Unmanned aerial vehicle mounting tool

By designing a drone installation fixture, using electric guide rails and rotary motors to adjust the spacing of the buffer rubber seats, and combining a flip-top frame and a limiting backplate, the problem of inconvenient installation caused by the large drone shell structure was solved, achieving stable support and convenient tool storage, and improving installation efficiency.

CN223533674UActive Publication Date: 2025-11-11CHENGDU THUNDERBIRD TECHNOLOGY CO LTD
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Patent Information

Application Number
CN202520001690.6
Authority / Receiving Office
CN · China
Patent Type
Utility models(China)
Current Assignee / Owner
Filing Date
2025-01-02
Publication Date
2025-11-11
Estimated Expiration
2035-01-02

AI Technical Summary

Technical Problem

The large size of the drone's fuselage structure makes component installation inconvenient and inefficient.

Method used

A drone installation fixture was designed, including an installation platform, adjustment components, and support components. The spacing of the buffer rubber seats is adjusted by an electric guide rail and a rotary motor, and stable support and tool storage are achieved by combining a flip-top frame and a limiting back plate.

Benefits of technology

It improves the convenience and efficiency of drone component installation, and ensures stable support at different workstations and convenient storage of tools.

✦ Generated by Eureka AI based on patent content.

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Abstract

The utility model relates to the technical field of unmanned aerial vehicles, in particular to an unmanned aerial vehicle installation tool which comprises an installation platen, an adjusting groove is formed in the center of one end of the top of the installation platen, an adjusting assembly is arranged above the top of the adjusting groove, and a plurality of buffering rubber bases are arranged above the top of the adjusting assembly. An assembling groove is formed in the center of the other end of the top of the mounting table plate, a tool box is mounted in the assembling groove in an inserted mode, and two supporting assemblies are arranged below the bottom of the mounting table plate. The unmanned aerial vehicle mounting tool is simple in overall structure and convenient and fast to carry, can be conveniently used on different unmanned aerial vehicle mounting stations, and can have a firm and stable supporting effect on a mounting table plate; and meanwhile, the distance between the buffer rubber bases can be adjusted according to the size and model of the unmanned aerial vehicle, so that the unmanned aerial vehicle is conveniently supported, mounting tools needed for mounting the parts are conveniently stored, and the mounting convenience of the parts of the unmanned aerial vehicle is improved.
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Description

Technical Field

[0001] This utility model relates to the field of unmanned aerial vehicle (UAV) technology, and in particular to a UAV installation fixture. Background Technology

[0002] Unmanned aerial vehicles (UAVs) are unmanned aircraft controlled by radio remote control equipment and their own program control devices. They have no cockpit but are equipped with autopilots, program control devices, and other equipment. Ground, shipboard, or mothership remote control stations track, locate, remotely control, telemetry, and transmit data digitally to them using radar and other equipment.

[0003] UAV assembly fixtures are tools or devices specifically designed for UAV assembly. They are mainly used to ensure the accuracy, stability and efficiency of the various components of the UAV during the assembly process.

[0004] During the assembly of a drone, components need to be installed and fixed inside the drone's casing. However, the drone's casing structure is large and difficult to support, resulting in low component installation efficiency. Therefore, a drone installation fixture is proposed to address the above problems. Utility Model Content

[0005] The present invention addresses the problem of providing a drone installation fixture with a simple overall structure, convenient handling, and easy use at different drone installation stations. It provides a firm and stable support for the installation platform. Furthermore, the spacing between the buffer rubber bases can be adjusted according to the size and model of the drone, facilitating drone support and providing a stable bearing effect. Additionally, it allows for convenient storage of installation tools required for installing components, improving the ease and efficiency of drone component installation.

[0006] To achieve the above objectives, the present invention adopts the following technical solution:

[0007] A drone installation fixture includes an installation platform. An adjustment groove is provided at the center of one top end of the installation platform, and an adjustment component is provided above the top of the adjustment groove. Several buffer rubber seats are provided above the top of the adjustment component. A fitting groove is provided at the center of the other top end of the installation platform, and a tool box is inserted into the fitting groove. Two support components are provided at the bottom of the installation platform.

