Unmanned aerial vehicle performance array placing device

Abstract

The utility model provides an unmanned aerial vehicle performance array placing device which comprises a center plate, four inserting holes are evenly formed in the bottom of the center plate, column rods are inserted in the four inserting holes, threaded blind holes are formed in the middle positions of the upper surfaces of the column rods, threaded heads matched with the threaded blind holes are installed in the middle positions of the lower surfaces of the column rods, and the threaded blind holes are connected with the threaded heads. The threaded head on one column rod is in threaded connection with the interior of the threaded blind hole in the other column rod, a transverse plate is arranged on the lower side of the column rod on the lowermost layer, a vertical screw hole is formed in one side of the upper surface of the transverse plate, the threaded head on the column rod on the lowermost layer is in threaded connection with the interior of the vertical screw hole, and an inserting rod is installed on the side, away from the vertical screw hole, of the lower surface of the transverse plate. And lifting pieces used for supporting undercarriages at the bottoms of the unmanned aerial vehicles are mounted on the two parallel side surfaces of the central plate. The unmanned aerial vehicle supporting device has the following beneficial effect that a plurality of unmanned aerial vehicles can be placed on the uneven ground at the same level.

Description

TECHNICAL FIELD

[0001] The utility model relates to an unmanned plane performance array placing device and belongs to the field of unmanned plane performance facilities. BACKGROUND

[0002] The unmanned plane performance array is a new artistic expression form using multiple unmanned planes to work cooperatively, and through advanced computer program control technology and positioning systems, the multiple unmanned planes can form various patterns, characters or perform dynamic light shows in the air. The unmanned plane performance array requires a large number of unmanned planes and needs a relatively wide site, and then the unmanned planes are placed at the required points in the wide site by using a tape measure. The wide site is uneven, for example, in a wide site such as a lawn, the unmanned planes are difficult to place on the same level, so that the multiple unmanned planes take different time to take off to the same height, and the unmanned planes take off in disorder at the initial stage, which increases the difficulty of unmanned plane control. CONTENT OF THE UTILITY MODEL

[0003] In view of the deficiencies in the prior art, the utility model aims to provide an unmanned plane performance array placing device to solve the problems in the background art, and the utility model places multiple unmanned planes on the same level on uneven ground.

[0004] In order to achieve the above-mentioned purpose, the utility model is implemented by the following technical scheme: an unmanned plane performance array placing device, comprising a center plate, four insertion holes are uniformly arranged on the bottom of the center plate, four column rods are inserted into the insertion holes, a threaded blind hole is arranged in the middle position of the upper surface of the column rod, a threaded head matched with the threaded blind hole is arranged in the middle position of the lower surface of the column rod, the threaded head on one column rod is threadedly connected into the threaded blind hole on another column rod, a horizontal plate is arranged on the lower side of the lowermost column rod, a vertical screw hole is arranged on one side of the upper surface of the horizontal plate, the threaded head on the lowermost column rod is threadedly connected into the vertical screw hole, an insertion rod is arranged on the side of the lower surface of the horizontal plate away from the vertical screw hole, and a lifting piece for supporting the bottom landing gear of the unmanned plane is arranged on both parallel sides of the center plate.

[0005] Further, the lifting piece comprises an insertion plate, T-shaped grooves are formed in two parallel sides of the center plate, two insertion plates are inserted into the T-shaped grooves, a connecting plate is fixedly connected to one side of the insertion plate, one end of the connecting plate away from the insertion plate extends to the outside of the T-shaped groove, an L-shaped plate is installed on the side of the upper surface of the insertion plate close to the center plate, the horizontal part of the L-shaped plate is in sliding contact with the upper surface of the center plate, a first screw hole is formed in the upper surface of the horizontal part of the L-shaped plate, a positioning screw for limiting the relative position of the L-shaped plate and the center plate is screw-connected in the first screw hole, a first insertion groove is formed in one side of the connecting plate away from the insertion plate, a plate head is inserted into the first insertion groove, the plate head is connected with the connecting plate through a connecting screw, and a supporting plate for lifting the bottom landing gear of the unmanned aerial vehicle is fixedly connected to one end of the plate head away from the first insertion groove.

