of short endurance of the unmanned aerial vehicle, can continuously exchange flying and charging, and can complete a remote flying task without human control.

The utility model discloses an aerial cruising system of a solar unmanned aerial vehicle, which comprises an unmanned aerial vehicle body, wherein four connecting rods are fixedly connected to the periphery of the unmanned aerial vehicle body, the other ends of the four connecting rods are fixedly connected with a propeller base, a propeller is installed at the top end of the propeller base, a containing box is installed at the bottom end of the unmanned aerial vehicle body, two containing cavities are formed in the containing box, an infrared sensing camera is fixedly connected to the front end face of the containing box, sliding grooves are formed in two sides of the inner part of each containing cavity, sliding blocks are sleeved and inserted in the sliding grooves, solar panel modules are fixedly connected to the other ends of the sliding blocks, a first hydraulic rod is connected to one side of the containing box in an embedded mode, the first hydraulic rod is fixedly connected with the solar panel modules, and two ultrasonic identification modules are fixedly connected to the bottom end of the containing box.

Preferably, the solar panel module is movably connected with the containing cavity, and the solar panel module forms a sliding structure through the sliding block and the sliding groove.

Preferably, one end of the first hydraulic rod is connected with the inside of the storage cavity, and the solar panel module and the storage box form a telescopic structure through the first hydraulic rod.

Preferably, the two sides of the bottom end of the containing box are fixedly connected with first movable shafts, the other ends of the first movable shafts are rotatably connected with a supporting frame, the bottom end of the containing box is fixedly connected with two second movable shafts, the other ends of the second movable shafts are rotatably connected with second hydraulic rods, and third movable shafts are fixedly connected between the second hydraulic rods and the supporting frame.

Preferably, the second hydraulic rod forms a first rotating structure with the support frame through the third movable shaft, and the second hydraulic rod forms a second rotating structure with the storage box through the second movable shaft.

Preferably, the support frame forms a third rotating structure through the space between the first movable shaft and the storage box, and the support frame forms a foldable structure through the space between the second hydraulic rod and the first movable shaft and the storage box.

Compared with the prior art, the utility model has the beneficial effects that:

1. according to the utility model, the flat light flow on the ground can be monitored through the ultrasonic identification module, when the unmanned aerial vehicle needs charging operation, a flat road section which is suitable for landing and has illumination charging on a flight road can be identified, then the solar panel module in the containing cavity can be pushed out through the first hydraulic rod, so that the two solar panel modules are unfolded for solar charging operation, the unfolded solar panel can improve the charging speed, and can be contained in the flight, the wind resistance is reduced, the flight operation is not hindered, in addition, through the infrared sensing camera, whether human beings and animals approach to the solar panel module can be monitored when the unmanned aerial vehicle stops on the ground, once adverse factors exist, the current position can be abandoned, and the unmanned aerial vehicle can take off and continue cruising and searches for a safe landing point.

2. According to the unmanned aerial vehicle, the support frames can be pushed to rotate through the second hydraulic rod, so that the two support frames can rotate to proper angles, and the unmanned aerial vehicle body can be more stable when parked and charged through the two adjustable support frames, so that the unmanned aerial vehicle is prevented from toppling over due to ground depressions.

Drawings

FIG. 1 is a schematic front view of an electric heating type air heating apparatus according to the present invention;

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

fig. 3 is a schematic top view of the storage box according to the present invention.

In the figure: 1. an unmanned aerial vehicle body; 2. a connecting rod; 3. a propeller base; 4. a propeller; 5. a storage box; 6. an infrared sensing camera; 7. a receiving cavity; 8. a chute; 9. a slider; 10. a solar panel module; 11. a first hydraulic lever; 12. an ultrasonic identification module; 13. a first movable shaft; 14. a support frame; 15. a second movable shaft; 16. a second hydraulic rod; 17. a third movable shaft.

Detailed Description

In order to make the objects, technical solutions and advantages of the present invention more apparent, the present invention is described in further detail below with reference to the accompanying drawings and embodiments. It should be understood that the specific embodiments described herein are merely illustrative of the utility model and are not intended to limit the utility model.

Referring to fig. 1-3, the utility model provides an aerial cruising system of a solar unmanned aerial vehicle, comprising an unmanned aerial vehicle body 1, four connecting rods 2 fixedly connected around the unmanned aerial vehicle body 1, a propeller base 3 fixedly connected with the other ends of the four connecting rods 2, and the top end of the propeller base 3 is provided with a propeller 4, the bottom end of the unmanned aerial vehicle body 1 is provided with a containing box 5, two containing cavities 7 are arranged in the containing box 5, the front end face of the containing box 5 is fixedly connected with an infrared sensing camera 6, sliding grooves 8 are arranged on two sides in the containing cavities 7, a slide block 9 is sleeved and inserted in the slide groove 8, the other end of the slide block 9 is fixedly connected with a solar panel module 10, one side of the containing box 5 is embedded and connected with a first hydraulic rod 11, the first hydraulic rod 11 is fixedly connected with the solar panel module 10, and the two ultrasonic identification modules 12 are fixedly connected with the bottom end of the storage box 5.

In this embodiment, a section of the spectrum of the infrared sensor camera 6 having a wavelength from 0.76 to 400 μm is called infrared ray, which is invisible ray, and all substances above absolute zero (-273.15 ℃) can generate infrared ray. Modern physics, known as heat rays, can monitor whether a human or animal is in proximity to the device.

Specifically, the solar panel module 10 is movably connected with the accommodating cavity 7, and the solar panel module 10 forms a sliding structure with the sliding chute 8 through the sliding block 9. In the present embodiment, the first hydraulic lever 11 can push the solar panel modules 10 to unfold or store the two solar panel modules 10.

