Solar charging hangar

Abstract

The utility model discloses a solar charging hangar, which comprises a hangar and a solar panel, a first cavity and a second cavity are formed in the hangar, and a charging device is installed in the first cavity to place and charge a to-be-charged unmanned aerial vehicle; the second cavity is used for placing a storage battery, and the storage battery is connected with the charging device; the solar panel is suitable for being installed on the outer surface of the hangar and connected with the storage battery. According to the structure, when the unmanned aerial vehicle is used at the position far away from the charging pile, the solar charging hangar can be carried to the position close to the using position of the unmanned aerial vehicle, when the electric quantity of the unmanned aerial vehicle is insufficient, the unmanned aerial vehicle can be placed on the charging device in the first cavity to be charged, and the charging portability is improved. Solar energy is converted into electric energy, environmental pollution is avoided, the timeliness of power supply is improved, and the situation that normal power supply of the unmanned aerial vehicle is affected due to the fact that a storage battery is out of power is avoided.

Description

Technical Field

[0001] The utility model relates to the technical field of UAV auxiliary devices, and particularly relates to a solar charging hangar. Background Art

[0002] A UAV is an unmanned aircraft using radio remote control equipment and self - contained program control devices. According to different platforms, it can be divided into three major platforms: fixed - wing UAVs, unmanned helicopters, and multi - rotor UAVs. Multi - rotor UAVs are mostly used for leisure purposes such as consumer aerial photography and games due to their convenient operation.

[0003] However, in the related art, if alternating current from the power grid is used, preset cables are required. When using a UAV at a location far from the charging pile, charging is rather troublesome. Summary of the Utility Model

[0004] Therefore, the technical problem to be solved by the utility model is to overcome the defect that if alternating current from the national power grid is used, preset cables are required, and when using a UAV at a location far from the charging pile, charging is rather troublesome.

[0005] For this reason, the utility model provides a solar charging hangar, including:

[0006] A hangar, in which a first cavity and a second cavity are arranged. A charging device is installed in the first cavity to place the UAV to be charged and charge it; the second cavity is used to place a storage battery, and the storage battery is connected to the charging device;

[0007] A solar panel, which is suitable for being installed on the outer surface of the hangar, and the solar panel is connected to the storage battery.

[0008] Optionally, the above - mentioned solar charging hangar further includes a control structure. The solar panel is suitable for being installed on the control structure, and the control structure is used to drive the solar panel to rotate to change the working angle of the solar panel.

[0009] Optionally, the above - mentioned control structure includes:

[0010] A fixing plate, which is installed on the surface of the hangar;

[0011] A driving member, which is connected to the fixing plate. An installation bracket is arranged at the output shaft end of the driving member, and the installation bracket is used to fix the solar panel.

[0012] Optionally, the plane where the surface of the solar panel facing the light source is located intersects with the central axis of the output shaft of the driving member.

[0013] Optionally, the above control structure further includes: a light intensity detector, and / or a light sensor; both the light intensity detector and the light sensor are used to detect the light intensity to control the operation of the driving member.

[0014] Optionally, a first connecting portion is provided on the fixing plate close to the hangar, and a second connecting portion is provided on the side surface of the hangar. The fixing plate can be detachably mounted on the surface of the hangar through the cooperation of the first connecting portion and the second connecting portion.

[0015] Optionally, the above first connecting portion is a clamping groove, and the second connecting portion is a snap.

[0016] Optionally, both the first connecting portion and the second connecting portion are magnetic members, and the opposite surfaces of the first connecting portion and the second connecting portion have opposite magnetic polarities.

[0017] Optionally, both the fixing plate and the mounting bracket are made of lightweight materials.

[0018] Optionally, a plurality of the above first cavities can be provided, and the plurality of first cavities can be installed at intervals and stacked on the top of the second cavity;

[0019] At least one charging device is provided in a single first cavity.