[0006] Further, a second screw hole is formed in the upper surface of the plate head, a first small hole that is communicated with the first insertion groove is formed in the upper surface of the connecting plate, a connecting screw is inserted into the first small hole, and one end of the connecting screw in the first small hole is screw-connected in the second screw hole.

[0007] Further, a second insertion groove is formed in one side of the supporting plate away from the plate head, the plate head on one supporting plate is inserted into the second insertion groove on another supporting plate, a second small hole is formed in the side of the upper surface of the supporting plate close to the second insertion groove, the second small hole is communicated with the second insertion groove, and a connecting screw for limiting the relative position of two adjacent supporting plates is inserted into the second small hole.

[0008] Further, the L-shaped plate and the connecting plate are integrally formed, and the insertion plate and the connecting plate are integrally formed.

[0009] Further, a third screw hole is formed in the side of the lower surface of the horizontal plate away from the vertical screw hole, an external thread is formed on the upper end of the insertion rod, and the threaded end of the insertion rod is screw-connected in the third screw hole.

[0010] The utility model discloses beneficial effects:

[0011] 1. According to the ups and downs of the ground, the center plate is arranged at the unmanned aerial vehicle placing point position, then the proper number of column rods are selected, the threaded head on one column rod is screw-connected in the threaded blind hole on another column rod, and the assembly between multiple column rods is completed in this way, so that the column rod on the uppermost layer of the structure formed by multiple column rods is inserted into the insertion hole on the center plate, the center plate is lifted by the structure formed by four groups of multiple column rods, then the supporting structure formed by the insertion rod and the horizontal plate is installed on the lowermost layer column rod, the center plate can be conveniently and stably placed on the uneven ground, the heights of multiple center plates remain consistent, multiple unmanned aerial vehicles are placed on the multiple center plates respectively, the multiple unmanned aerial vehicles are placed on the uneven ground at the same level, the multiple unmanned aerial vehicles are orderly arranged at the initial stage of taking off, and the difficulty of controlling the unmanned aerial vehicle is reduced.

[0012] 2. Screw the threaded head on the bottommost column into the vertical screw hole on the horizontal plate. This facilitates the assembly and disassembly of the column and the horizontal plate, and also allows for adjusting the orientation of the horizontal plate as needed. This helps to offset the insertion rods from hard ground. Additionally, it facilitates the assembly of the columns and the insertion of the columns into the center plate, making it easier to store and transport the center plate, columns, and other components separately.

[0013] 3. Install the plate head on one of the trays into the first slot to complete the assembly of the tray and the connecting plate. Adjust the position of the insert plate along the T-slot. At this time, the relative position of the tray and the center plate changes. When the distance between the two trays on both sides of the center plate meets the needs of the UAV's bottom landing gear, use the positioning screws to limit the relative position of the L-shaped plate and the center plate. At this time, the relative position of the tray and the center plate remains unchanged, realizing the adjustment of the tray position according to the width of the UAV's bottom landing gear, while eliminating the need to manufacture a large center plate.

[0014] 4. Install the plate head on one tray into the second slot on another tray, and so on, to complete the assembly of multiple trays. This makes it easy to increase or decrease the number of trays on both sides of the center plate according to the spacing of the drone's bottom landing gear, which facilitates the lifting of landing gears with different spacing at the bottom of the drone and expands the scope of application. Attached Figure Description

[0015] Other features, objects, and advantages of this invention will become more apparent from the following detailed description of non-limiting embodiments with reference to the accompanying drawings:

[0016] Figure 1 This is a schematic diagram of the structure of a drone performance array placement device according to the present invention;

[0017] Figure 2 This is a perspective view of the central plate in a drone performance array placement device according to the present invention;