[0008] The adjustment assembly includes a first electric guide rail, two first electric guide rails are respectively fixedly installed on the top center of the adjustment groove, and a first guide rail slide is installed on the top of the first electric guide rail. An electric cylinder is fixedly installed on the top center of the first guide rail slide, and a piston push rod is installed on the top center of the electric cylinder. A crossbeam is fixedly installed on the top of the piston push rod. A second electric guide rail is fixedly installed on both ends of the crossbeam, and a second guide rail slide is installed on the top of the second electric guide rail. A mounting bracket is provided above the top of the second guide rail slide, and the bottom end of the buffer rubber seat is fixedly connected to the top end face of the mounting bracket.

[0009] Furthermore, a rotary motor is fixedly installed at the center of the top end face of the second guide rail slide, and a rotating shaft is connected to the center of the top of the rotary motor. The bottom end of the mounting bracket is fixedly connected to the top end of the rotating shaft. When the rotary motor is working, the mounting bracket can be rotated through the rotating shaft, which makes it easy to adjust the angle of the mounting bracket and facilitates support for the UAV equipment.

[0010] Furthermore, the support assembly includes a flip-up top frame. Four flip-up top frames are respectively welded and fixedly installed around the bottom end face of the mounting platform. The end face of the flip-up top frame has a flip-up through hole. A T-shaped rotating rod is inserted between two flip-up through holes on the end face of the flip-up top frame. A load-bearing support rod is fixedly installed between two T-shaped rotating rods on the same side. An assembly plate is sleeved on the bottom side of the load-bearing support rod. One end of the assembly plate has a first locking stud threaded to both ends on one side. The other end of the outer wall of the assembly plate has a second locking stud threaded to both ends. One end of the second locking stud passes through the assembly plate and connects to the inside of the load-bearing support rod. An anti-slip groove is provided in the center of the bottom end face of the assembly plate, and an anti-slip pad is fixedly installed inside the anti-slip groove. The support assembly facilitates the support and sustenance of the mounting platform. Moreover, it is easy to fold and store, has a compact size, and is easy to transport to different workstations for installation and use.

[0011] Furthermore, a limiting back plate is fixedly installed on one side of the inner end face of the flip-top frame, and the outer side of the limiting back plate is connected to the top outer wall of the load-bearing support rod; the limiting back plate can limit and stop the load-bearing support rod.

[0012] Furthermore, both sides of the outer wall of the load-bearing bracket are provided with stop grooves, and one end of the second locking stud passes through the assembly plate and is inserted into the inside of the stop groove; by connecting the second locking stud through the assembly plate and the stop groove, the assembly plate is fixed to the outside of the load-bearing bracket, which facilitates the limiting of the assembly plate.

[0013] Furthermore, mounting pads are fixedly installed on both sides of the top of the mounting platform, which are located on the outer sides of the mounting slot. A transfer plate is provided on the center of both sides of the top of the tool box, and the bottom of the transfer plate is in close contact with the top end face of the mounting pad. A transfer handle is provided on the center of the top of the transfer plate. The mounting pads support the transfer plate, thereby improving the structural stability of the tool box. The transfer handle allows the tool box to be moved and adjusted, facilitating the storage and installation of installation tools and improving the convenience of drone assembly and installation.