[0020] The technical solution provided by the present utility model has the following advantages:

[0021] 1. The solar charging hangar provided by the present utility model includes: a hangar and a solar panel; a first cavity and a second cavity are provided inside the hangar. A charging device is installed in the first cavity to place the drone to be charged and charge it; the second cavity is used to place a storage battery, and the storage battery is connected to the charging device; the solar panel is suitable for being installed on the outer surface of the hangar, and the solar panel is connected to the storage battery.

[0022] When using the drone at a position far from the charging pile, this structure can move the entire solar charging hangar to the vicinity of the drone use position. When the drone's battery is low, the drone can be placed on the charging device in the first cavity for charging, improving the charging portability. And using solar energy to convert it into electric energy will not cause environmental pollution, improving the timeliness of power supply. There will be no situation where the storage battery runs out of power and affects the normal power supply of the drone. Moreover, the direct current generated by the solar panel can be directly transmitted to the storage battery to charge the drone, greatly improving the resource utilization rate.

[0023] 2. The solar charging hangar further includes a control structure, which includes: a fixing plate and a driving member. The fixing plate is installed on the surface of the hangar, and the driving member is fixed on the fixing plate. The output shaft direction of the driving member is vertically upward, and an installation bracket is fixed on the output shaft of the driving member, and a solar panel is fixed on the installation bracket. Moreover, a light intensity detector or a light sensor is separately fixed on the installation brackets on both sides of the solar panel. In this embodiment, a light intensity detector and a light sensor are respectively installed on both sides of the solar panel. During the installation process, the solar panel is placed obliquely, that is, the plane where the surface of the solar panel facing the light source intersects with the central axis of the output shaft of the driving member, and the inclination angles of the light intensity detector and the light sensor are the same as the inclination angle of the solar panel, so as to ensure that the light intensity detected by the light intensity detector and the light sensor is the same as the light intensity of the sunlight received by the solar panel, ensuring the stability and consistency of the measurement.

[0024] When the light intensity detector and the light sensor detect the voltage value converted from the collected light energy, when the voltage value is less than the set voltage, it will be fed back to the controller, controlling the driving member to rotate, driving the installation bracket to rotate, and rotating the solar panel to a suitable position until the voltage value of the light sensor is greater than or equal to the set value; at this time, the whole solar panel stays at this position and maintains the power generation state. Through the above settings, the solar panel can find a suitable angle to generate electricity at the maximum power at any time period, so as to improve the use efficiency. BRIEF DESCRIPTION OF THE DRAWINGS

[0025] In order to more clearly illustrate the specific embodiments of the present invention or the technical solutions in the prior art, the following will briefly introduce the drawings required for use in the description of the specific embodiments or the prior art. Obviously, the drawings in the following description are some embodiments of the present invention. For those of ordinary skill in the art, other drawings can be obtained based on these drawings without creative efforts.

[0026] Figure 1 It is an internal perspective view of the hangar in the solar charging hangar provided in the present invention;

[0027] Figure 2 It is a schematic structural diagram of the control structure provided in the present invention;

[0028] Description of the reference numerals:

[0029] 1 - Hangar; 11 - First cavity; 12 - Second cavity;

[0030] 2 - Solar panel;

[0031] 3 - Battery;

[0032] 4 - UAV;

[0033] 5 - Control structure; 51 - Fixed plate; 52 - Driving part; 53 - Mounting bracket;

[0034] 61 - Illuminance detector; 62 - Light sensor. Specific implementation mode

[0035] The technical solution of the present utility model will be clearly and completely described below with reference to the accompanying drawings. Obviously, the described embodiments are part of the embodiments of the present utility model, rather than all of them. All other embodiments obtained by those of ordinary skill in the art based on the embodiments in the present utility model without creative efforts shall fall within the protection scope of the present utility model.

[0036] In the description of the present utility model, it should be noted that the orientation or positional relationship indicated by the terms "center", "upper", "lower", "left", "right", "vertical", "horizontal", "inner", "outer", etc. is based on the orientation or positional relationship shown in the accompanying drawings, and is only for the convenience of describing the present utility model and simplifying the description, rather than indicating or implying that the device or element referred to must have a specific orientation, be constructed and operated in a specific orientation, and therefore cannot be understood as a limitation to the present utility model. In addition, the terms "first" and "second" are only used for descriptive purposes and cannot be understood as indicating or implying relative importance.

