CN213879715U

CN213879715U - Soft unmanned aerial vehicle solar panel mount

Info

Publication number: CN213879715U
Application number: CN202022933217.1U
Authority: CN
Inventors: 张珩
Original assignee: Hubei Daxiu Intelligent Control Technology Development Co ltd
Current assignee: Hubei Daxiu Intelligent Control Technology Development Co ltd
Priority date: 2020-12-07
Filing date: 2020-12-07
Publication date: 2021-08-03
Anticipated expiration: 2030-12-07

Abstract

The utility model relates to a soft unmanned aerial vehicle solar panel fixing frame, which comprises a bottom plate, a vertical plate, a first side plate, a second side plate, a solar panel and a driving mechanism; the riser is installed to bottom plate top one side, and the bottom plate all is equipped with first curb plate with the both sides that the riser is adjacent, all is equipped with first spout on two first curb plates, and the riser all is equipped with the second curb plate with the both sides that the bottom plate is adjacent, all is equipped with the second spout on two second curb plates, and solar panel one side both ends all are equipped with the first slider with first spout matched with, and solar panel opposite side both ends all are equipped with the second slider with second spout matched with, and the solar panel bottom is passed through actuating mechanism with the bottom plate top and is connected. The utility model has the advantages that: this kind of software unmanned aerial vehicle solar panel mount can drive solar panel through actuating mechanism and remove between bottom plate and riser, adjusts solar panel's angle, makes solar panel fully accept illumination, improves solar panel's generating efficiency.

Description

Soft unmanned aerial vehicle solar panel mount

Technical Field

The utility model relates to a software unmanned aerial vehicle technical field especially relates to a software unmanned aerial vehicle solar panel mount.

Background

The soft unmanned aerial vehicle is an unmanned aerial vehicle without a hard framework, is formed by inflating an air bag, has strong loading capacity and high endurance compared with the traditional unmanned aerial vehicle, can fly at ultra-low speed and ultra-low altitude, has good elasticity, is impact-resistant and is not damaged, and can be used for aerial photography, aerial survey, remote sensing and other purposes. The solar panel of the existing soft unmanned aerial vehicle is generally stuck and fixed on the air bag body, and the direction of the solar panel cannot be adjusted according to the sunlight illumination direction, so that the power generation efficiency is low.

SUMMERY OF THE UTILITY MODEL

The utility model aims to solve the technical problem that a software unmanned aerial vehicle solar panel mount is provided, solve the not enough of prior art.

The utility model provides an above-mentioned technical problem's technical scheme as follows: a soft unmanned aerial vehicle solar panel fixing frame comprises a bottom plate, a vertical plate, a first side plate, a second side plate, a solar panel and a driving mechanism; bottom plate top side-mounting there is the riser, the bottom plate with the both sides that the riser is adjacent all are equipped with first curb plate, two all be equipped with first spout on the first curb plate, the riser with the both sides that the bottom plate is adjacent all are equipped with the second curb plate, two all be equipped with the second spout on the second curb plate, solar panel one side both ends all be equipped with first spout matched with first slider, solar panel opposite side both ends all be equipped with second spout matched with second slider, the solar panel bottom with the bottom plate top is passed through actuating mechanism connects, actuating mechanism can drive solar panel at the bottom plate with remove between the riser.

The utility model has the advantages that: this kind of software unmanned aerial vehicle solar panel mount can drive solar panel through actuating mechanism and remove between bottom plate and riser, adjusts solar panel's angle, makes solar panel fully accept illumination, improves solar panel's generating efficiency.

Further: actuating mechanism includes motor, threaded rod, bearing, thread bush, first hinge ear and the hinge ear of second, the motor is installed the bottom plate top, the output shaft of motor with threaded rod one end is connected, the threaded rod other end is established in the bearing, the bearing is installed the bottom plate top, the thread bush is established on the threaded rod, the thread bush outer wall is equipped with first hinge ear, first hinge ear with the hinge ear of second is articulated, the hinge ear of second is installed the solar panel bottom.