[0014] The beneficial effects of this utility model are as follows: The drone installation fixture has a simple overall structure and is easy to transport. The support components facilitate the support of the mounting platform, making it convenient to use at different drone installation stations and providing a firm and stable support effect for the mounting platform. At the same time, the adjustment components allow for adjustment of the spacing between the buffer rubber seats according to the size and model of the drone, thereby facilitating the support of the buffer rubber seats for the drone and providing a stable support effect. Furthermore, the tool box facilitates the storage of installation tools required for installing components, improving the convenience and efficiency of drone component installation. Attached Figure Description

[0015] Figure 1 This is a schematic diagram of the first overall structure of the present invention;

[0016] Figure 2 This is a schematic diagram of the second overall structure of the present invention;

[0017] Figure 3 This is the overall front view of the present invention;

[0018] Figure 4 This is an overall side view of the present invention;

[0019] Figure 5 This is a top view of the entire utility model;

[0020] Figure 6 for Figure 5 Schematic diagram of the cross section of AA;

[0021] Figure 7 for Figure 5 Cross-sectional view of BB;

[0022] Figure 8 This is a bottom view of the entire utility model.

[0023] Legend:

[0024] 1. Mounting platform; 2. Adjustment slot; 3. Adjustment assembly; 4. Buffer rubber seat; 5. Assembly slot; 6. Mounting pad; 7. Tool box; 8. Support assembly; 31. First electric guide rail; 32. First guide rail slide; 33. Electric cylinder; 34. Piston push rod; 35. Crossbeam frame; 36. Second electric guide rail; 37. Second guide rail slide; 38. Rotary motor; 39. Rotary shaft; 310. Mounting bracket; 81. Tilting top frame; 82. Limiting back plate; 83. Tilting through hole; 84. T-shaped rotating rod; 85. Load-bearing support rod; 86. Assembly plate; 87. First locking stud; 88. Second locking stud; 89. Anti-slip bottom pad. Detailed Implementation

[0025] The technical solutions of the present utility model will be clearly and completely described below with reference to the accompanying drawings of the embodiments. Obviously, the described embodiments are only some embodiments of the present utility model, and not all embodiments. Based on the embodiments of the present utility model, all other embodiments obtained by those skilled in the art without creative effort are within the protection scope of the present utility model.

[0026] Specific implementation examples are given below.

[0027] See Figures 1 to 8 A drone installation fixture includes a mounting platform 1, which provides stable and effective load-bearing capacity. An adjustment groove 2 is centrally located at one top end of the mounting platform 1, and an adjustment component 3 is positioned above the top of the adjustment groove 2, facilitating the installation and fixation of the adjustment component 3. Several buffer seats 4 are positioned above the top of the adjustment component 3, supporting the drone and facilitating the installation and fixation of its components. A fitting groove 5 is centrally located at the other top end of the mounting platform 1, and a tool box 7 is inserted into the fitting groove 5 for storing installation tools needed for drone installation, making it convenient for installation workers to access and use. Two support components 8 are positioned at the bottom of the mounting platform 1, providing support and fixation to the mounting platform 1, effectively improving its structural stability.

[0028] The adjustment assembly 3 includes a first electric guide rail 31. Two first electric guide rails 31 are respectively fixedly installed at the center of the top two sides of the adjustment groove 2. A first guide rail slide 32 is installed at the top of the first electric guide rail 31. An electric cylinder 33 is fixedly installed at the center of the top of the first guide rail slide 32. A piston push rod 34 is installed at the center of the top of the electric cylinder 33. A crossbeam frame 35 is fixedly installed at the top of the piston push rod 34. Second electric guide rails 36 are fixedly installed at both ends of the crossbeam frame 35. A second guide rail slide 37 is installed at the top of the second electric guide rail 36. A mounting bracket 310 is provided above the top of the second guide rail slide 37. The bottom end of the buffer rubber seat 4 is fixedly connected to the top end face of the mounting bracket 310. A rotary motor 38 is fixedly installed at the center of the top end face of the second guide rail slide 37. A rotating shaft 39 is connected to the center of the top of the rotary motor 38. The bottom end of the mounting bracket 310 is fixedly connected to the top end of the rotating shaft 39. When the rotary motor 38 is working, it can drive the mounting bracket 310 to rotate via the rotary shaft 39, making it easy to adjust the angle of the mounting bracket 310 and support the drone equipment. When the two first electric guide rails 31 inside the adjustment groove 2 are working, the first guide rail slide 32 slides on the top of the first electric guide rail 31, thereby adjusting the distance between the two crossbeams 35. According to the installation height requirements of the drone workpiece, the electric cylinder 33 works, and the height of the crossbeam 35 can be adjusted via the piston push rod 34. At the same time, the second electric guide rail 36 inside the crossbeam 35 works, causing the second guide rail slide 37 to adjust the distance between the mounting brackets 310, making it easy for the buffer rubber seat 4 on the top of the mounting bracket 310 to support and support the drone. At the same time, according to the installation requirements of the drone, the rotary motor 38 can drive the mounting bracket 310 to rotate via the rotary shaft 39, and the buffer rubber seat 4 can easily support and support the drone, making it convenient for the installation workers to install the drone parts.