[0037] In the description of the present utility model, it should be noted that unless otherwise clearly specified and limited, the terms "installation", "connection", and "connection" should be understood in a broad sense. For example, it can be a fixed connection, a detachable connection, or an integral connection; it can be a mechanical connection or an electrical connection; it can be directly connected, or indirectly connected through an intermediate medium, and it can be the communication inside two elements. For those of ordinary skill in the art, the specific meanings of the above terms in the present utility model can be understood according to specific situations.

[0038] In addition, the technical features involved in different implementation modes of the present utility model described below can be combined with each other as long as they do not conflict with each other.

[0039] Embodiment

[0040] This embodiment provides a solar charging hangar 1, as Figures 1 to 2As shown in the figure, it includes a hangar 1 and a solar panel 2. The hangar 1 is in a cube shape as a whole, and is provided with a first cavity 11 and a second cavity 12 inside. The first cavity 11 is arranged above the second cavity 12. A charging device (not shown in the figure) is installed in the first cavity 11 to place the drone 4 to be charged and charge it. There can be several first cavities 11, and several first cavities 11 can be installed in a stacked and spaced manner at the top of the second cavity 12, that is, a plurality of first cavities are vertically spaced above the second cavity 12, and installation can be completed without occupying too much area. At least one charging device is provided in a single first cavity 11 to increase the number of drones 4 that can be charged simultaneously. The second cavity 12 is used to place the storage battery 3, and the storage battery 3 is connected to the charging device. The solar panel 2 is suitable for being installed on the outer surface of the hangar 1, and the solar panel 2 is connected to the storage battery 3. At least one charging device is provided in a single second cavity 12.

[0041] When using the drone 4 at a position far from the charging pile, the entire solar charging hangar 1 can be carried to the vicinity of the position where the drone 4 is used. When the battery of the drone 4 is insufficient, the drone 4 can be placed on the charging device in the first cavity 11 for charging, improving the portability of charging. And by converting solar energy into electric energy, it will not cause environmental pollution, improving the timeliness of power supply. There will be no situation where the storage battery 3 runs out of power and affects the normal power supply of the drone 4. Moreover, the direct current generated by the solar panel 2 can be directly transmitted to the storage battery 3 to charge the drone 4, greatly improving the resource utilization rate.

[0042] In some other implementable ways, such as Figures 1 to 2 As shown in the figure, the solar charging hangar 1 further includes a control structure 5. The control structure 5 includes: a fixing plate 51 and a driving member 52. The fixing plate 51 is installed on the surface of the hangar 1, and the driving member 52 is fixed on the fixing plate 51. The output shaft direction of the driving member 52 is vertically upward, and a mounting bracket 53 is fixed on the output shaft of the driving member 52, and a solar panel is fixed on the mounting bracket 53. And a light intensity detector 61 or a light sensor 62 is separately fixed on the mounting brackets 53 on both sides of the solar panel. In this embodiment, a light intensity detector 61 and a light sensor 62 are respectively installed on both sides of the solar panel. During installation, the solar panel 2 is placed obliquely, that is, the plane where the surface of the solar panel 2 facing the light source intersects with the central axis of the output shaft of the driving member 52, and the inclination angles of the light intensity detector 61 and the light sensor 62 are the same as the inclination angle of the solar panel 2, so as to ensure that the light intensity detected by the light intensity detector 61 and the light sensor 62 is the same as the light intensity of the sunlight contacted by the solar panel 2, ensuring the stability and consistency of the measurement.

[0043] When the illuminance detector 61 and the light sensor 62 detect the voltage value converted from the collected light energy, when the voltage value is less than the set voltage, it will feedback to the controller to control the rotation of the driving member 52, drive the mounting bracket 53 to rotate, and rotate the solar panel to a suitable position until the voltage value of the light sensor 62 is greater than or equal to the set value; at this time, the entire solar panel 2 stays at this position and maintains the power generation state. Through the above settings, the solar panel 2 can find a suitable angle for maximum power generation at any time period, so as to improve the use efficiency.