[0018] Figure 3 This is a schematic diagram of the assembly of the threaded head and the column rod in a drone performance array placement device according to the present invention;

[0019] Figure 4 This is a schematic diagram of the assembly of the insert rod and the horizontal plate in a drone performance array placement device according to the present invention;

[0020] Figure 5 This is an assembly diagram of the insert plate, L-shaped plate and connecting plate in a drone performance array placement device of this utility model;

[0021] Figure 6 This is a schematic diagram of the assembly of the board head and the support plate in a drone performance array placement device according to the present invention;

[0022] In the figure: 1 - center plate, 2 - T-shaped slot, 3 - support plate, 4 - second slot, 5 - column, 6 - cross plate, 7 - plug rod, 8 - connecting plate, 9 - L-shaped plate, 10 - positioning screw, 11 - connecting screw, 12 - jack, 13 - threaded blind hole, 14 - threaded head, 15 - vertical screw hole, 16 - first screw hole, 17 - plug plate, 18 - first slot, 19 - first small hole, 20 - second screw hole, 21 - plate head, 22 - second small hole. DETAILED DESCRIPTION

[0023] In order to make the technical means, creative features, purposes and effects of the utility model easy to understand, the utility model is further described below in combination with specific embodiments.

[0024] Please refer to Figures 1-4 The utility model provides a kind of technical scheme: a kind of unmanned plane performance array placing device, including center plate 1, four jacks 12 are evenly provided in the bottom of center plate 1, four jacks 12 are evenly inserted with column 5, threaded blind hole 13 is set in the middle position of the upper surface of column 5, threaded head 14 matched with threaded blind hole 13 is installed in the middle position of the lower surface of column 5, the lower side of the lowermost column 5 is equipped with cross plate 6, vertical screw hole 15 is set in the upper surface of cross plate 6 one side, threaded head 14 on the lowermost column 5 is screwed in vertical screw hole 15, plug rod 7 is installed in the side of the lower surface of cross plate 6 away from vertical screw hole 15, wherein the third screw hole is set in the side of the lower surface of cross plate 6 away from vertical screw hole 15, plug rod 7 upper end is processed with external thread, so that the end of plug rod 7 with external thread is screwed in third screw hole, it is convenient for the disassembly and assembly of plug rod 7 and cross plate 6.

[0025] Please refer to Figures 1-4, according to the ups and downs of the ground, the center plate 1 is set at the unmanned aerial vehicle placement point position, then the appropriate number of column 5 is selected, the threaded head 14 on one column 5 is screwed into the threaded blind hole 13 on another column 5, and so on, the assembly between multiple columns 5 is completed, the uppermost column 5 of the structure is inserted into the insertion hole 12 on the center plate 1, the center plate 1 is lifted by the structure formed by four groups of multiple columns 5, then the support structure formed by the cross plate 6 and the insertion rod 7 is installed on the lowermost column 5, the center plate 1 is stably placed on the uneven ground, the height of multiple center plates 1 is kept consistent, multiple unmanned aerial vehicles are placed on multiple center plates 1, multiple unmanned aerial vehicles are placed on the same level on the uneven ground, the initial flight of multiple unmanned aerial vehicles is avoided, the difficulty of unmanned aerial vehicle control is reduced, the threaded head 14 on the lowermost column 5 is screwed into the vertical screw hole 15 on the cross plate 6, on the one hand, the disassembly and assembly of the column 5 and the cross plate 6 are facilitated, on the other hand, the orientation of the cross plate 6 is adjusted according to the need, the insertion rod 7 is staggered on the ground with high hardness, the column 5 is assembled with each other, and the column 5 and the center plate 1 form the plug-in relationship, the separate storage and transportation of the center plate 1, the column 5 and other components are facilitated, the plate head 21 on one supporting plate 3 is installed in the first insertion slot 18, the assembly of the supporting plate 3 and the connecting plate 8 is completed, the position of the insertion plate 17 is adjusted along the T-shaped slot 2, the relative position of the supporting plate 3 and the center plate 1 is changed, when the distance between the two supporting plates 3 on both sides of the center plate 1 meets the needs of the unmanned aerial vehicle bottom landing gear, the relative position of the L-shaped plate 9 and the center plate 1 is limited by the positioning screw 10, the relative position of the supporting plate 3 and the center plate 1 remains unchanged, the position of the supporting plate 3 is adjusted according to the width of the unmanned aerial vehicle bottom landing gear, and a center plate 1 with large size does not need to be made.

