Solar charging device for wing surface of unmanned aerial vehicle

Abstract

The utility model relates to the technical field of unmanned aerial vehicle airfoil solar charging, in particular to an unmanned aerial vehicle airfoil solar charging device, which is provided with a protection mechanism and an overturning mechanism, so that a solar panel can face the sun to the greatest extent during use in the unmanned aerial vehicle airfoil solar charging process, and electric energy can be conveniently supplemented during use. The storage is convenient; comprising a driving mechanism; the device further comprises two sets of protection mechanisms, two sets of overturning mechanisms, two sets of folding wing mechanisms and two sets of connecting mechanisms, the two sets of protection mechanisms are installed on the driving mechanism, one set of overturning mechanism is installed in each set of protection mechanism, and one set of folding wing mechanism is installed on each set of protection mechanism. Each group of protection mechanism is connected with each group of folding wing mechanism through a group of connecting mechanism; the driving mechanism is used for driving, the protection mechanism is used for protection, the overturning mechanism is used for charging energy, the wing folding mechanism is used for storage, and the connecting mechanism is used for connection.

Description

TECHNICAL FIELD

[0001] The utility model relates to the technical field of unmanned aerial vehicle wing surface solar charging, especially to an unmanned aerial vehicle wing surface solar charging device. BACKGROUND

[0002] As a kind of radio remote control or by itself program control-based unmanned aircraft, compared with manned aircraft, unmanned aircraft is low in cost, easy to use, and can be used to detect dangerous or inaccessible places.

[0003] In the existing unmanned aerial vehicle wing surface solar charging device, for example, the utility model patent with application number 201820801905.2 discloses a kind of unmanned aerial vehicle solar range extender, which can generate electricity using solar energy and laser power, and is light in weight, enabling positioning and identification of unmanned aerial vehicles, with longer endurance time than single solar charging.

[0004] However, during the unmanned aerial vehicle wing surface solar charging process, it is necessary to charge the unmanned aerial vehicle during flight to maintain the flight duration. However, during sunrise and sunset, sunlight is relatively horizontal, and the unmanned aerial vehicle cannot be covered and charged. UTILITY MODEL CONTENT

[0005] To solve the above technical problems, the utility model provides an unmanned aerial vehicle wing surface solar charging device by setting protection mechanism and overturning mechanism, so that the solar panel can be oriented towards the sun during use during the unmanned aerial vehicle wing surface solar charging process, facilitating the replenishment of electric energy during use, and facilitating storage.

[0006] The utility model discloses an unmanned aerial vehicle wing surface solar charging device, which comprises a driving mechanism, two groups of protection mechanisms, two groups of overturning mechanisms, two groups of folding wing mechanisms and two groups of connecting mechanisms.

[0007] The driving mechanism drives, the protection mechanism protects, the overturning mechanism charges, the folding wing mechanism stores, and the connecting mechanism connects. The unmanned aerial vehicle is driven by the driving mechanism, the equipment is protected by the protection mechanism, the overturning mechanism charges, the folding wing mechanism stores, and the connecting mechanism stably connects, so that the solar panel can be oriented towards the sun during use during the unmanned aerial vehicle wing surface solar charging process, facilitating the replenishment of electric energy during use, and facilitating storage.

[0008] Preferably, the driving mechanism comprises a fuselage, two sets of tail wings and a steering wing, the two sets of tail wings are installed on the fuselage, and the steering wing is installed on the upper end of the fuselage; the fuselage cooperates with the tail wings to drive, and the steering wing is used for steering.

[0009] Preferably, the protection mechanism comprises wings and a light-transmitting plate, the wings are installed on the fuselage, and the light-transmitting plate is installed on the wings; the wings are used for flying, and the light-transmitting plate is used for facilitating sunlight to enter and protecting the equipment.

[0010] Preferably, the overturning mechanism comprises a solar panel, two sets of telescopic rods, a threaded block, a lead screw and a motor, the solar panel is rotatably installed in the wing, the two sets of telescopic rods are rotatably connected with the solar panel, the threaded block is rotatably connected with the two sets of telescopic rods, the lead screw is rotatably installed in the wing and is threadedly connected with the threaded block, and the motor is installed in the wing and connected with the input end of the lead screw; the motor is turned on to drive the lead screw to rotate, the lead screw rotates to threadedly connect with the threaded block to move the threaded block, and the threaded block moves to connect with the telescopic rods to incline the solar panel towards the sun.

[0011] Preferably, the folding wing mechanism comprises a sub-wing and a control wing, the sub-wing is rotatably installed on the wing, the control wing is rotatably installed on the sub-wing, and the sub-wing and the wing are provided with a connecting and fixing device; the sub-wing is turned over to facilitate storage, and the control wing is used for lifting the aircraft.