The beneficial effects of the further scheme are as follows: the motor can drive the threaded rod to rotate, the threaded rod drives the threaded sleeve to move, and the threaded sleeve drives the solar panel to move through the first hinge lug and the second hinge lug which are mutually hinged.

Further: still include the fixed plate, the fixed plate includes plate body, coupling assembling and pastes the layer, the plate body top with the bottom plate passes through coupling assembling can dismantle the connection, the plate body bottom is equipped with paste the layer.

The beneficial effects of the further scheme are as follows: can paste the plate body on software unmanned aerial vehicle's gasbag fuselage through pasting the layer, can be connected the plate body through coupling assembling simultaneously and fix with the bottom plate, when need not charge unmanned aerial vehicle, can dismantle the mount from software unmanned aerial vehicle, alleviate software unmanned aerial vehicle's weight.

Further: the sticking layer is a foam adhesive layer.

The beneficial effects of the further scheme are as follows: the foam adhesive layer can firmly be pasted on the air bag body of the unmanned aerial vehicle.

Further: coupling assembling includes first fixed block, fixed column, second fixed block and fixing bolt, first fixed block is four and establishes respectively on four angles of bottom plate, every first fixed block top all is equipped with the fixed column, the second fixed block is four and establishes respectively on four angles of plate body, every all be equipped with on the second fixed block with fixed column matched with fixed orifices, every all be equipped with the screw hole in the fixed column, every all be equipped with in the screw hole fixing bolt.

The beneficial effects of the further scheme are as follows: when fixing bolt in the fixed column, can be with first fixed block and second fixed block fixed connection to with bottom plate and plate body fixed connection, when unscrewing fixing bolt in the fixed column, can make first fixed block and second fixed block separation, thereby make bottom plate and plate body separation, convenient operation.

Further: the head of the fixing bolt is provided with a cross-shaped knob.

The beneficial effects of the further scheme are as follows: the cross-shaped knob is arranged at the head of the fixing bolt, so that the fixing bolt can be screwed by hands without using other tools.

Drawings

Fig. 1 is a schematic structural view of a soft unmanned aerial vehicle solar panel fixing frame according to an embodiment of the present invention;

fig. 2 is a schematic view of a local structure of a soft unmanned aerial vehicle solar panel fixing frame according to an embodiment of the present invention;

fig. 3 is a schematic structural view of a connection assembly according to an embodiment of the present invention;

in the figure: 1. a base plate; 2. a vertical plate; 3. a first side plate; 31. a first chute; 4. a second side plate; 41. a second chute; 5. a solar panel; 6. a drive mechanism; 61. a motor; 62. a threaded rod; 63. a bearing; 64. a threaded sleeve; 65. a first hinge ear; 66. a second hinge ear; 7. a fixing plate; 71. a plate body; 72. a connecting assembly; 721. a first fixed block; 722. fixing a column; 723. a second fixed block; 724. fixing the bolt; 725. a cross-shaped knob; 73. and (7) sticking the layer.

Detailed Description

The principles and features of the present invention are described below in conjunction with the following drawings, the examples given are only intended to illustrate the present invention and are not intended to limit the scope of the present invention.

Example one

As shown in fig. 1-3, a soft unmanned aerial vehicle solar panel fixing frame comprises a bottom plate 1, a vertical plate 2, a first side plate 3, a second side plate 4, a solar panel 5 and a driving mechanism 6; riser 2 is installed to 1 top one side of bottom plate, and bottom plate 1 all is equipped with first curb plate 3 with the adjacent both sides of riser 2, all is equipped with first spout 31 on two first curb plates 3, and riser 2 all is equipped with second curb plate 4 with 1 adjacent both sides of bottom plate, all is equipped with second spout 41 on two

second curb plates

4, and 5 one side both ends of solar panel all are equipped with first slider 51 with first spout 31 matched with, and 5 opposite side both ends of solar panel all are equipped with second slider 52 with second spout 41 matched with, and 5 bottoms of solar panel are passed through actuating mechanism 6 with 1 top of bottom plate and are connected, actuating mechanism 6 can drive solar panel 5 is in bottom plate 1 with remove between the riser 2.