[0026] Referring to Figure 1 , Figure 2 , Figure 5 and Figure 6, the two parallel sides of the center plate 1 are provided with T-shaped grooves 2, two plug plates 17 are inserted into the T-shaped grooves 2, one side of the plug plate 17 is connected and fixed with a connecting plate 8 integrally formed with the plug plate 17, the end of the connecting plate 8 away from the plug plate 17 extends to the outside of the T-shaped groove 2, the upper surface of the plug plate 17 close to one side of the center plate 1 is provided with an L-shaped plate 9 integrally formed with the connecting plate 8, the horizontal part of the L-shaped plate 9 is in sliding contact with the upper surface of the center plate 1, the upper surface of the horizontal part of the L-shaped plate 9 is provided with a first screw hole 16, the first screw hole 16 is threadedly connected with a positioning screw 10 for limiting the relative position of the L-shaped plate 9 and the center plate 1, one side of the connecting plate 8 away from the plug plate 17 is provided with a first insertion groove 18, a plate head 21 is inserted into the first insertion groove 18, that is, the upper surface of the plate head 21 is provided with a second screw hole 20, the upper surface of the connecting plate 8 is provided with a first small hole 19 communicating with the first insertion groove 18, the first small hole 19 is inserted with a connecting screw 11, one end of the connecting screw 11 in the first small hole 19 is threadedly connected in the second screw hole 20, one end of the plate head 21 outside the first insertion groove 18 is connected and fixed with a supporting plate 3 for supporting the bottom landing gear of the unmanned aerial vehicle, so that the plate head 21 on one supporting plate 3 is installed in the first insertion groove 18, the assembly of the supporting plate 3 and the connecting plate 8 is completed, the position of the plug plate 17 is adjusted along the T-shaped groove 2, at this time the relative position of the supporting plate 3 and the center plate 1 changes, when the distance between the two supporting plates 3 on both sides of the center plate 1 meets the needs of the bottom landing gear of the unmanned aerial vehicle, the relative position of the L-shaped plate 9 and the center plate 1 is limited by the positioning screw 10, at this time the relative position of the supporting plate 3 and the center plate 1 remains unchanged, the position of the supporting plate 3 is adjusted according to the width of the bottom landing gear of the unmanned aerial vehicle, and meanwhile there is no need to make a larger center plate 1.

[0027] Referring to Figure 1 , Figure 5 and Figure 6 , one side of the supporting plate 3 away from the plate head 21 is provided with a second insertion groove 4, the plate head 21 on one supporting plate 3 is inserted into the second insertion groove 4 on the other supporting plate 3, one side of the upper surface of the supporting plate 3 close to the second insertion groove 4 is provided with a second small hole 22, the second small hole 22 communicates with the second insertion groove 4, the second small hole 22 is inserted with a connecting screw 11 for limiting the relative position of the two adjacent supporting plates 3, so that the plate head 21 on one supporting plate 3 is installed in the second insertion groove 4 on the other supporting plate 3, and so on, the assembly between the plurality of supporting plates 3 is completed, the number of the supporting plates 3 on both sides of the center plate 1 is increased or decreased according to the distance of the bottom landing gear of the unmanned aerial vehicle, the supporting of the unmanned aerial vehicle with different distance landing gears is facilitated, and the application range is expanded.