[0012] Preferably, the connecting mechanism comprises two sets of sliding plates, a plurality of springs and a connecting plate, the two sets of sliding plates are slidably installed in the wing and the sub-wing through the plurality of springs, and the two sets of sliding plates are rotatably connected through the connecting plate; the springs support the sliding plates to stabilize the structure, and the connecting plate is used for facilitating the bending of the equipment.

[0013] Compared with the prior art, the unmanned aerial vehicle can maximize the inclination of the solar panel towards the sun during the solar charging process, supplement the electric energy during use, and facilitate storage. BRIEF DESCRIPTION OF DRAWINGS

[0014] Figure 1 is the isometric structural schematic diagram of the utility model;

[0015] Figure 2 is the front view sectional isometric structural schematic diagram of the utility model;

[0016] Figure 3 is the left view sectional isometric structural schematic diagram of the utility model;

[0017] Figure 4 is the axial measurement structure schematic view of the utility model;

[0018] Figure 5 is the axial measurement structure schematic view of the utility model;

[0019] In the drawing, mark: 1, drive mechanism;11, fuselage;12, tail wing;13, steering wing;2, protection mechanism;21, wing;22, light transmission plate;3, overturning mechanism;31, solar panel;32, telescopic rod;33, screw block;34, lead screw;35, motor;4, folding wing mechanism;41, auxiliary wing;42, control wing;5, connecting mechanism;51, sliding plate;52, spring;53, connecting plate. DETAILED DESCRIPTION

[0020] In order to facilitate understanding the utility model, the utility model will be described more fully below with reference to relevant drawings.The utility model can be realized in many different forms, and is not limited to the embodiments described herein.Contrarily, the purpose of providing these embodiments is to make the disclosure of the utility model more thorough and comprehensive.

[0021] Embodiment 1

[0022] As Figures 1 to 5 shown, a kind of unmanned aerial vehicle wing surface solar charging device, including drive mechanism 1, still including two groups of protection mechanism 2, two groups of overturning mechanism 3, two groups of folding wing mechanism 4 and two groups of connecting mechanism 5, two groups of protection mechanism 2 are installed on drive mechanism 1, each group of protection mechanism 2 is installed with a group of overturning mechanism 3, each group of protection mechanism 2 is installed with a group of folding wing mechanism 4, each group of protection mechanism 2 and each group of folding wing mechanism 4 are connected by a group of connecting mechanism 5;

[0023] The drive mechanism 1 drives, protection mechanism 2 protects, overturning mechanism 3 charges, folding wing mechanism 4 is stored, and connecting mechanism 5 is connected;

[0024] Drive mechanism 1 includes fuselage 11, two groups of tail wing 12 and steering wing 13, two groups of tail wing 12 are installed on fuselage 11, and steering wing 13 is installed on the upper end of fuselage 11;

[0025] Protection mechanism 2 includes wing 21 and light transmission plate 22, wing 21 is installed on fuselage 11, and light transmission plate 22 is installed on wing 21;

[0026] The overturning mechanism 3 comprises a solar panel 31, two groups of telescopic rods 32, a threaded block 33, a lead screw 34 and a motor 35, the solar panel 31 is rotatably installed in the wing 21, the two groups of telescopic rods 32 are rotatably connected with the solar panel 31, the threaded block 33 is rotatably connected with the two groups of telescopic rods 32, the lead screw 34 is rotatably installed in the wing 21 and is threadedly matched with the threaded block 33, and the motor 35 is installed in the wing 21 and is connected with the input end of the lead screw 34;

[0027] The folding wing mechanism 4 comprises a sub-wing 41 and a control wing 42, the sub-wing 41 is rotatably installed on the wing 21, the control wing 42 is rotatably installed on the sub-wing 41, and the sub-wing 41 is provided with a connecting and fixing device on the wing 21;

[0028] The connecting mechanism 5 comprises two groups of sliding plates 51, a plurality of springs 52 and a connecting plate 53, the two groups of sliding plates 51 are slidably installed in the wing 21 and the sub-wing 41 through the plurality of springs 52, and the two groups of sliding plates 51 are rotatably connected through the connecting plate 53;

[0029] The unmanned aerial vehicle wing surface solar charging device is driven by the fuselage 11 in cooperation with the tail wing 12, is turned by the steering wing 13, flies by the wing 21, facilitates sunlight to enter and protects the equipment at the same time by the light-transmitting plate 22, drives the lead screw 34 to rotate by opening the motor 35, the lead screw 34 is threadedly matched with the threaded block 33 to move the threaded block 33 while rotating, the threaded block 33 is moved while cooperating with the telescopic rod 32 to make the solar panel 31 incline towards the sun to charge, is convenient for storage by turning over the sub-wing 41, and the lifting of the aircraft is carried out by cooperating with the control wing 42, the structure is stabilized by supporting the sliding plate 51 by the spring 52, and the equipment is bent by cooperating with the connecting plate 53.

