CN211442765U

CN211442765U - Solar energy continuation of journey unmanned vehicles with gliding fin device

Info

Publication number: CN211442765U
Application number: CN201921871560.9U
Authority: CN
Inventors: 杜远坤; 王磊
Original assignee: Individual
Current assignee: Individual
Priority date: 2019-11-01
Filing date: 2019-11-01
Publication date: 2020-09-08
Anticipated expiration: 2029-11-01

Abstract

The utility model belongs to the technical field of unmanned vehicles, especially, be a solar energy continuation of journey unmanned vehicles with gliding fin device, including the aircraft body and stop screw, the top of the aircraft body is fixed with the wing, and the upper surface of wing has seted up the draw-in groove to the internally mounted of draw-in groove has solar cell panel, stop screw sets up in solar cell panel's the outside, the aircraft nose is installed to one side of the aircraft body, and the opposite side of the aircraft body installs the connecting plate to the avris of connecting plate is connected with the gliding wing. This solar energy continuation of journey unmanned vehicles with gliding fin device is provided with the glide vane, through according to installing the glide vane in the aircraft body outside for the aircraft has possessed the function of gliding, and the inside slider that is provided with of glide vane, slides through the slider and can take out the glide vane, increases the area of glide vane, has improved the gliding performance of the aircraft body, makes the aircraft have better flight performance.

Description

Solar energy continuation of journey unmanned vehicles with gliding fin device

Technical Field

The utility model relates to an unmanned vehicles technical field specifically is a solar energy continuation of journey unmanned vehicles with gliding fin device.

Background

The unmanned aerial vehicle is used as intelligent flight equipment and is generally used for executing special tasks, operators only need to remotely control the unmanned aerial vehicle on the ground, and casualties possibly caused by the tasks are reduced, so that the unmanned aerial vehicle is widely applied to all countries in the world.

The unmanned vehicles on the market mostly rely on the power supply of unmanned vehicles self-carrying, because of the volume restriction, the power supply ability is limited, leads to duration weaker, and does not possess the gliding fin for the maneuverability of aircraft is relatively poor, makes the use of aircraft receive the limitation.

Aiming at the problems, innovative design is urgently needed on the basis of the original unmanned aerial vehicle.

SUMMERY OF THE UTILITY MODEL

An object of the utility model is to provide a solar energy continuation of journey unmanned vehicles with gliding fin device to solve the current unmanned vehicles on the market that proposes in the above-mentioned background art and rely on unmanned vehicles from the mains operated who takes mostly, because of the volume restriction, the power supply ability is limited, leads to the continuation of journey ability weaker, and does not possess the gliding fin, makes the mobility of aircraft relatively poor, makes the use of aircraft receive the problem of limitation.

In order to achieve the above object, the utility model provides a following technical scheme: a solar energy endurance unmanned aerial vehicle with gliding tail wing device comprises a vehicle body and a limit screw, wherein wings are fixed above the vehicle body, the upper surfaces of the wings are provided with clamping grooves, and a solar cell panel is arranged in the clamping groove, the limiting screw is arranged on the outer side of the solar cell panel, a nose is arranged on one side of the aircraft body, a connecting plate is arranged on the other side of the aircraft body, the side of the connecting plate is connected with a glider, a propeller is arranged in the nose, a protective net is arranged outside the propeller, a servo motor is arranged in the aircraft body, a gear is arranged on the side of the servo motor, and the avris of gear is connected with the rack, the camera is fixed to the bottom of rack, the spout has been seted up to the inside of connecting plate, and the internally mounted of spout has the slider, the inside of connecting plate runs through there is the check lock pole.

Preferably, the number of the limit screws is 2 about the central axis of the solar cell panel, and the solar cell panel and the clamping groove form a detachable mounting structure through the limit screws.

Preferably, the gliding wing and the connecting plate form a telescopic structure through a sliding block, and the sliding block is in sliding connection with the sliding groove.

Preferably, the inner diameter of the machine head is the same as the outer diameter of the protective net, and the protective net is connected with the machine head in a clamping mode.

Preferably, the camera and the aircraft body form a lifting structure through a rack, and the rack is in meshed connection with the gear.

Preferably, the end of the locking rod is arranged in a threaded manner, and the locking rod is in threaded connection with the connecting plate.