Example two

On the basis of the embodiment, actuating mechanism 6 includes motor 61, threaded rod 62, bearing 63, thread bush 64, first articulated ear 65 and second articulated ear 66, motor 61 installs at 1 top of bottom plate, the output shaft and the threaded rod 62 one end of motor 61 are connected, the threaded rod 62 other end is established in bearing 63, bearing 63 installs at 1 top of bottom plate, thread bush 64 cover is established on threaded rod 62, thread bush 64 outer wall is equipped with first articulated ear 65, first articulated ear 65 is articulated with second articulated ear 66, second articulated ear 66 installs in solar panel 5 bottom.

EXAMPLE III

On the basis of the second embodiment, the fixing plate 7 further comprises a fixing plate 7, wherein the fixing plate 7 comprises a plate body 71, a connecting assembly 72 and an adhesive layer 73, the adhesive layer 73 is a foam adhesive layer, the top of the plate body 71 is detachably connected with the bottom plate 1 through the connecting assembly 72, and the adhesive layer 73 is arranged at the bottom of the plate body 71.

Example four

On the basis of the third embodiment, the method comprises the following steps of,

the connecting assembly 72 includes four first fixing blocks 721, four fixing posts 722, four second fixing blocks 723 and fixing bolts 724, the four first fixing blocks 721 are respectively disposed at four corners of the bottom plate 1, the top of each first fixing block 721 is provided with a fixing post 722, the four second fixing blocks 723 are respectively disposed at four corners of the plate body 71, each second fixing block 723 is provided with a fixing hole matched with the fixing post 722, each fixing post 722 is internally provided with a threaded hole, and each threaded hole is internally provided with a fixing bolt 724.

The head of the fixing bolt 724 is provided with a cross-shaped knob 725.

In the description of the present invention, it is to be understood that the terms "center", "longitudinal", "lateral", "length", "width", "thickness", "upper", "lower", "front", "rear", "left", "right", "vertical", "horizontal", "top", "bottom", "inner", "outer", "clockwise", "counterclockwise", "axial", "radial", "circumferential", and the like, indicate the orientation or positional relationship indicated based on the drawings, and are only for convenience of description and simplicity of description, and do not indicate or imply that the device or element referred to must have a particular orientation, be constructed and operated in a particular orientation, and therefore, should not be construed as limiting the present invention.

Furthermore, the terms "first", "second" and "first" are used for descriptive purposes only and are not to be construed as indicating or implying relative importance or implicitly indicating the number of technical features indicated. Thus, a feature defined as "first" or "second" may explicitly or implicitly include at least one such feature. In the description of the present invention, "a plurality" means at least two, e.g., two, three, etc., unless specifically limited otherwise.

In the present invention, unless otherwise expressly stated or limited, the terms "mounted," "connected," and "fixed" are to be construed broadly and may, for example, be fixedly connected, detachably connected, or integrally formed; can be mechanically or electrically connected; they may be directly connected or indirectly connected through intervening media, or they may be connected internally or in any other suitable relationship, unless expressly stated otherwise. The specific meaning of the above terms in the present invention can be understood according to specific situations by those skilled in the art.

In the present application, unless expressly stated or limited otherwise, the first feature may be directly on or directly under the second feature or indirectly via intermediate members. Also, a first feature "on," "over," and "above" a second feature may be directly or diagonally above the second feature, or may simply indicate that the first feature is at a higher level than the second feature. A first feature being "under," "below," and "beneath" a second feature may be directly under or obliquely under the first feature, or may simply mean that the first feature is at a lesser elevation than the second feature.