[0029] The support assembly 8 includes four flip-top brackets 81, which are respectively fixedly installed around the bottom end face of the mounting platform 1 by welding. Each flip-top bracket 81 has a flip-through hole 83 on its end face. A T-shaped rotating rod 84 is inserted between two flip-through holes 83 on the end face of each flip-top bracket 81. A load-bearing support rod 85 is fixedly installed between two T-shaped rotating rods 84 on the same side. An assembly plate 86 is sleeved on the bottom outer side of the load-bearing support rod 85. Both ends of one side of the assembly plate 86 are threaded with first locking studs 87. Two... Each end is connected by a second locking stud 88 via a threaded connection, and one end of the second locking stud 88 passes through the assembly plate 86 and connects to the inside of the load-bearing support rod 85. The bottom end face of the assembly plate 86 has an anti-slip groove in the center, and an anti-slip pad 89 is fixedly installed inside the anti-slip groove. The support assembly 8 facilitates the support and support of the mounting platform 1, and is easy to fold and store, with a compact size, making it easy to move the mounting platform 1 to different workstations for installation and use. A limiting back plate 82 is fixedly installed on one side of the inner end face of the flip-top frame 81, and the outer side of the limiting back plate 82 is connected to the top side of the load-bearing support rod 85. The outer wall is connected; the load-bearing support rod 85 can be limited and stopped by the limiting back plate 82; both sides of the outer wall of the load-bearing support rod 85 are provided with stop grooves, and one end of the second locking stud 88 passes through the assembly plate 86 and is inserted into the stop groove; the second locking stud 88 passes through the assembly plate 86 and connects to the stop groove, thereby fixing the assembly plate 86 to the outside of the load-bearing support rod 85, which facilitates the limitation of the assembly plate 86; in use, after placing the mounting plate 1 in a suitable installation position, the load-bearing support rod 85 is rotated, so that the load-bearing support rod 85 drives the T-shaped rotating rod 84 to rotate through the flipping through hole 8 inside the flipping top frame 81. Rotate between 3 until one end of the outer wall of the load-bearing support rod 85 is in contact with and pressed against the end face of the limiting back plate 82. Rotate the assembly plate 86 so that after the load-bearing support rod 85 is rotated to the appropriate position, pass the second locking stud 88 through the assembly plate 86 and connect it to the stop groove, thereby fixing the assembly plate 86 to the outside of the load-bearing support rod 85. Continue until the anti-slip pad 89 at the bottom of the assembly plate 86 is in contact with the end face of the installation position. Use the first locking stud 87 to pass through the assembly plate 86 and connect and fix it to the installation position, thereby fixing and supporting the installation platform 1, so that the installation platform 1 has a firm and stable support and load-bearing effect.

[0030] Mounting pads 6 are fixedly installed on both sides of the top of the mounting platform 1, which is located on the outer side of the mounting slot 5. A transfer plate is provided on the center of the top two sides of the tool box 7, and the bottom of the transfer plate is in close contact with the top end face of the mounting pad 6. A transfer handle is provided on the center of the top of the transfer plate. The mounting pads 6 support the transfer plate, thereby improving the structural stability of the tool box 7. The transfer handle allows the tool box 7 to be moved and adjusted, making it convenient to store and install tools and improving the ease of assembly and installation of the drone.