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

1. the solar cruising unmanned aerial vehicle with the gliding tail wing device is provided with the protective net, the protective net is embedded in the machine head to protect the propeller, and the problem that the propeller is damaged, the normal work of an engine is influenced, and accidents such as crash and the like are easily caused due to the collision of the unmanned aerial vehicle with some flying birds or sundries in the flying process is avoided;

2. the solar cruising unmanned aerial vehicle with the gliding tail wing device is provided with the lifting device, the servo motor drives the gear to rotate forwards and backwards, the gear is meshed with the rack to control the rack to move upwards and downwards, and further the camera is driven to extend and retract, and the camera can be protected by the lifting device, so that the camera is prevented from being exposed outside for a long time and damaged, and the service life of the device is prevented from being influenced;

3. this solar energy continuation of journey unmanned vehicles with gliding fin device is provided with the glide vane, through according to installing the glide vane in the aircraft body outside for the aircraft has possessed the function of gliding, and the inside slider that is provided with of glide vane, slides through the slider and can take out the glide vane, increases the area of glide vane, has improved the gliding performance of the aircraft body, makes the aircraft have better flight performance.

Drawings

FIG. 1 is a schematic view of the overall side view structure of the present invention;

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

FIG. 3 is a schematic view of the fastening structure of the head and the protection net of the present invention;

fig. 4 is a schematic view of the connection structure of the glider wing and the connection plate of the present invention.

In the figure: 1. an aircraft body; 2. an airfoil; 3. a limit screw; 4. a solar panel; 5. a card slot; 6. a glider wing; 7. a machine head; 8. a protective net; 9. a propeller; 10. a servo motor; 11. a gear; 12. a rack; 13. a camera; 14. a connecting plate; 15. a chute; 16. a slider; 17. a locking lever.

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. 1-4, the present invention provides a technical solution: a solar energy endurance unmanned aerial vehicle with a gliding tail wing device comprises a vehicle body 1, wings 2, a limit screw 3, a solar cell panel 4, a clamping groove 5, a gliding wing 6, a machine head 7, a protective net 8, a propeller 9, a servo motor 10, a gear 11, a rack 12, a camera 13, a connecting plate 14, a chute 15, a slider 16 and a locking rod 17, wherein the wings 2 are fixed above the vehicle body 1, the clamping groove 5 is arranged on the upper surface of the wings 2, the solar cell panel 4 is arranged in the clamping groove 5, the limit screw 3 is arranged on the outer side of the solar cell panel 4, the machine head 7 is arranged on one side of the vehicle body 1, the connecting plate 14 is arranged on the other side of the vehicle body 1, the gliding wing 6 is connected to the lateral side of the connecting plate 14, the propeller 9 is arranged in the machine head 7, and the protective net 8 is arranged on the outer, a servo motor 10 is arranged in the aircraft body 1, a gear 11 is arranged on the side of the servo motor 10, a rack 12 is connected to the side of the gear 11, a camera 13 is fixed to the bottom of the rack 12, a sliding groove 15 is formed in a connecting plate 14, a sliding block 16 is arranged in the sliding groove 15, and a locking rod 17 penetrates through the connecting plate 14;

the number of the limiting screws 3 is 2, the limiting screws are symmetrically arranged about the central axis of the solar cell panel 4, the solar cell panel 4 and the clamping groove 5 form a detachable mounting structure through the limiting screws 3, the solar cell panel 4 is limited and fixed through the limiting screws 3, the possibility that the solar cell panel 4 falls in the flying process is avoided, and the solar cell panel 4 is convenient to maintain;

the glider 6 and the connecting plate 14 form a telescopic structure through the slider 16, the slider 16 is connected with the sliding groove 15 in a sliding way, the aircraft has a gliding function through the glider 6 arranged outside the aircraft body 1, the slider 16 is arranged inside the glider 6, the glider 6 can be drawn out through the sliding of the slider 16, the area of the glider 6 is increased, the gliding performance of the aircraft body 1 is improved, and the aircraft has better flight performance;

the inner diameter of the nose 7 is the same as the outer diameter of the protective net 8, the protective net 8 is connected with the nose 7 in a clamping mode, the protective net 8 is installed inside the nose 7 in an embedded mode and protects the propeller 9, and the problem that the propeller 9 is damaged due to collision of the unmanned aerial vehicle with some birds or sundries in the flying process, the normal work of an engine is affected, and accidents such as crash are easily caused is avoided;