[0044] Specifically, a first connection portion (not shown in the figure) is provided on the fixing plate 51 close to the hangar 1. The first connection portion is a clamping groove. There are two first connection portions and they are symmetrically installed on the fixing plate 51 at intervals. A second connection portion (not shown in the figure) is provided on the side of the hangar 1. The second connection portion is a buckle. There are also two second connection portions corresponding to the first connection portion and they are symmetrically opened on the side of the hangar 1 at intervals. The fixing plate 51 can be detachably installed on the surface of the hangar 1 through the cooperation of the first connection portion and the second connection portion. The solar charging panel can be installed on the side wall surface to increase the number of solar panels 2 that can be installed.

[0045] In other implementable ways, both the first connection portion and the second connection portion are magnetic members, and the opposite surfaces of the first connection portion and the second connection portion have opposite magnetisms. Ensure the connection stability between the first connection portion and the second connection portion. Prevent the control structure 5 from falling off the side of the hangar 1 and causing damage to the solar panel 2. And both the fixing plate 51 and the mounting bracket 53 are made of lightweight materials, such as aluminum; reduce the overall mass of the control structure 5 and further reduce the possibility of falling.

[0046] Obviously, the above embodiments are only examples given for clear illustration, rather than limitations on the implementation manners. For those of ordinary skill in the art, other different forms of changes or modifications can be made based on the above description. It is not necessary and impossible to enumerate all the implementation manners here. And the obvious changes or modifications derived therefrom are still within the protection scope of the present invention.

Claims

1. A solar charging hangar, characterized in that, Comprising: A hangar (1), in which a first cavity (11) and a second cavity (12) are provided. A charging device is installed in the first cavity (11) to place an unmanned aerial vehicle (4) to be charged and charge it; the second cavity (12) is used to place a storage battery (3), and the storage battery (3) is connected to the charging device. A solar panel (2), which is adapted to be installed on the outer surface of the hangar (1), and the solar panel (2) is connected to the storage battery (3).

2. The solar-powered charging hangar according to claim 1, wherein The solar charging hangar (1) further includes a control structure (5), the solar panel (2) is adapted to be installed on the control structure (5), and the control structure (5) is used to drive the solar panel (2) to rotate to change the working angle of the solar panel (2).

3. The solar-powered charging hangar according to claim 2, characterized in that, The control structure (5) includes: A fixing plate (51), which is installed on the surface of the hangar (1). A driving member (52), which is connected to the fixing plate (51). An installation bracket (53) is provided at the output shaft end of the driving member (52), and the installation bracket (53) is used to fix the solar panel (2).

4. The solar charging hangar according to claim 3, characterized in that, The plane where the surface of the solar panel (2) facing the light source is located intersects with the central axis of the output shaft of the driving member (52).

5. The solar charging hangar according to claim 3, wherein, The control structure (5) further includes: a light intensity detector (61), and / or a light sensor (62); both the light intensity detector (61) and the light sensor (62) are used for detecting light intensity to control the operation of the driving member (52).

6. The solar charging hangar according to claim 3, characterized in that, A first connecting portion is provided on the fixing plate (51) close to the hangar (1), and a second connecting portion is provided on the side of the hangar (1). The fixing plate (51) can be detachably installed on the surface of the hangar (1) through the cooperation of the first connecting portion and the second connecting portion.

7. The solar charging hangar according to claim 6, wherein, The first connecting portion is a clamping groove, and the second connecting portion is a buckle.

8. The solar-powered charging hangar according to claim 6, wherein Both the first connecting portion and the second connecting portion are magnetic members, and the opposite surfaces of the first connecting portion and the second connecting portion have opposite magnetic polarities.

9. The solar energy charging hangar according to claim 3, characterized in that, Both the fixing plate (51) and the installation bracket (53) are made of lightweight materials.

10. The solar charging hangar according to any one of claims 1-9, characterized in that, A plurality of the first cavities (11) can be provided, and the plurality of the first cavities (11) can be installed at intervals and stacked on the top of the second cavity (12). At least one charging device is provided in a single first cavity (11).

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