[0031] The above description is only a preferred embodiment of the present utility model, but the protection scope of the present utility model is not limited thereto. Any equivalent substitutions or changes made by those skilled in the art within the technical scope disclosed in the present utility model, based on the technical solution and the inventive concept of the present utility model, should be included within the protection scope of the present utility model.

Claims

1. A UAV installation fixture, characterized in that, The mounting platform (1) includes an adjustment groove (2) at the center of one top end of the mounting platform (1), an adjustment component (3) is provided above the top of the adjustment groove (2), a plurality of buffer rubber seats (4) are provided above the top of the adjustment component (3), a fitting groove (5) is provided at the center of the other top end of the mounting platform (1), a tool box (7) is inserted into the fitting groove (5), and two support components (8) are provided at the bottom of the mounting platform (1). The adjustment assembly (3) includes a first electric guide rail (31), two first electric guide rails (31) are fixedly installed on the top two sides of the adjustment groove (2), and a first guide rail slide (32) is installed on the top of the first electric guide rail (31). An electric cylinder (33) is fixedly installed on the top center of the first guide rail slide (32), and a piston push rod (34) is installed on the top center of the electric cylinder (33). A crossbeam frame (35) is fixedly installed on the top of the piston push rod (34). A second electric guide rail (36) is fixedly installed on both ends of the crossbeam frame (35), and a second guide rail slide (37) is installed on the top of the second electric guide rail (36). A mounting bracket (310) is provided above the top of the second guide rail slide (37), and the bottom end of the buffer rubber seat (4) is fixedly connected to the top end face of the mounting bracket (310).

2. The UAV installation fixture according to claim 1, characterized in that, A rotary motor (38) is fixedly installed at the center of the top end face of the second guide rail slide (37), and a rotary shaft (39) is connected and installed at the center of the top end of the rotary motor (38). The bottom end of the mounting bracket (310) is fixedly connected to the top end of the rotary shaft (39).

3. The UAV installation fixture according to claim 2, characterized in that, The support assembly (8) includes a flip-top frame (81). Four flip-top frames (81) are respectively fixedly installed around the bottom end face of the mounting platform (1) by welding. The end face of the flip-top frame (81) is provided with a flip-through hole (83). A T-shaped rotating rod (84) is inserted between two flip-through holes (83) on the end face of the flip-top frame (81). A load-bearing support rod (85) is fixedly installed between two T-shaped rotating rods (84) on the same side. The bottom side of the load-bearing support rod (85) An assembly plate (86) is externally fitted, and a first locking stud (87) is threadedly connected to both ends of one side of the assembly plate (86). A second locking stud (88) is threadedly connected to both ends of the other side of the outer wall of the assembly plate (86). One end of the second locking stud (88) passes through the assembly plate (86) and is internally connected to the load-bearing support rod (85). An anti-slip groove is provided in the center of the bottom end face of the assembly plate (86), and an anti-slip pad (89) is fixedly installed inside the anti-slip groove.

4. The UAV installation fixture according to claim 3, characterized in that, A limiting back plate (82) is fixedly installed on one side of the inner end face of the flip-top frame (81), and the outer side of the limiting back plate (82) is connected to the top outer wall of the load-bearing support rod (85).

5. The UAV installation fixture according to claim 4, characterized in that, Both sides of the outer wall of the load-bearing support rod (85) are provided with stop grooves, and one end of the second locking stud (88) passes through the assembly plate (86) and is inserted into the inside of the stop groove.

6. The UAV installation fixture according to claim 5, characterized in that, The other end of the top of the mounting plate (1) is fixedly installed with mounting pads (6) on both sides of the outer side of the mounting slot (5). The tool box (7) is provided with a transport plate in the center of both sides of the top, and the bottom of the transport plate is in close contact with the top end face of the mounting pad (6). The transport plate is provided with a transport handle in the center of the top.