the camera 13 and the aircraft body 1 form a lifting structure through a rack 12, the rack 12 is meshed with the gear 11, the gear 11 is driven to rotate forwards and backwards through the servo motor 10, the gear 11 is meshed with the rack 12 to control the rack 12 to move upwards and downwards so as to drive the camera 13 to extend and retract, and the camera 13 can be protected through the lifting device, so that the camera 13 is prevented from being damaged due to long-term exposure and the service life of the device is prevented from being influenced;

the end of the locking rod 17 is arranged by threads, the locking rod 17 is in threaded connection with the connecting plate 14, the locking rod 17 is convenient to install and detach by virtue of threaded connection, and when the glider wing 6 is pulled out, the locking rod 17 is in through connection with the connecting plate 14, so that the situation that the glider wing 6 is suddenly retracted in the flying process to influence the balance of the aircraft body 1 and cause flight accidents is avoided.

The working principle is as follows: the solar energy endurance unmanned aerial vehicle with the gliding tail wing device comprises the following steps that firstly, a solar cell panel 4 is installed along a clamping groove 5 positioned above a wing 2 in a sliding mode, then the solar cell panel 4 is limited and fixed through a limiting screw rod 3, the situation that the solar cell panel 4 is loosened and falls in the flying process is avoided, a protective net 8 is clamped with a machine head 7, a propeller 9 is protected, the situation that the unmanned aerial vehicle collides with some birds or sundries in the flying process to cause damage of the propeller 9 and influence the normal work of an engine is avoided, a servo motor 10 is turned on, the servo motor 10 drives a gear 11 to rotate forwards, a rack 12 moves downwards, a camera 13 is driven to extend out for use, the camera 13 can stretch out and draw back through the servo motor 10, the situation that the camera 13 is exposed outside for a long time and damaged is avoided, the service life of the device is influenced, and the gliding wing 6 is taken out from the inside a connecting plate 14 through a, when the glider wing 6 is pulled out, the locking rod 17 is connected with the connecting plate 14 in a penetrating way, so that the glider wing 6 is prevented from being suddenly withdrawn in the flying process, the balance of the aircraft body 1 is influenced, and the flying accident is avoided.

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 a solar energy continuation of journey unmanned vehicles with gliding fin device, includes the aircraft body (1) and stop screw (3), its characterized in that: the aircraft is characterized in that wings (2) are fixed above an aircraft body (1), a clamping groove (5) is formed in the upper surface of each wing (2), a solar cell panel (4) is arranged inside each clamping groove (5), a limit screw (3) is arranged outside each solar cell panel (4), a nose (7) is installed on one side of the aircraft body (1), a connecting plate (14) is installed on the other side of the aircraft body (1), a gliding wing (6) is connected to the side of each connecting plate (14), a propeller (9) is installed inside each nose (7), a protective net (8) is arranged outside each propeller (9), a servo motor (10) is installed inside the aircraft body (1), a gear (11) is installed on the side of each servo motor (10), a rack (12) is connected to the side of each gear (11), a camera (13) is fixed at the bottom of each rack (12), the connecting plate is characterized in that a sliding groove (15) is formed in the connecting plate (14), a sliding block (16) is arranged inside the sliding groove (15), and a locking rod (17) penetrates through the connecting plate (14).

2. The solar cruising unmanned aerial vehicle having a gliding tail device as claimed in claim 1, wherein: the limiting screw rods (3) are symmetrically arranged about the central axis of the solar cell panel (4) in number 2, and the solar cell panel (4) and the clamping grooves (5) form a detachable mounting structure through the limiting screw rods (3).

3. The solar cruising unmanned aerial vehicle having a gliding tail device as claimed in claim 1, wherein: the gliding wing (6) and the connecting plate (14) form a telescopic structure through a sliding block (16), and the sliding block (16) is in sliding connection with the sliding groove (15).

4. The solar cruising unmanned aerial vehicle having a gliding tail device as claimed in claim 1, wherein: the inner diameter of the machine head (7) is the same as the outer diameter of the protective net (8), and the protective net (8) is connected with the machine head (7) in a clamping mode.

5. The solar cruising unmanned aerial vehicle having a gliding tail device as claimed in claim 1, wherein: the camera (13) and the aircraft body (1) form a lifting structure through a rack (12), and the rack (12) is in meshed connection with the gear (11).

6. The solar cruising unmanned aerial vehicle having a gliding tail device as claimed in claim 1, wherein: the end of the locking rod (17) is arranged by threads, and the locking rod (17) is in threaded connection with the connecting plate (14).