In the description herein, references to the description of the term "one embodiment," "some embodiments," "an example," "a specific example," or "some examples," etc., mean that a particular feature, structure, material, or characteristic described in connection with the embodiment or example is included in at least one embodiment or example of the invention. In this specification, the schematic representations of the terms used above are not necessarily intended to refer to the same embodiment or example. Furthermore, the particular features, structures, materials, or characteristics described may be combined in any suitable manner in any one or more embodiments or examples. Furthermore, various embodiments or examples and features of different embodiments or examples described in this specification can be combined and combined by one skilled in the art without contradiction.

Although embodiments of the present invention have been shown and described, it is understood that the above embodiments are exemplary and should not be construed as limiting the present invention, and that variations, modifications, substitutions and alterations can be made to the above embodiments by those of ordinary skill in the art without departing from the scope of the present invention.

Claims

1. A soft unmanned aerial vehicle solar panel fixing frame is characterized by comprising a bottom plate (1), a vertical plate (2), a first side plate (3), a second side plate (4), a solar panel (5) and a driving mechanism (6); the vertical plate (2) is arranged on one side of the top of the bottom plate (1), the first side plates (3) are arranged on two sides of the bottom plate (1) adjacent to the vertical plate (2), first sliding grooves (31) are arranged on the two first side plates (3), the two sides of the vertical plate (2) adjacent to the bottom plate (1) are respectively provided with the second side plates (4), the two second side plates (4) are respectively provided with a second sliding chute (41), two ends of one side of the solar panel (5) are respectively provided with a first sliding block (51) matched with the first sliding groove (31), two ends of the other side of the solar panel (5) are respectively provided with a second sliding block (52) matched with the second sliding groove (41), the bottom of the solar panel (5) is connected with the top of the bottom plate (1) through the driving mechanism (6), the driving mechanism (6) can drive the solar panel (5) to move between the bottom plate (1) and the vertical plate (2).

2. The soft unmanned aerial vehicle solar panel mount of claim 1, the driving mechanism (6) comprises a motor (61), a threaded rod (62), a bearing (63), a threaded sleeve (64), a first hinge lug (65) and a second hinge lug (66), the motor (61) is arranged at the top of the bottom plate (1), an output shaft of the motor (61) is connected with one end of the threaded rod (62), the other end of the threaded rod (62) is arranged in the bearing (63), the bearing (63) is arranged at the top of the bottom plate (1), the threaded sleeve (64) is sleeved on the threaded rod (62), the outer wall of the threaded sleeve (64) is provided with the first hinge lug (65), the first hinge lug (65) is hinged with the second hinge lug (66), and the second hinge lug (66) is installed at the bottom of the solar panel (5).

3. The soft unmanned aerial vehicle solar panel mount of claim 1, further comprising a fixing plate (7), wherein the fixing plate (7) comprises a plate body (71), a connecting assembly (72) and a paste layer (73), the top of the plate body (71) is detachably connected with the bottom plate (1) through the connecting assembly (72), and the paste layer (73) is arranged at the bottom of the plate body (71).

4. The soft unmanned aerial vehicle solar panel mount of claim 3, wherein the adhesive layer (73) is a foam adhesive layer.

5. The soft unmanned aerial vehicle solar panel fixing frame of claim 3, wherein the connecting assembly (72) comprises four first fixing blocks (721), four fixing columns (722), four second fixing blocks (723) and fixing bolts (724), the four first fixing blocks (721) are respectively arranged at four corners of the bottom plate (1), the fixing column (722) is arranged at the top of each first fixing block (721), the four second fixing blocks (723) are respectively arranged at four corners of the plate body (71), each second fixing block (723) is provided with a fixing hole matched with the fixing column (722), each fixing column (722) is provided with a threaded hole, and each threaded hole is provided with the fixing bolt (724).

6. The soft unmanned aerial vehicle solar panel mount of claim 5, wherein the fixing bolt (724) head is provided with a cross-shaped knob (725).