One end of the first hydraulic rod 11 is connected with the inside of the storage cavity 7, and the solar panel module 10 and the storage box 5 form a telescopic structure through the first hydraulic rod 11. In the present embodiment, the solar panel module 10 is connected to a battery built in the main body 1 of the unmanned aerial vehicle via a connection line.

Further, the two sides of the bottom end of the containing box 5 are fixedly connected with first movable shafts 13, the other ends of the first movable shafts 13 are rotatably connected with a supporting frame 14, the two bottom ends of the containing box 5 are fixedly connected with two second movable shafts 15, the other ends of the second movable shafts 15 are rotatably connected with second hydraulic rods 16, and third movable shafts 17 are fixedly connected between the second hydraulic rods 16 and the supporting frame 14.

In the present embodiment, the second hydraulic rod 16 can push the supporting frame 14, so that the supporting frame 14 can rotate through the first movable shaft 13 to adjust the angle.

Further, the second hydraulic rod 16 forms a first rotation structure through the third movable shaft 17 and the support frame 14, and the second hydraulic rod 16 forms a second rotation structure through the second movable shaft 15 and the storage box 5. In this embodiment, the device can be stably supported by the two angle-adjustable support frames 14.

Further, the support frame 14 forms a third rotation structure with the storage box 5 through the first movable shaft 13, and the support frame 14 forms a foldable structure with the storage box 5 through the second hydraulic rod 16 and the first movable shaft 13. In this embodiment, the support frame 14 can be folded, and the unmanned aerial vehicle body 1 thereof reduces the wind resistance when flying.

The working principle and the using process of the utility model are as follows: when the unmanned aerial vehicle is used, firstly, when the electric quantity of the unmanned aerial vehicle body 1 is insufficient, the flat light stream on the ground is monitored and scanned through the ultrasonic identification module 12, a flat road section which is suitable for landing and has illumination and charging is searched, when the unmanned aerial vehicle body 1 is parked on a proper ground, the support frame 14 is pushed through the second hydraulic rod 16, the support frame 14 is enabled to rotate through the first movable shaft 13, the two support frames 14 are enabled to rotate to a proper angle, the unmanned aerial vehicle body 1 is stably parked through the two adjustable support frames 14, the solar panel module 10 is pushed through the first hydraulic rod 11, the solar panel module 10 slides in the sliding groove 8 through the sliding block 9 and is pushed out from the containing cavity 7, the two solar panel modules 10 are unfolded for solar charging operation, whether human beings and animals approach or not is monitored and scanned through the infrared sensing camera 6, and once adverse factors exist, the solar panel module 10 is stored, the current position is abandoned, and the solar panel module takes off to continue cruising and searches for a safe landing point, thereby completing the working principle of the utility model.

The above description is only for the purpose of illustrating the preferred embodiments of the present invention and is not to be construed as limiting the utility model, and any modifications, equivalents and improvements made within the spirit and principle of the present invention are intended to be included within the scope of the present invention.

Claims

1. The utility model provides a solar energy unmanned aerial vehicle's aerial continuation of journey system, includes unmanned aerial vehicle body (1), its characterized in that: four connecting rods (2) are fixedly connected around the unmanned aerial vehicle body (1), the other ends of the four connecting rods (2) are fixedly connected with a propeller base (3), a propeller (4) is installed at the top end of the propeller base (3), a containing box (5) is installed at the bottom end of the unmanned aerial vehicle body (1), two containing cavities (7) are formed in the containing box (5), an infrared sensing camera (6) is fixedly connected with the front end face of the containing box (5), sliding grooves (8) are formed in two sides in the containing cavities (7), sliding blocks (9) are sleeved and inserted in the sliding grooves (8), a solar panel module (10) is fixedly connected with the other ends of the sliding blocks (9), a first hydraulic rod (11) is connected to one side of the containing box (5) in an embedded mode, and the first hydraulic rod (11) is fixedly connected with the solar panel module (10), two ultrasonic identification modules (12) are fixedly connected to the bottom end of the containing box (5).

2. The aerial endurance system of a solar drone of claim 1, wherein: the solar panel module (10) is movably connected with the containing cavity (7), and the solar panel module (10) and the sliding chute (8) form a sliding structure through the sliding block (9).

3. The aerial endurance system of a solar drone of claim 1, wherein: one end of the first hydraulic rod (11) is connected with the interior of the containing cavity (7), and the solar panel module (10) and the containing box (5) form a telescopic structure through the first hydraulic rod (11).

4. The aerial endurance system of a solar drone of claim 1, wherein: containing box (5) bottom both sides fixedly connected with first loose axle (13), and first loose axle (13) other end rotates and is connected with support frame (14), two second loose axles (15) of containing box (5) bottom fixedly connected with, and second loose axle (15) other end rotate and are connected with second hydraulic stem (16), fixedly connected with third loose axle (17) between second hydraulic stem (16) and support frame (14).

5. The aerial endurance system of a solar drone of claim 4, wherein: the second hydraulic rod (16) forms a first rotating structure with the support frame (14) through the third movable shaft (17), and the second hydraulic rod (16) forms a second rotating structure with the containing box (5) through the second movable shaft (15).

6. The aerial endurance system of a solar drone of claim 5, wherein: the support frame (14) forms a third rotating structure through the space between the first movable shaft (13) and the containing box (5), and the support frame (14) forms a foldable structure through the space between the second hydraulic rod (16), the first movable shaft (13) and the containing box (5).