[0030] As shown in Figures 1 to 5 The unmanned aerial vehicle wing surface solar charging device is driven by the fuselage 11 in cooperation with the tail wing 12, is turned by the steering wing 13, flies by the wing 21, facilitates sunlight to enter and protects the equipment at the same time by the light-transmitting plate 22, drives the lead screw 34 to rotate by opening the motor 35, the lead screw 34 is threadedly matched with the threaded block 33 to move the threaded block 33 while rotating, the threaded block 33 is moved while cooperating with the telescopic rod 32 to make the solar panel 31 incline towards the sun to charge, is convenient for storage by turning over the sub-wing 41, and the lifting of the aircraft is carried out by cooperating with the control wing 42, the structure is stabilized by supporting the sliding plate 51 by the spring 52, and the equipment is bent by cooperating with the connecting plate 53.

[0031] The motor 35 is purchased on the market, and the technical personnel in the industry only needs to install and operate according to the use instruction book attached, so that the technical personnel in the field does not need to pay creative labor.

[0032] The main function realized by the utility model is that in the unmanned aerial vehicle wing surface solar charging working process, the protection mechanism and the overturning mechanism are arranged, so that the unmanned aerial vehicle wing surface solar charging process can maximize the solar panel to face the sun during use, the electric energy is supplemented during use, and storage is facilitated.

[0033] The above is only the preferred embodiment of the utility model, and it should be pointed out that for ordinary technical personnel in the technical field, without departing from the technical principle of the utility model, a number of improvements and modifications can be made, and these improvements and modifications should be regarded as the protection range of the utility model.

Claims

1. An unmanned airfoil solar charging device comprising a driving mechanism (1); characterized in that, Two sets of protection mechanisms (2), two sets of overturning mechanisms (3), two sets of folding wing mechanisms (4) and two sets of connecting mechanisms (5) are also included, the two sets of protection mechanisms (2) are installed on the driving mechanism (1), each set of protection mechanism (2) is installed with a set of overturning mechanism (3), each set of protection mechanism (2) is installed with a set of folding wing mechanism (4), and each set of protection mechanism (2) and each set of folding wing mechanism (4) are connected through a set of connecting mechanism (5); The driving mechanism (1) drives, the protection mechanism (2) protects, the overturning mechanism (3) charges, the folding wing mechanism (4) stores, and the connecting mechanism (5) connects.

2. A solar charging device for unmanned airfoils as claimed in claim 1, wherein, The driving mechanism (1) includes a fuselage (11), two sets of tail wings (12) and a steering wing (13), the two sets of tail wings (12) are installed on the fuselage (11), and the steering wing (13) is installed on the upper end of the fuselage (11).

3. A solar charging apparatus for unmanned airfoils as claimed in claim 2, wherein, The protection mechanism (2) includes a wing (21) and a light transmission plate (22), the wing (21) is installed on the fuselage (11), and the light transmission plate (22) is installed on the wing (21).

4. A solar charging apparatus for unmanned airfoils as claimed in claim 3, wherein, The overturning mechanism (3) includes a solar panel (31), two sets of telescopic rods (32), a threaded block (33), a lead screw (34) and a motor (35), the solar panel (31) is rotatably installed in the wing (21), the two sets of telescopic rods (32) are rotatably connected with the solar panel (31), the threaded block (33) is rotatably connected with the two sets of telescopic rods (32), the lead screw (34) is rotatably installed in the wing (21) and is threadedly matched with the threaded block (33), and the motor (35) is installed in the wing (21) and has an output end connected with an input end of the lead screw (34).

5. A solar charging apparatus for unmanned airfoils as claimed in claim 3, wherein, The folding wing mechanism (4) includes a secondary wing (41) and a control wing (42), the secondary wing (41) is rotatably installed on the wing (21), the control wing (42) is rotatably installed on the secondary wing (41), and the secondary wing (41) is provided with a connecting and fixing device on the wing (21).

6. A solar charging apparatus for unmanned airfoils as claimed in claim 5, wherein, The connecting mechanism (5) includes two sets of sliding plates (51), a plurality of springs (52) and a connecting plate (53), the two sets of sliding plates (51) are slidably installed in the wing (21) and the secondary wing (41) through the plurality of springs (52), and the two sets of sliding plates (51) are rotatably connected through the connecting plate (53).

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