[0028] Although the present specification is described in terms of embodiments, not every embodiment exhibits every characteristic or implements every combination of features described in the present specification. In addition, not every embodiment includes every embodiment described in the present specification. The description herein of any embodiment, including any preferred embodiment, is thus intended to be illustrative, and not restrictive. The scope of the present application is thus intended to be broad, and will be set forth in the following claims.

Claims

1. An unmanned aerial vehicle performance array placement device comprising a central plate (1), characterized in that: The bottom of the center plate (1) is uniformly provided with four insertion holes (12), four columnar rods (5) are inserted into the insertion holes (12), a threaded blind hole (13) is formed in the middle of the upper surface of the columnar rod (5), a threaded head (14) is arranged on the middle of the lower surface of the columnar rod (5) and matched with the threaded blind hole (13), the threaded head (14) on one columnar rod (5) is screwed into the threaded blind hole (13) on another columnar rod (5), the lowermost columnar rod (5) is provided with a horizontal plate (6) on the lower side, a vertical screw hole (15) is formed in one side of the upper surface of the horizontal plate (6), the threaded head (14) on the lowermost columnar rod (5) is screwed into the vertical screw hole (15), an insertion rod (7) is arranged on the lower surface of the horizontal plate (6) and away from the vertical screw hole (15), and the two parallel sides of the center plate (1) are both provided with supporting members for supporting the bottom landing gear of the unmanned aerial vehicle.

2. The unmanned aerial vehicle performance array placement device of claim 1, wherein: The supporting member comprises an insertion plate (17), T-shaped grooves (2) are formed in the two parallel sides of the center plate (1), two insertion plates (17) are inserted into the T-shaped grooves (2), a connecting plate (8) is connected and fixed to one side of the insertion plate (17), one end of the connecting plate (8) away from the insertion plate (17) extends to the outside of the T-shaped groove (2), an L-shaped plate (9) is arranged on one side of the upper surface of the insertion plate (17) and close to the center plate (1), the horizontal part of the L-shaped plate (9) is in sliding contact with the upper surface of the center plate (1), a first screw hole (16) is formed in the upper surface of the horizontal part of the L-shaped plate (9), a positioning screw (10) for limiting the relative position of the L-shaped plate (9) and the center plate (1) is screwed into the first screw hole (16), a first insertion slot (18) is formed in one side of the connecting plate (8) away from the insertion plate (17), a plate head (21) is inserted into the first insertion slot (18), the plate head (21) is connected with the connecting plate (8) through a connecting screw (11), and a supporting plate (3) for supporting the bottom landing gear of the unmanned aerial vehicle is connected and fixed to one end of the plate head (21) outside the first insertion slot (18).

3. The drone performance array placement device of claim 2, wherein: A second screw hole (20) is formed in the upper surface of the plate head (21), a first small hole (19) is formed in the upper surface of the connecting plate (8) and communicated with the first insertion slot (18), the connecting screw (11) is inserted into the first small hole (19), and one end of the connecting screw (11) in the first small hole (19) is screwed into the second screw hole (20).

4. The unmanned aerial vehicle performance array placement device of claim 2, wherein: One end of the plate head (21) on one supporting plate (3) is inserted into the second insertion slot (4) on another supporting plate (3), a second small hole (22) is formed in one side of the upper surface of the supporting plate (3) and close to the second insertion slot (4), the second small hole (22) is communicated with the second insertion slot (4), and a connecting screw (11) for limiting the relative position of two adjacent supporting plates (3) is inserted into the second small hole (22).

5. The unmanned aerial vehicle performance array placement device of claim 2, wherein: The L-shaped plate (9) and the connecting plate (8) are in an integral forming structure, and the insertion plate (17) and the connecting plate (8) are in an integral forming structure.

6. The drone performance array placement device of claim 1, wherein: The lower surface of the transverse plate (6) is provided with a third threaded hole on the side away from the vertical threaded hole (15), and the upper end of the insertion rod (7) is provided with external threads.

Images